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1988 INDEX

1988-001: THE ESA POLICY AND PROGRAMME FOR THE DEVELOPMENT OF ELECTRIC PROPULSION; W. Berry, C. Bartoli, A. Trippi, ESA/ESTEC Technical Directorate, Noordwijk, The Netherlands

1988-002: THE NASA ELECTRIC PROPULSION; James R. Stone, Office of Aeronautics and Space Techology, David C. Byers, National Aeronautics and Space Administration, and David Q. King, Jet Propulsion Laboratory

1988-003: ELECTRIC PROPULSION PROJECTS AND RESEARCHES IN JAPAN; Kyoichi Kuriki, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara-shi 229, Japan; Yoshihiro Nakamura, National Aerospace Laboratory, Jindaiji-higashi-cho, Chofu, Toyko 182, Japan

1988-004: RECENT PROGRESS IN THE USSR ELECTRIC PROPULSION; V.V. Zhurin, A.S. Koroteev, A.A. Porotnikov, B.B. Rodrevich, Academy of Sciences, Moscow, USSR

1988-005: INTERESTS IN ELECTRIC PROPULSION; Captin Wayne M. Schmidt, USAF, and John C. Andrews, U.S. Air Force Astronautics Laboratory, Edwards Air Force Base, CA

1988-006: ELECTRIC PROPULSION: IMPLEMENTATION ISSUES; Rolland Schreib, International Telecommunication Satellite Organization (INTELSAT), Washington, D.C. 20008, USA

1988-007: THE ROLE OF ELECTRIC PROPULSION IN EXTENDING THE ECONOMIC LIFE-CYCLE OF COMMERCIAL EUROPEAN TELECOMMUNICATION SATELLITES; H. G. Lechte and L. C. van Holtz, ESA/ESTEC Communications Department, Noordwijk, The Netherlands

1988-008: ELECTRIC PROPULSION FOR LOW EARTH ORBIT APPLICATIONS; M. Andrenucci, Dipartimento di Ingegneria Aerospaziale, UniversitÃ di Pisa, Pisa, Italy; and A. Trippi, ESA/ESTEC Technical Directorate, Noordwijk, The Netherlands

1988-009: THE ROSETTA/CNSR MISSION: A POSSIBLE APPLICATION OF ELECTRIC PROPULSION TO INTERPLANETARY MISSIONS; A. Atzei, D/SCI, ESA/ESTEC, Noordwijk, The Netherlands

1988-011: PLASMA PROPULSION ACTIVITIES AT SNIA BPD; G. Baiocchi, G. Cruciani, E. Tosti, SNIA BPD, Colleferro, Italy

1988-013: SPACECRAFT AND MISSION DESIGN FOR THE SP-+100 FLIGHT EXPERIMENT, William D. Deininger, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA; and Robert J. Vondra, W. J. Schafer, Associates, Arlington, Virginia, USA

1988-015: DEVELOPMENT OF AN MPD PROPULSION SYSTEM, Y. Shimizu, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Sagamihara-shi, Kanagawa 229, Japan

1988-016: INTERACTION OF HIGH VOLTAGE SOLAR ARRAY WITH IONOSPHERIC PLASMA; H. Kurninaka, S. Satori, Y. Nozaki, and K. Kuriki; Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan

1988-018: THE INTERACTION BETWEEN A POSITIVELY BIASED CONDUCTOR ON A HIGH VOLTAGE SOLAR ARRAY AND A PLASMA; Daniel E. Hastings, MIT, Cambridge, MA 02139, USA

1988-019: DEPLOYABLE AEROSPACE PHOTOVOLTAIC ARRAY BASED ON AMORPHOUSE SILICON ALLOYS; J. J. Hanak, Lee Walter, David Dobias and Harvey Flaisher, Sovonics Solar Systems, 100 West Maple Road, Troy, Michigan 48084, USA

1988-020: FEEP POWER CONDITIONING UNIT: DESIGN AND DEVELOPMENT STATUS; A. Bonati and C. Bocchiola, F.I.A.R., Milan, Italy and D. Valentian, S.E.P. Vernon, France

1988-021: FIELD EMISSION ELECTRIC PROPULSION: EMISSION PERFORMANCE OF SLIT-TYPE LIQUID METAL ION SOURCES; J. Mitterauer, Technishce UniversitÃ¤t Wien, Vienna, Austria

1988-022: FIELD EMISSION ELECTRIC PROPULSION (FEEP) ATTITUDE CONTROL CAPABILILTIES; D. Valentian and J. P. Bugeat; SEP; AND C. Bartoli and H. Von Rohden; ESA/ESTEC

1988-025: CYLINDRICAL STEADY-STATE MPD THRUSTER; H. L. Kurtz, M. Auweter-Kurtz, B. Glocker, H. Habiger, W. Merke, and H. O. Schrade, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart

1988-026: IMPROVED THRUST GENERATION MECHANISM FOR ELECTROTHERMAL/ELECTROMAGNETIC ARCJET; Eiji Nishida, Mitsubishi Electric Corporation and Yukio Shimizu and Kyoichi Kuriki, Institute of Space and Astronautical Science

1988-028: NOZZLE TYPE AND THRUSTER EXPERIMENTAL INVESTIGATION; W. D. Merke, H. Auweter-Kurtz, H. Habiger, H. Kurtz and H. O. Schrade, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart

1988-029: STATUS OF THE RITA – EXPERIMENT ON EURECA; H. Bassner, H-P. Berg, MBB Ottobrunn, FRG; C. Bartoli, and A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands

1988-031: THE PROPOSED DEMONSTRATION OF THE UK-10 ION PROPULSION SYSTEM ON ESA’S SAT-2 SPACECRAFT; D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hants., UK

1988-033: DESIGN AND DEVELOPMENT OF THE UK-10 ION PROPULSION SUBSYSTEM; P. Smith, Principal Propulsion Engineer, Marconi Space Systems Ltd., Portsmouth, U.K.

1988-034: AUXILIARY PROPULSION RF-ENGINE RIT 15 – PROTOTYPE DESIGN AND PERFORMANCE, K. H. Groh, A. Dillmann, H. W. Loeb, F. Weber, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1988-035: SUCCESSFUL COMPLETION OF A CYCLIC GROUND TEST OF A MERCURY ION AUXILIARY PROPULSION SYSTEM; David R. Francisco, Charles A. Low, Jr., and John L. Power; National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1988-036: DESIGN AND INTEGRATION OF AN ELECTRIC PROPULSION SYSTEM ON THE EUROSTAR SPACECRAFT; T. Duhamel, P. H. Ricaud, and P. Greff, MATRA Espace, Toulouse, France

1988-038: NUMERICAL CODES FOR CYLINDRICAL MPD THRUSTERS; P. C. Sleziona, M. Auweter-Kurtz, and H. O. Schrade, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart

1988-039: FLUID MECHANICS IN A MAGNETOPLASMADYNAMIC THRUSTER; D. J. Heimerdinger, and M. Martinez-Sanchez, Massachusetts Institute of Technology, Space Systems Laboratory, Cambridge, Massachusetts 02139

1988-040: AN IMPROVED CODE FOR NOZZLE TYPE STEADY STATE MPD THRUSTERS; M. Auweter-Kurtz, S. F. Glaser, H. L. Kurtz, H. O. Schrade, and P. C. Sleziona; Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart

1988-042: CURRENT DRIVEN INSTABILITIES OF AN ELECTROMAGNETICALLY ACCELERATED PLASMA; E. Y. Choueiri, A. J. Kelly, and R. G. Jahn; Electric Propulsion Laboratory, Princeton University, Princeton, NJ 08544

1988-043: INVESTIGATION OF INSTABILITIES IN MPD THRUSTER FLOWS USING A LINEAR DISPERSION RELATION; D. Rempfer and M. Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart; H. J. Kaeppeler, Institut fÃ¼r Plasmaforschung, UniversitÃ¤t Stuttgart; and M. Maurer, MAN Technologie GmbH, MÃ¼nchen, Federal Republic of Germany

1988-045: DC POWER CONTROL FOR A LIQUID-FED RESISTOJET; Robert P. Gruber, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1988-047: DEVELOPMENT OF A FLIGHT STANDARD POWER CONDITIONING AND CONTROL SYSTEM FOR THE T5 ION THRUSTER; Manoj Mohan, Royal Aerospace Establishment, Farnborough, UK; David Diani, Royal Aerospace Establishment, Farnborough, UK and Polytechnic of Wales, Pontypridd, UK; and David Rees, Polytechnic of Wales, Pontypridd, UK

1988-048: VERIFICATION OF PERFORMANCE AND ENDURANCE OF CAPACITOR BANK FOR THE ELECTRIC PROPULSION EXPERIMENT (EPEX); Y. Kunii, M. Sumida, T. Moriai, H. Sasaki, T. Okamura, H. Harada, and K. Ijichi; Mitsubishi Electric Corporation, Kamakura Works, Kamimachiya, Kamakura, Kanagawa 247, Japan and Y. Shimizu and K. Toki, Institute of Space and Astronautical Science, yoshinodai, Sagamihara, Kanagawa 229, Japan

1988-049: VERIFICATION OF CONTROL SEQUENCE AND ARGORITHM FOR THE ELECTRIC PROPULSION EXPERIMENT (EPEX); M. Sumida, Y. Kunii, T. Moriai, T. Okamura, T. Yoshida, and K. Ijichi; Mitsubishi Electric Corporation, Kamakura Works, Kamimachiya, Kamakura, Kanagawa 247, Japan; and Y. Shimizu and K. Toki; Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa 229, Japan

1988-051: CONTROLLING A STATIONARY ORBIT USING ELECTRIC PROPULSION; Bernard M. Anzel, Laboratory Scientist, Hughes Aircraft Company, Space and Communications Group, Systems Laboratories, El Segundo, California, U.S.A.

1988-056: CONTINUOUS OPERATION OF A QUASI-STEADY MPD PROPULSION SYSTEM WITH AN EXTERNAL MAGNETIC FIELDS; T. Yoshikawa, Y. Kagaya, H. Tahara, and T. Wasa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1988-057: OPTIMIZAATION OF CURRENT DISTRIBUTION IN AN APPLIED-FIELD MPD THRUSTER; A. Sasoh, A. E. Solem, and Y. Arakawa, University of Tokyo, Tokyo, Japan

1988-058: HYBRID MPD THRUSTER WITH AXIAL AND CUSP MAGNETIC FIELDS; H. Tahara, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1988-060: XENON ION THRUSTER TEST FACILITY – DESIGN AND OPERATION; S. Kitamura, K. Miyazaki, Y. Hayakawa, and Y. Nakamura, National Aerospace Laboratory, Tokyo, Japan

1988-061: DISCHARGE PERFORMANCE OF A 12 CM CUSP XENON ION THRUSTER; Yoshihiro Nakamura, Manabu Matsumoto, Shoji Kitamura, and Katsuhiro Miyazaki, National Aerospace Laboratory, Jindaiji-higashi, Chofu, Tokyo 182, Japan, Tokai University

1988-062: HIGH THRUST OPERATION OF THE UK-10 RARE GAS ION THRUSTER (T4A); A. R. Martin and P. M. Latham, Culham Laboratory, Abingdon, Oxon OX14 3DB, England

1988-064: RING CUSP/HOLLOW CATHODE DISCHARGE CHAMBER PERFORMANCE STUDIES; J. A. Vaughn and P. J. Wilbur, Colorado State University, Fort Collins, Colorado U.S.A.

1988-065: SURVEY OF ELECTRIC PROPULSION THRUSTER APPLICABILITY TO NEAR EARTH SPACE MISSIONS; Mitat Birkan, Air Force Office of Scientific Research, Bolling AFB, DC; Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA

1988-067: ELECTRICAL TRANSFER VEHICLE ANALYSIS FOR FUTURE SPACE OPERATIONS (MESCATS); W. Kleinau, D. E. Koelle and W. MÃ¼ller, MBB Space Communications and Propulsion Systems Division, Munich/ Fed. Rep. of Germany

1988-068: A CASE STUDY OF A MISSION TO THE KORDYLEWSKI CLOUDS USING ION PROPULSION; K. A. Ryden, Pinehurt Cottages; P. G. Herrington, Wayman Rd.; and N. C. Wallace, Farnborough Rd., Farnborough, Hants, UK.

1988-069: A SMALL ION-PROPELLED SPACECRAFT FOR NEAR EARTH EXPERIMENTS; K. A. Ryden and N. C. Wallace, Space Department, Royal Aerospace Establishment, Farnborough, Hants, UK

1988-072: CATHODE PROCESSES IN A MPD ARCJET; K. D. Goodfellow and S. N. B. Murthy; School of Mechanical Engineering, Purdue University, West Lafayette, IN 47907

1988:073: THERMAL DESIGN IMPROVEMENTS FROM 30kWe ARCJET ENGINES; W. D. Deininger, A. Chopra, D. Q. King, and T. J. Pivirotto, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1988-074: ELECTRODE EROSION IN STEADY-STATE ELECTRIC PROPULSION ENGINES; Thomas J. Pivirotto and W. D. Deininger, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1988-075: CHARACTERIZATION OF COLD CATHODE EROSION PROCESSES; J. E. Polk, A. J. Kelly, and R. G. Jahn, Electric Propulsion Laboratory, Princeton University, Princeton, NJ 08544

1988-076: ANODE-NOZZLE EXPERIMENTAL ANALYSIS IN A COAXIAL NON-STEADY SOLID PROPELLANT MPD THRUSTER; Giorgio Paccani, University of Roma “La Sapienza,” Roma, Italy

1988-077: THE PROPELLANT SUPPLY AND MONITORING EQUIPMENT (PSME) FOR THE UK-10 ION PROPULSION SUBSYSTEM; S. D. Watson, Senior Propulsion Engineer, Marconi Space Systems Ltd, Portsmouth, England

1988-078: A REVIEW OF THE CATHODE CONSTRUCTION FOR THE RAE 10/25mN THRUSTER; S. A. Gair, Central Materials Laboratory, Philips Components, Mitcham, England; and P. T. Harris, Central Materials Laboratory, Philips Components, Mitcham, England

1988-079: DISCHARGE PLASMA CALCULATIONS IN CUSPED ION THRUSTERS USING THE FINITE ELEMENT METHOD; Yoshihiro Arakawa, University of Tokyo, Tokyo, Japan; and Paul J. Wilbur, Colorado State University, Fort Collins, Colorado, USA.

1988-080: AN APPROACH TO THE PARAMETRIC DESIGN OF ION THRUSTERS; Paul J. Wilbur, Colorado State University, Fort Collins, Colorado 80523, U.S.A.; and John R. Beattie and Jay Hyman, Jr., Hughes Research Laboratories, Malibu, California 90265, U.S.A.

1988-082: MAGNETIC INDUCTION THRUSTER WITH LITHIUM PROPELLANT, Stewart A. Burton and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA

1988-083: EXPERIMENTAL STUDY OF DOUBLE STAGE DISCHARGE HALL ION THRUSTER; Y. Yamagiwa and K. Kuriki, Toshiba Komukai Works, 1 Komukaitoshiba-cho, The Institute of Space and Astronautical Science 3-1-1 Yoshinodai, Sagamihara-shi, Japan

1988-084: ULTIMATE PERFORMANCE LIMITS AND MISSION CAPABILITIES OF ADVANCED ION THRUSTERS; A. R. Martin, A. Bond, and R. A. Bond, Culham Laboratory, Abindon, Oxon, OX14 3DB, England

1988-085: INTERSTELLAR FLIGHT: ASPECTS OF BEAMED ELECTRIC PROPULSION; G. L. Matloff, Baruch College of CUNY, Dept. of Natural Sciences, New York, NY, USA and St. Hilda’s and St. Hugh’s School, Dept. of Mathematics, New York, NY and E. F. Mallove, MIT News Office, Cambridge, MA, USA

1988-086: INTEGRATED FUSION PROPULSION PLANTS FOR AEROSPACE PLANES AND SPACE VEHICLES; Alex Farkas, Mechanical Engineer, Westinghouse Electric Corporation, Sunnyvale, California, U.S.A.

1988-088: QUANTITATIVE IMAGING OF MPD FLOWFIELDS; T. Nakayama, K. Toki, and K. Kuriki, Sagamihara-shi, Kanagawa 229, Japan

1988-091: EXPERIMENTAL EVALUATION OF RESISTOJET THRUSTER PLUME SHIELDS; Lynnette M. Carney, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135; and Allan B. Bailey, Calspan Corporation, Arnold Engineering Development C enter, Arnold Air Force Base, TN 37389

1988-092: ANALYTICAL AND NUMERICAL SOLUTIONS FOR CYLINDRICAL BLAST WAVES IN A PLASMA OF VARYING DENSITY; Bishun D. Pandey, The Ohio State University, Marion, Ohio 43302, U.S.A.

1988-095: A 30-CM DIAMETER XENON ION THRUSTER: DESIGN AND INITIAL TEST RESULTS; Y. Yamagiwa, Y. Takeshita, and H. Kawauchi, Toshiba Komukai Works, 1 Komukaitoshiba-cho, Saiwai-ku, Kawasaki, Japan; H. Yoshida, Toshiba R & D Center, 4-1 Ukishima-cho, Kawasaki-ku, Kawasaki, Japan; D. Miyazaki and T. Higuchi, Toshiba Horikawa-cho Works, 72 Horikawa-cho, Saiwai-ku, Kawasaki, Japan; K. Miyazaki, S. Kitamura, Y. Hayakawa, and Y. Nakamura, National Aerospace Laboratory, 7-44-1 Jindaiji-higashimachi, Chofu, Tokyo, Japan

1988-096: PROPELLANT SELECTION CRITERIA FOR DEEP SPACE ELECTRICALLY PROPELLED MISSIONS; A. R. Martin and P. M. Latham, Culham Laboratory, Abingdon, Oxon OX14 3DB, England

1988-098: INERT GAS PERFORMANCE OF THE RIT 35 MAIN PROPULSION UNIT; K. H. Groh, H. W. Loeb, W. Schmidt, B. Schuetz, and F. Zarnitz, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1988-099: CHARACTERISTICS OF FREE-FLOATING NITROGEN AND HELIUM PLASMAS GENERATED IN A MICROWAVE RESONANT CAVITY; Phillip Balaam, William Maul, and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802

1988-100: NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF A PROPATING MICROWAVE – HEATED PLASMA; Juergen Mueller and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA

1988-101: EXPERIMENTS AND ANALYSIS OF A COMPACT ELECTROTHERMAL THRUSTER; Jes Asmussen, Professor, Department of Electrical Engineering, Michigan State University, East Lansing, MI, USA 48824-1226; and Stan Whitehair, Research Engineer, IBM, T.S. Watson Research Center, Yorktown Hts., NY, USA 10598

1988-103: ELECTROTHERMAL THRUSTERS UTILIZING ELECTRODELESS DISCHARGES; H. Tahara, Y. Tanaka, K. Onoe, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1988-104: PERFORMANCE CALCULATION OF AN H2 ARCJET BY MEANS OF A DUAL CHANNEL MODEL; H. O. Schrade and P. C. Sleziona, UniversitÃ¤t Stuttgart, Institut fÃ¼r Raumfahrtsysteme

1988-105: NUMERICAL STUDIES OF THE FLOW FIELD IN A DC ARCJET THRUSTER; Michio NISHIDA, Department of Aeronautical Engineering, Kyoto University, Kyoto 606, Japan; Keiji KAITA, Kashima Steel Works, Sumitomo Metals Corporation, Kashima-cho, Ibaraki 314, Japan; and Ken-ichi TANAKA, Central Research Laboratory, Mitsubishi Electric Corporation, Amagasaki, Hyogo 661, Japan

1988-106: COMPUTATIONAL INVESTIGATION ON THE CHARACTERISTICS OF A LOW POWER DC ARCJET THRUSTER; Ken-ichi TANAKA and Kazuo TSUCHIYA, Central Research Laboratory, Mitsubishi Electric Corporations, Amagasaki, Hyogo 661, Japan; Keiji KAITA and Michio NISHIDA, Department of Aeronautical Engineering, Kyoto Univerity, Kyoto, 606 Japan

1988-107: A 15 KW EXPERIMENTAL ARCJET; H. L. Kurtz, M. Auweter-Kurtz, B. Glocker, W. Merke, and H. O. Schrade, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Stuttgart, West Germany

1988-108: OPERATING CHARACTERISTICS OF 1 kW HYDRAZINE ARCJET THRUSTER; T. Yoshikawa, K. Onoe, H. Yoshida, and S. Kotani, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan; and H. Suzuki and K. Uematsu, Ishikawajima-Harima Heavy Industries Co. Ltd.

1988-109: EXPERIMENTAL INVESTIGATION ON THE CHARACTERISTICS OF A LOW POWER DC ARCJET THRUSTER; Ken-ichi TANAKA and Kazuo TSUCHIYA, Central Research Laboratory, Mitsubishi Electric Corporation, Amagasaki, Hyogo 661, Japan; and Keiji KAITA and Michio NISHIDA, Department of Aeronautical Engineering, Kyoto University, Kyoto 606, Japan

1988-112: OPTICAL EMISSION SPECTRUM OF THE UK-10 ION THRUSTER OPERATING ON XENON; P. M. Lathem, A. R. Martin and M. T. Cresdee, Culham Laboratory, Abingdon, Oxon OX14 3DB, England

1988-113: DIAGNOSTIC TOOLS FOR AN ION THRUSTER IN SPACE; G. L. Wrenn, K. A. Ryden and D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hants, GU14 6TD, U.K.; A. R. Martin and P. M. Latham, UKAEA Culham Laboratory, Abingdon, Oxon, OX14 3DB, U.K.; and D. R. Rodgers, D. M. Walton, and A. D. Johnstone, UCL Mullard Space Science Laboratory, Holmbury St. Mary, Dorking, Surrey RH5 6NT, U.K.

1988-114: STEADY STATE MPD DEVICES FOR REENTRY SIMULATION; M. Auweter-Kurtz, J. Epple, H. Habiger, H. Kurtz, O. Loesener, E. Messerschmid, and D. Mulzer, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart

1988-116: A 6 CM DIAMETER ION SOURCE FOR ASSISTANT DEPOSITION; Kuang Yuan-Zhu, and Feng Yu-Cai, Space Science and Technology Center, Academia Sinica, P.O. Box 2703, Beijing, China

1988-117: DEVELOPMENT OF HIGH-CURRENT RF-PLASMA SOURCES FOR NEUTRAL PARTICLE INJECTORS; J. Freisinger, H. Hellmann, M. Kaufmann, H. W. Loeb, and A. Scharmann, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG; and W. Kraus, Max-Planck-Institute of Plasma Physics, Boltzmannstrasse 2, D-8046 Garching, FRG

1988-118: NON-PROPULSIVE APPLICATION OF THE RF-ION THRUSTER FOR MATERIAL PROCESSING WITH REACTIVE GASES; J. Freisinger, K. Groh, J. Krempel-Hesse, J. M. Krumeich, H. W. Loeb, A. Scharmann, and H. W. Velten; 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1988-119: THE USE OF ELECTRIC PROPULSION TECHNIQUES FOR LEO ATOMIC OXYGEN SIMULATION; M. A. Kinnersley and J. P. W. Stark, University of Southampton, England

1988-120: PERFORMANCE RESEARCH OF XENON ION ROCKET ENGINE; N. H. Wang, G. F. Wu, Z. Y. Guo, J. Z. Han, J. M. Qin, N. Wang, W. G. Wang, and Y. D. Chen, Chinese Academy of Space Technology, Lanzhou Institute of Physics, P. O. Box 94, Lanzhou, China

1988-124: KREM: A MODEL FOR EVALUATING ORBITAL TRANSFER VEHICLES UTILIZING NUCLEAR ELECTRIC PROPULSION SYSTEMS; W. F. Lyon, Research Associate, Advanced Nuclear Fuels Laboratory, Department of Nuclear Engineering, Texas A&M University, College Station, Texas, United States of America

1988-125: CAPACITORS FOR PULSED ELECTRIC PROPULSION, Rolf Dethlefsen and Joel Ennis, Maxwell Laboratories, Inc., 8888 Balboa Avenue, San Diego, California 92123, USA

1988-126: A TANDEM MIRROR HYBRID PLUME PLASMA PROPULSION FACILTIY; F. R. Chang-Diaz, T. F. Yang, W. A. Krueger, S. Peng, J. Urbahn, X. Yao, and D. Griffin, M.I.T. Plasma Fusion Center, Cambridge, Massachuesetts, 02139, Astronaut Office, NASA, Lyndon B. Johnson Space Center, Houston, Texas 77058, United States of America

1988-127: FIELD EMISSION ELECTRIC PROPULSION (FEEP): EXPERIMENTAL INVESTIGATIONS ON CONTINUOUS AND PULSED MODES OF OPERATION; C. Petagna, H. von Rohden, and C. Bartoli, ESA/ESTEC Technical Directorate, Noordwijk, The Netherlands; and D. Valentian, SEP, Vernon, France

1988 FILE DIRECTORY

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1991 INDEX

1991-001: REVIEW OF EUROPEAN ACTIVITIES ON ELECTRIC PROPULSION; C. Bartoli, ESA Technical Directorate, ESTEC, Noordwijk, The Netherlands

1991-002: AN OVERVIEW OF THE NASA ELECTRIC PROPULSION PROGRAM; Francis M. Curran, Gary L. Bennett, and Marcus A. Watkins, NASA Headquarters, Office of Aeronautics, Exploration, and Technology, Washington, D.C. 20546; David C. Byers, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; and John R. Brophy and Joel C. Sercel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

1991-003: STATE OF WORKS ON ELECTRICAL THRUSTERS IN THE USSR; A. S. Bober, Enterprise “Fakel”; V. P. Kim and G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute; A. S. Koroteev, Research Institute of Thermal Processes; L. A. Latyshev, Moscow Aviation Institute; A. I. Morozov, Institute of Atomic Energy named after I. V. Kurchatove; Yu P. Rylov, All-Union Research Institute of Electromechanics; and V. V. Zhurin, Institute of Earth Magnetism and Wave Propagation, of USSR AcSci

1991-004: ELECTRIC PROPULSION RESEARCH AND DEVELOPMENT IN JAPAN; T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-005: REVIEW OF PLASMA PROPULSION ACTIVITIES IN ITALY; W. D. Deininger, BPD Difesa E Spazio, Colleferro (Roma) Itally; M. Andrenucci, Centrospazio, Pisa, Italy, G. Paccani, University of Rome, Rome, Italy, A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands; and F. Rossi, ASSI, Rome, Italy

1991-006: THE STATUS AND FUTURE PLANS FOR ELECTRIC PROPULSION DEVELOPMENT BY THE UNITED STATES AIR FORCE; Capt. Terry M. Sanks, USAF, OLAC Phillips Laboratory, Edwards Air Force Base, CA 93525-5000; Lt. Barry Raygor, USAF, Space Systems Division AFSC, Los Angeles Air Force Base, CA 90009-2960; and Dr. Mitat A. Birkan, Air Force Office of Scientific Research, Bolling Air Force Base, Washington D.C. 00000-0000

1991-007: THE ADVANCED SPACE PROPULSION PROGRAMMES AT AEA TECHNOLOGY, CULHAM LABORATORY; R. A. Bond, A. R. Martin, and S. D. Watson, Space Applications Department, AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, United Kingdom

1991-009: THE UK-10 ION PROPULSION SYSTEM – A TECHNOLOGY FOR IMPROVING THE COST-EFFECTIVENESS OF COMMUNICATION SPACECRAFT; D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hampshire, UK

1991-010: 18-mN XENON ION PROPULSION SUBSYSTEM; J. R. Beattie, R. R. Robson, and J. D. Williams, Hughes Research Laboratories, Malibu, California 90265, USA

1991-013: HYDRAZINE ARCJET PROPULSION SYSTEM INTEGRATION TESTING; Sidney Zafran, Space & Technology Group, TRW Inc., Redondo Beach, CA 90278

1991-014: FINAL RESULTS OF 15 kWe WATER-COOLED ARCJET TESTING; E. Tosti, BPD Difesa e Spazio, Colleferro, Italy; B. Glocker, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart, Germany; and A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands

1991-015: EXPERIMENTAL AND NUMERICAL STUDIES OF A 10-kW WATER-COOLED ARCJET THRUSTER; H. Tahara, T. Sakakibara, K. Onoe, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-016: MEDIUM POWER ARCJET ANALYSIS AND EXPERIMENTS; B. Glocker, Th. RÃ¶sgen, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart; and A. Laxander, Institut fÃ¼r Computeranwendungen, UniversitÃ¤t Stuttgart

1991-018: HYDROGEN ARCJET TECHNOLOGY; John M. Sankovic, John A. Hamley, Thomas W. Haag, Charles J. Sarmiento, and Francis M. Curran, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1991-019: A REVIEW OF THE THEORY OF SELF-FIELD MPD THRUSTERS; J. L. Lawless, Space Power Inc., San Jose, CA 94134; and V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columbus, Ohio 43210-1107

1991-020: LOCAL ANALYSES IN MPD THRUSTER: MAGNETODYNAMIC REGIMES; J. Marc, G. Chanty, and M. Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, U.S.A.

1991-021: ONSET AND EROSION IN SELF-FIELD MPD THRUSTERS; V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columubs, Ohio 43210, U.S.A.

1991-022: THE ONSET PHENOMENA EXPLAINED BY RUN-AWAY JOULE HEATING; Herbert O. Schrade, Thomas Wegmann, and Thomas Rosgen, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart, Germany

1991-023: THE DEVELOPMENT OF THE CATHODES-COMPENSATORS FOR STATIONARY PLASMA THRUSTERS (SIT) IN USSR; B. A. Arkhipov and K. N. Kozubsky, Enterprise “Fakel, Kaliningrad (obl), USSR

1991-024: DESIGN CONSOLIDATION AND SPACE (PRE)QUALIFICATION OF A PLASMA BRIDGE NEUTRALIZER FOR THE RITA 10 ION THRUSTER; M. Bianconi, G. F. Cirri, G. Matticari, and A. Severi, Proel Tecnologi – Firenze, Italy

1991-025: EVALUATION OF ION THRUSTER BEAM NEUTRALIZATION; S. Shimada, Y. Gotoh, E. Nishida, and H. Takegahara, Space Systems Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Japan; and K. Nakamaru, H. Nagano, and K. Terada, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1991-026: ENDURANCE TEST OF PROEL NEUTRALIZER FOR THE RIT 10: REVIEW OF THE ACTIVITIES AT ESTEC LABORATORIES; H. V. Rohden, ESA/ESTEC – Electric Propulsion Unit, Noordwijk, The Netherland; and G. F. Cirri and G. Matticari, Proel Tecnologie, Firenze, Italy

1991-027: POWER SUPPLY AND CONTROL UNIT FOR RADIOFREQUENCY ION THURSTER RIT; P. Cesa, FIAR SpA Space Division, Corso Milano, 94 Padova, Italy; and S. Gandini, P. Leoni, and G. Passoni, FIAR SpA Space Division, Via Montefeltro, 8 Milano, Italy

1991-028: OPERATING LIMITS OF POWER CONVERTERS FOR HIGH POWER ION ENGINE CONTROL; A. J. Forsyth, P. D. Evans, K. W. E. Cheng, and M. R. D. Al-Mothafar, University of Birmingham, U.K., B15 2TT

1991-029: DEVELOPMENT OF A POWER CONDITIONER UNIT OF A 1-kW ARCJET; M. Andrenucci, University of Pisa, Pisa, Italy; and M. Sandrucci, CENTROSPAZIO, Pisa, Italy

1991-030: TESTING OF THE 30 kW ARCJET PCU STARTER USING THE SHORTING SWITCH APPROACH; See-pok Wong, Manager, Electrical Systems, Space Power, Inc., 621 River Oaks Parkway, San Jose, CA 95134

1991-031: PERFORMANCE MEASUREMENTS OF A RESONANT CAVITY ELECTROTHERMAL THRUSTER; Philip Balaam and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802

1991-032: THEORETICAL MODELING OF DIAGNOSTIC EVALUATIONS OF MICROWAVE GENERATED PLASMA SYSTEMS; Scott S. Haraburda, Department of Chemistry, United States Military Academy, West Point, New York, 10996; Martin C. Hawley and Duane W. Dinkel, Department of Chemical Engineering, Michigan State University, East Lansing, Michigan, 48824

1991-033: DESIGN AND PERFORMANCE CHARACTERISTICS OF A NEW MICROWAVE ELECTROTHERMAL THRUSTER; Juergen Mueller and Michael M. Micci, Department of Aeropsace Engineering, The Pennsylvania State University, University Park, PA, USA

1991-034: THE EFFECT OF MOLECULAR PROPELLANTS ON THE PERFORMANCE OF A RESONANT CAVITY ELECTROTHERMAL THRUSTER; D. J. Sullivan and M. M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA, USA

1991-035: NUCLEAR ELECTRIC PROPULSION FOR FUTURE NASA SPACE SCIENCE MISSIONS; Chen-wan L. Yen and Carl G. Sauer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1991-036: THE ULYSSES MISSION: THE ION PROPULSION ALTERNATIVE; D. G. Fearn, Space Department, Royal Aerospace Establishment, Farnborough, Hampshire, UK

1991-037: MISSION STUDY OF MARS/VENUS PROBES DRIVEN BY ELECTRIC PROPULSION; Hitoshi Kuninaka, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa 229, Japan

1991-038: MISSION AND SYSTEM OPTIMIZATION OF NUCLEAR ELECTRIC PROPULSION VEHICLES FOR LUNAR AND MARS MISSIONS; James H. Gilland, Sverdrup Technology, Inc. NASA Lewis Research Center, Brookpark, Ohio

1991-039: SYSTEMS ENGINEERING OF A NEP ROCKET TO THE MOON AND MARS; Dr. John A. Dearien, Idaho National Engineering Laboratory, Idaho Falls, Idaho; M. P. Doherty, J. A. George, and J. S. Sovey, NASA – Lewis Research Center, Cleveland, Ohio

1991-040: TO PLANETS USING NUCLEAR-ELECTRIC THRUST TO L1, THEN CHEMICAL TO OBTAIN LUNAR FUEL, SHIELDING, SUPPLIES, AND EARTH GRAVITY ASSIST; Thomas M. Morse, Consultant, Mooresville, N.C. 28115, USA

1991-041: IGNITION STABILTY OF A LOW POWER ARCJET; T. Yamada, Y. Iwamoto, Y. Shimizu, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229, Japan

1991-042: DEVELOPMENT OF A LOW POWER RADIATIVELY COOLED THERMAL ARCJET THRUSTER; D. M. Zube, B. Glocker, and H. L. Kurtz, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart, 7000 Stuttgart 80, F. R. Germany; M. Kinnersley and G. MatthÃ¤us, MBB-ERNO Raumfahrttechnik GmBH, 2800 Bremen, F.R. Germany

1991-043: DEVELOPMENT OF A LOW POWER ARCJET THRUSTER: THRUST PERFORMANCE AND LIFE EVALUATION; T. Yoshikawa, K. Onoe, and S. Tsuri, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan; M. Ishil and K. Uematsu, Ishikawajima Harima Heavy Industries Co. Ltd., Isogo, Yokohama, Kanagawa 235, Japan

1991-044: ADVANCED LABORATORY MODEL, 1 kW-CLASS ARCJET ENGINE TESTING; G. Cruciani, M. J. Glogowski, and W. D. Deininger, BPD Difesa e Spazio, Collefero (Roma), Italy; and A. Trippi, ESA/ESTEC, Noordwijk, The Netherlands

1991-045: PERFORMANCE STUDY OF A LABORATORY MODEL OF LOW POWER ARCJET; M. Andrenucci, University of Pisa, Pisa, Italy; G. Saccoccia, ESTEC, Noordwijk, The Netherlands, F. Scortecci, N. Panattoni, U. Schulz, CENTROSPAZIO, Pisa, Italy; and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1991-047: PLASMA DIAGNOSTICS IN MPD THRUSTER PLUMES; M. Andrenucci, F. Paganucci, A. Venturini, and A. Turco, CENTROSPAZIO, Pisa, Italy; and G. Paccani, University of Rome, Italy

1991-048: OPTICAL MEASUREMENT OF VELOCITY DISTRIBUTIONS IN MPD ARCJET; T. Nakayama, T. Yoshida, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1991-049: MPD THRUSTER EXHAUST VELOCITY MEASUREMENT USING INJECTED PLASMA WAVES; K. D. Diamant, D. L. Tilley, E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ 08544

1991-052: IONIZATION PROCESSES IN THE INTERELECTRODE REGION OF AN MPD THRUSTER; T. M. Randolph, W. F. von Jaskowsky, A. J. Kelly and R. G. Jahn, Electric Propulsion Laboratory, Princeton, University, Princeton, NJ 08544

1991-053: MISSION AND OPERATION ASPECTS OF IN-ORBIT ION PROPULSION MANAGEMENT; L. Mazzini and A. Notarantonio, Alenia Spazio S.p.A. Rome, Italy; and S. Falzini and F. Palutan, Space Engineering, S.r.l., Rome, Italy

1991-054: INTEGRATION OF ION PROPULSION TECHNOLOGY IN A SYNCHRONOUS SATELLITE: THE ARTEMIS CHALLENGE; M. SilvI, Alenia Spazio S.p.A., and H. Kellermeier, M.B.B.

1991-055: ION PROPULSION PACKAGE FOR N/S – STATIONKEEPING OF THE ARTEMIS SATELLITE; H. Bassner, H. P. Berg, K. Fetzer, and G. MÃ¼ller, Deutsche Aerospace, Messerschmitt BÃ¶lkow Blohm, Space Communications and Propulsion Systems Division, Munich, Germany

1991-056: THE UK-10 ION THRUSTER TEST PROGRAMME AT AEA TECHNOLOGY, CULHAM LABORATORY; Staff of the Space Applications Department (Principal Author S. D. Watson), AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, United Kingdom

1991-057: RITA DEVELOPMENT AND FABRICATION FOR THE ARTEMIS SATELLITE; H. Bassner, H. P. Berg, and R. Kukies, Deutsche Aerospace, Messerschmitt BÃ¶lkow Blohm GMBH, Space Communications and Propulsion Systems Division

1991-058: DESIGN OF AN MPD ARCJET FOR OPERATION AT GIGAWATT POWER LEVELS; P. J. Turchi, The Ohio State University, Columbus, Ohio, USA

1991-059: BASIC EQUATIONS AND ELEMENTS OF THE DISPERSION RELATION FOR A FOUR-FLUID FORMALISM OF MAGNETO-PLASMADYNAMICS WITH NON-EQUILIBRIUM IONIZATION; H. J. Kaeppeler, Institut fÃ¼r Plasmaforschung der UniversitÃ¤t Stuttgart. F. R. Germany

1991-060: VISCOUS AND DIFFUSIVE EFFECTS IN ELECTROTHERMAL AND MPD ARCJET THRUSTERS; S. Miller and M. Martinez-Sanchez, Space Power and Propulsion Laboratory, Dept. of Aeronautics and Astronautics, MIT, Cambridge, MA 02139

1991-061: QUASI ONE-DIMENSIONAL IONIZING MPD FLOW; G. Lefever-Button and V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columbus, Ohio 43210, U.S.A.

1991-062: THRUST FORMULA FOR AN APPLIED-FIELD MPD THRUSTER DERIVED FROM ENERGY CONSERVATION EQUATION; Akihiro Sasoh, Institute of Fluid Science, Tohoku University, Sendai, Japan; and Yoshihiro Arakawa, Department of Aeronautics, University of Tokyo, Tokyo, Japan

1991-063: A FLIGHT TEST OF THE ALLEVIATION OF SPACECRAFT CHARGING USING A UK-10 ION THRUSTER CATHODE; N. C. Wallace, Space Department, Defence Research Agency, Aerospace Division, Farnborough, Hampshire, U.K.

1991-064: PLASMA CONTRACTOR FOR THE ISTP/POLAR SPACECRAFT; R. R. Robson and W. S. Williamson, Hughes Research Laboratories, Malibu, California 90265; R. C. Olsen, Naval Postgraduate School, Monterey, California 93943; and T. E. Moore, NASA, Marshall Spaceflight Center, Huntsville, Alabama 35812

1991-065: A METAL-ION IMPLANTER BASED ON ION-THRUSTER TECHNOLOGY; Paul J. Wilbur and Ronghua Wei, Department of Mechanical Engineering, Colorado State University, Fort Collins, Colorado

1991-066: THE RF-ION SOURCES ‘RIM’ AND ‘PRIS’ FOR MATERIAL PROCESSING AND SURFACE MODIFICATION; M. Bisten, J. Freisinger, J. Heland, J. Krempel-Hesse, J. Krumeich, H.LÃ¶b, and P. Neumann, 1st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, D-6300 Giessen, FRG

1991-067: ELECTRIC PROPULSION APPLICATIONS IN PLASMA-DRIVEN ELECTROMAGNETIC RAILGUNS; B. Azzerboni, Istituto di Elettrotecnica ed Elettronica, V. le A. Dorica 6, 95125 Catania; and E. Cardelli, M. Raugi, and A. Tellini, Dipartimento di Sistemi Elettrici ed Automazione, Via Diotisalvi 2, 56100 Pisa

1991-068: ENDURANCE TEST OF AN AMMONIA ARCJET AT 10 kWe; J. E. Polk and K. D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1991-070: TESTING OF 30 kW ARCJET PCU WITH ARCJET THRUSTERS; See-pok Wong, Manager, Electrical Systems, Space Power, Inc., 621 River Oaks Parkway, San Jose, CA 95134

1991-071: ACOUSTICAL RESONANT BEHAVIOR AND V-1 CURVES FOR A 30 kWe NITROGEN ARCJET; Montgomery D. Grimes, Southwest Research Institute, San Antonio, TX 78228; and William J. Harris, Edgar A. O’Hair, Lynn L. Hatfield, Magne Kristiansen, and Mary C. Baker; Pulsed Power Laboratory, Texas Tech University, Lubbock, TX 79409

1991-072: HIGH POWER ARCJET THRUSTER EXPERIMENTS; T. M. GÃ¶lz, M. Auweter-Kurtz, H. L. Kurtz, and H. O. Schrade; Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart

1991-073: PERFORMANCE CHARACTERISTICS AND DISCHARGE FEATURES OF A QUASI-STEADY APPLIED-FIELD MPD ARCJET; H. Tahara, F. Takiguchi, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-074: AN EXPERIMENTAL AND NUMERICAL INVESTIGATION OF AN APPLIED-FIELD MAGNETOPLASMADYNAMIC SPACE PROPULSION ENGINE; Thomas J. Pivirotto and Keith D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA

1991-075: CONTINUOUS OPERATIONAL TESTS OF A QUASI-STEADY MPD ARCJET SYSTEM: THERMAL AND PERFORMANCE CHARACTERISTICS; T. Yoshikawa, Y, Kagaya, and K. Onoe, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka 560, Japan

1991-076: PRELIMINARY TEST RESULTS OF A HOLLOW CATHODE MPD THRUSTER; M. A. Mantenieks, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; and R. M. Myers, Sverdrup Technology, Inc., Lewis Research Center Group, Brook Park, Ohio 44142

1991-078: PLASMA ACCELERATION PROCESS IN A HALL-CURRENT THRUSTER; Kimiya Komurasaki, Miharu Hirakawa, and Yoshihiro Arakawa, Department of Aeronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Toyoko, Japan

1991-079: PHYSICAL …. AND CHARACTERISTICS OF STATIONARY PLASMA THRUSTERS WITH CLOSED ELECTRONS DRIFT; A. I. Bugrova, Moscow Institute of Radioelectronics and Automatics, Moscow, USSR; V.P. Kim; Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, USSR; N. A. Maslennikov; Enterprise “Fakel”, Kaliningrad, USSR; and A. I. Morozov, Institute of Atomic Energy Named After I. V. Kurchatov, Moscow, USSR.

1991-080: THE STATE OF RESEARCH AND DEVELOPMENT OF END-HALL PLASMA THRUSTERS IN THE USSR; V. V. Zhurin, Front Range Research, Fort Collins, Colorado; A. G. Popov, A. A. Porotnikov, and V. B. Tikhonov, Moscow Aviation Institute, Moscow; and Iu. A. Utkin, Research Institute for Thermal Processes, Moscow

1991-081: RESEARCH OF ION THRUSTERS IN THE USSR; V. N. Korovkin, Scientific Research Assotiation “Verter”, Kalliningrad, USSR; L. A. Latyshev and V. G. Grigoryan, Moscow Aviation Institute, Moscow, USSR; V. A. Obukhov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute Moscow, USSR

1991-082: RECENT PERFORMANCE RESULTS OF THE RIT 15 AUXILIARY PROPULSION ENGINE; K. H. Groh, N. Kreiling, H. W. Loeb, Th. Schmidkunz, and F. Zarnitz; 1st Institute of Physics, Giessen University, D-6300 Giessen, FRG

1991-083: BEAM DIAGNOSTICS FOR THE CHARACTERIZATION OF ION THRUSTER BEAM PARAMETERS; K. H. Groh, N. Kreiling, H. W. Loeb, Th. Schmidkunz; Ist Institute of Physics, Giessen University, D-6300 Giessen, FRG

1991-084: MICROWAVE ION THRUSTER WITH ELECTRON CYCLOTRON RESONANCE DISCHARGE; H. Miyoshi, S. Ichimura, H. Kuninaka, and K. Kuriki; Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan; and Y. Horiuchi, NEC Corporation, Ikebe-cho, Midori-ku, Yokohama, Kanagawa, Japan

1991-085: PERFORMANCE CHARACTERISTICS OF A MICROWAVE ION THRUSTER USING A RESONANT CAVITY; T. Yasui, H. Tahara, K. Onoe, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Machikaneyama, Toyonaka, Osaka, Japan

1991-087: MPD THRUSTER CALCULATION CONSIDERING HIGH IONIZATION MODES; P. C. Sleziona, M. Auweter-Kurtz, and H. O. Schrade, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart, FRG

1991-088: IONIZATIONAL IGNITION AT THE INLET OF AN MPD THRUSTER; E. J. Sheppard and M. Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, U.S.A.

1991-089: PRE-IONIZATION PROCESSES IN A SELF-FIELD MPD ACCELERATOR; Rodney L. Burton and Nicholas Tiliakos, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1991-091: OPTICAL DIAGNOSTICS OF A LOW POWER HYDROGEN ARCJET; M. A. Cappelli, R. K. Hanson, J. G. Liebeskind, and D. H. Manzella, Stanford University, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford, CA 94305, U.S.A.

1991-092: PLUME ANALYSIS OF A 10 kWe/N ARCJET USING EMISSION SPECTROSCOPY; E. Tosti and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1991-093: LASER FLUORESCENCE VELOCIMETRY OF AN ARCJET EXHAUST PLUME; Wilhelmus M. Ruyten, University of Tennessee-Calspan, Center for Space Transportation and Applied Research, UTSI Research Park, Tullahoma, Tennessee 37388; Dennis Keefer, Center for Laser Applications, University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1991-095: ADVANCED DIAGNOSTICS OF ARCJETS; M. W. Crofton, R. P. Welle, S. W. Janson, and R. B. Cohen, The Aerospace Corporation, Los Angeles, CA 90009

1991-096: EROSION PROCESSES IN THE UK-25 ION THRUSTER; P. M. Latham, A. J. Pearce, and R. A. Bond, Space Applications Department, AEA Technology, Culham Laboratory, Abingdon, OXON OX14 3DB, United Kingdom

1991-097: METAL AND METAL NITRIDE EROSION RATES IN A DIVERGENT FIELD ION ENGINE; Charles E. Garner, John R. Brophy, and L. C. Pless, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1991-098: EROSION RATE DIAGNOSTICS IN ION THRUSTERS USING LASER-INDUCED FLUORESCENE; C. J. Gaeta, R. S. Turley, J. N. Matossian, J. R. Beattie, W. S. Williamson, and J. D. Williams, Hughes Research Laboratories, Malibu, CA 90265

1991-099: THE HALL EFFECT IN A NUMERICAL MODEL OF MPD THRUSTERS; E. H. Niewood and M. Martinez-Sanchez, Space Power and Propulsion Laboratory, Dept. of Aeronautics and Astronautics, MIT, Cambridge, MA 02139

1991-100: CURRENT-DRIVEN PLASMA ACCELERATION VERSUS CURRENT-DRIVEN ENERGY DISSIPATION PART II: ELECTROMAGNETIC WAVE STABILITY THEORY AND EXPERIMENTS; E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ 08544, USA

1991-101: GRADIENT INFLUENCED SPACE CHARGE INSTABILITIES IN MPD THRUSTERS; H. P. Wagner, M. Auwetere-Kurtz, E. W. Messerschmid, Institut fÃ¼r Raumfahrtsysteme (IRS); H. J. Kaeppeler, Institut fÃ¼r Plasmaforschung (IPF), UniversitÃ¤t Stuttgart, FRG

1991-102: AN MPD CODE WITH ANOMALOUS TRANSPORT; G. Caldo, E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey 08544, USA

1991-103: EXPERIMENTAL STUDY OF FEEP EMITTER STARTING CHARACTERISTICS; M. Andrenucci, University of Pisa, Pisa, Italy; S. Marcuccio, L. Spagli, A. Genovese, and F. Repola, CENTROSPAZIO, Pisa, Italy

1991-104: EXPERIMENTAL INVESTIGATION OF FIELD EMISSION ELECTROSTATIC THRUSTERS; A. Ciucci, Auburn University, Auburn, Al, USA; G. Genuini, CENTROSPAZIO, Pisa, Italy, and M. Andrenucci, University of Pisa, Pisa, Italy

1991-105: PROSPECTS OF LIQUID METAL ION THRUSTERS FOR ELECTRIC PROPULSION; J. Mitterauer, Technische UniversitÃ¤t Wien Institut fÃ¼r Allgemeine Elektrotechnick und Elektronik, Gusshausstrasse 27-29, 1040 Wien, Austria

1991-106: THERMIONIC SYSTEMS FOR NUCLEAR ELECTRIC PROPULSION; Thomas H. Van Hagan, General Atomics, P.O. Box 85608, San Diego, California, USA 92186-9784

1991-107: PROPELLANT STORAGE CONSIDERATIONS FOR ELECTRIC PROPULSION; Richard P. Welle, The Aerospace Corporation, Los Angeles, CA 90009

1991-108: A LIGHTWEIGHT LIQUID HYDROGEN STORAGE SYSTEM FOR ELECTRICAL ORBITL TRANSFER VEHICLE APPLICATION; T. M. Miller and E. C. Cady, McDonnell Douglas Space Systems Company, Huntington Beach, California

1991-109: MASS FLOW CONTROLLER OF ION ENGINE SYSTEM; S. Shimada, Y. Gotoh, and H. Takagahara, Space Systems Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Kanagawa, Japan; and H. Nagano, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1991-110: MOEDLLING ARCJET THRUSTER PERFORMANCE; R. Spurrett and R. A. Bond, AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, United Kingdom

1991-111: COMPARISON OF MODEL CALCULATIONS WITH EXPERIMENTAL DATA FROM HYDROGEN ARCJETS; Robert Rhodes and Dennis Keefer, Center for Laser Applications, University of Tennessee Space Institute, Tullahoma, TN 37388

1991-112: NUMERICAL STUDIES OF THE FLOW FIELD IN A LOW POWER DC ARCJET THRUSTER USING NAVIER-STOKES EQUATIONS; Hiroyuki Okamoto and Michio Nishida, Department of Aeronautical Engineering, Kyushu University, Fukouka 812, Japan; and Ken-ichi Tanaka, Central Research Laboratory, Mitsubishi Electric Corporation, Hyougo 661, Japan

1991-113: DEVELOPMENT OF A COMPUTER PROGRAMME OF THE ANALYSIS OF ARCJET NOZZLES; M. Andrenucci, University of Pisa, Pisa, Italy, F. Scortecci, G. Capecchi, and T. WÃ¼nsch, CENTROSPAZIO, Pisa, Italy

1991-114: OPERATION OF A PULSED ELECTROTHERMAL DEVICE WITH THE XRAM INDUCTIVE GENERATOR, J. Ashkenazy, R. Cerny, M. Kanter, and Z. Kaplan, Soreq Nuclear Research Center, Yavne 70600, Israel

1991-115: AN OPTIMAL DESIGN PROCEDURE FOR A PULSE FORMING NETWORK; E. Cardelli, N. Esposito, and M. Raugi, Dipartimento di Sistemi Elettrici ed Automazione, Via Diotisalvi 2, 56100 Pisa; and G. Tina, Dipartimento di Elettrotecnica ed Elettronica, Viale A. Doria 6, 95125 Catania

1991-118: A NUMERICAL CODE FOR CUSPED ION THRUSTERS; Yoshihiro Arakawa and Kazutomi Ishihara, Department of Aeronautics, University of Tokyo, Hongo, Tokyo, 113 Japan

1991-119: THREE-DIMENSIONAL PARTICLE SIMULATION OF GRID EROSION IN ION THRUSTERS; Xiaohang Peng, Wilhelmus M. Ruyten, and Dennis Keefer, Center for Space Transportation and Applied Research and University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1991-120: VARIATIONS OF TRIPLE-GRID GEOMETRY AND POTENTIALS TO ALLEVIATE ACCEL GRID EROSION; B. Free, Scionics, inc. Derwood, MD, USA; J. R. Owens, INTELSAT, Washington, D.C. USA, and P. Wilbur, Colorado State University, Fort Collins, CO, USA

1991-121: ORBITAL CONTROL AND MANOEUVERING OF LIGHTSATS/SYNCHRONOUS SATELLITES: ASSESSMENT OF NEW ION PROPULSION TECHNOLOGIES, BASED ON THE ELECTRON CYCLOTRON RESONANCE PHENOMENON, TO IMPROVE THE PERFORMANCES OF THRUSTERS IN THE MILLINEWTON RANGE; G. Perrotta, Alenia Spazio, Via Saccomuro n. 24-00131 Roma (Italy); M. Bianconi, A. Bicci, M. Capacci, G. F. Cirri, and G. Matticari, Proel Technologie, Viale Machiavelli n. 29-50125 Firenze (Italy)

1991-122: AN INVESTIGATION OF MICROINSTABILITIES IN A kW LEVEL SELF-FIELD MPD THRUSTER; D. L. Tilley, E. Y. Choueiri, A. J. Kelly, R. G. Jahn, Electric Propulsion & Plasma Dynamics Lab, Princeton University, Princeton, NJ 08544

1991-123: SCALE EFFECTS ON THE PERFORMANCE OF MPD THRUSTERS; M. Andrenucci, University of Pisa, Pisa, Italy; F. Paganucci, M. Frazzetta, G. LaMotta, and G. Schianchi, CENTROSPAZIO, Pisa, Italy

1991-125: ANODE POWER DEPOSTITIOIN IN MPD THRUSTERS; A. D. Gallimore, A. J. Kelly, and R. G. Jahn, Electric Propulsion Laboratory, Princeton University, Princeton, New Jersey 08544

1991-126: EXPERIMENTAL COMPARISION OF ELECTRIC OF KINETIC ENERGY TRANSFORMATION EFFECTIVENESS IN ELECTRODISCHARGE AND ELECTRODYNAMIC SYSTEMS; F. G. Rutberg, A. I. Kulishevitch, G. M. Cherniavsky, and S. A. Kaliadin, Department of Physics and Technology, USSR Academy of Sciences, Leningrad, USSR

1991-127: FROM ANTI-GRAVITY TO ZERO-POINT ENERGY: A TECHNICAL REVIEW OF ADVANCED PROPULSION CONCEPTS; George D. Hathaway, Hathaway Consulting Services, 39 Kendal Ave., Toronto, Ontario, Canada M5R 1L5

1991-128: DESIGN CHARACTERISTICS OF THE VARIABLE ISP PLASMA ROCKET; F. R. Chang Diaz and T. F. Yang, M.I.T. Plasma Fusion Center, Cambridge, MA USA

1991-129: AN ICRF PLASMA HEATING EXPERIMENT IN THE TANDEM MIRROR PROPULSION DEVICE; T. F. Yang and S. Peng, MIT Plasma Fusion Center, Cambridge, MA 02139, USA; and F. R. Chang-Diaz, Astronaut Office, NASA, Lyndon B. Johnson Space Center, Houston, TX 77058, USA

1991-130: HIGH CURRENT PULSE HELIUM DISCHARGE AT HIGH PRESSURE; F. G. Bakst, A. M. Voronov, V. N. Zhuravlev, and F. G. Rutberg, VNIIElectromash, Leningrad

1991-132: A LOW ALTITUDE ION-PROPELLED REMOTE SENSING SPACECRAFT; J. Reale, Space Department, Defence Research Agency (Aerospace Division), Royal Aerospace Establishment, Farnborough, Hampshire, United Kingdom

1991-133: SYSTEMS ANALYSIS FOR AN OPERATIONAL EOTV; T. M. Miller, McDonnell Douglas Space Systems Company, Huntington Beach, California

1991-134: OPTIMAL ELECTRIC PROPULSION ORBITAL TRANSFER VEHICLE DESIGN; Y. A. Zakharov, Moscow Aviation Institute, Moscow, USSR

1991-143: PROBLEMS OF ELECTRIC PROPULSION ENDURANCE TESTS; V. I. Baranov, A. I. Vasin, and V. A. Petrosov, Research Institute for Thermal Processes, Moscow; and V. V. Zhurin, Front Range Research, Fort Collins, Colorado

1991-144: SYSTEM PROGRAMMATIC ASPECTS OF THE ION PROPULSION PACKAGE ONBOARD THE ARTEMIS SATELLITE; M. Protto, M. Silvi, S. Greco, Alenia Spazio, H. Kellermeier, M.B.B.

1991-145: ION ENGINE SYSTEM DEVELOPMENT OF ETS-VI; S. Shimada, K. Satoh, Y. Gotoh, E. Nishida, and H. Takegahara, Space Systems Department, Kamakura Works, Mitsubishi Electric Corporation, Kamakura, Kanagawa, Japan; K. Nakamaru, H. Nagano, and K. Terada, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1991-146: ELITE PROGRAM OVERVIEW; Major Ed Avila, OLAC Phillips Laboratory, Edwards Air Force Base, CA 93525-5000

1991-147: DEVELOPMENT OF MPD ACRJET SYSTEM EM FOR SFU-1; Yukio Shimizu and Kyoichiro Toki, Institute of Space and Astronautical Science, Kanagawa, Japan, Hiroshi Suzuki, Kazuo Uematsu, Takenori Otsuka, and Kotaro Shiina, Ishikawajima-Harima Heavy Industries Co. Ltd., Tokyo, Japana, and Yoshinori Kunii, Mitsubishi Electric Co., Kanagawa, Japan

1991-149: APPLICATION AND REVIEW OF THE DEVELOPMENT OF THE CLOSED DRIFT HALL THRUSTER; Joseph R. Wetch, and John L. Lawless, International Scientific Products, San Jose, CA 95134; 408-434-9500; and A. S. Koroteev, The Scientific Research Institute of Thermal Processes, Moscow, USSR

1991-150: DERATED ION THRUSTER DESIGN ISSUES; Michael J. Patterson and Vincent K. Rawlin, National Aeronautics and Space Administration, Lewis Research Center

1991-151: NEUTRALIZER OPTIMIZATION; Michael J. Patterson, National Aeronautics and Space Administration, Lewis Research Center, and Kayhan Mohajeri, Department of Physics, Purdue University

1991-152: THE USE OF SUPERCONDUCTIN MAGNETS FOR PLASMA THRUSTERS; D. E. Gonzalez and G. r. Karr, The University of Alabama in Huntsville, Mechanical Engineering Dept., Huntsville, AL 35899

1991-153: THE ADVANCED PROPULSION SPACE TEST FACILITIES AT AEA TECHNOLOGY, CULHAM LABORATORY; M. S. Harvey & Staff of Space Applications Department, AEA Technology, Culham Laboratory, Abingdon, Oxon OX14 3DB, UK

1991-154: ELECTROSTATIC PROPULSION USING C60 MOLEULES; Stephanie D. Leifer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109; and Winston A. Saunders, California Institute of Technology, Pasadena, CA 91125

1991-155: ARCJET TEST MISSION (ARTEMIS) ON EURECA; Dieter M. Zube, Bernd Glocker, Helmut L. Kurtz, and Ernst W. Messerschmid, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, 7000 Stuttgart 80, F. R. Germany

1991 FILE DIRECTORY

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1993 INDEX

1993-001: DEVELOPMENT AND APPLICATION OF ELECTRIC PROPULSION THRUSTERS IN RUSSIA; A. Bober and N. Maslennikov, FAKEL Enterprises, Kaliningrad, Russia; M. Day, Space Systems/Loral, Palo Alto, CA; G. Popov and Yu. Rylov, Moscow Aviation Institute, Moscow, Russia

1993-002: OVERVIEW OF THE BALLISTIC MISSILE DEFENSE ORGANIZATION’S ELECTRIC PROPULSION PROGRAM; Leonard H. Caveny, Ballistic Missile Defense Organization, Innovative Science and Technology, Washington, DC 20301-7100; Francis M. Curran, NASA Lewis Research Center, Cleveland, Ohio 44135; and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

1993-003: EUROPEAN ELECTRIC PROPULSION ACTIVITIES IN THE ERA OF APPLICATION; C. Bartoli and G. Saccoccia, ESA Technical Directorate, ESTEC, Noordwijk, The Netherlands

1993-004: AN OVERVIEW OF THE AIR FORCE’S ELECTRIC PROPULSION PROGRAM; David R. Perkins, Phillips Laboratory, Edwards AFB, California

1993-005: REVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Y. Arakawa, University of Toyko, Tokyo, Japan

1993-007: FLIGHT QUALIFICATIONS OF A 1.8 KW HYDRAZINE ARCJET SYSTEM; R. D. Smith, S. E. Yano, K. Armbruster, and C. R. Roberts, Rocket Research Company, Redmond, WA USA; D. A. Lichtin and J. W. Beck, Martin Marietta Astro Space, Princeton, NJ, USA

1993-008: DEVELOPMENT AND QUALIFICATION TEST OF A SPT ELECTRIC PROPULSION SYSTEM FOR “GALS” SPACECRAFT; A. Bober, K. Kozubsky, G. Komarow, and N. Maslennikov, FAKEL, Kaliningrad Region, Russia; A. Kozlov and A. Romashko, NPO PM, Krasnoyarsk 26, Russia

1993-009: DEVELOPMENT OF ION ENGINE SYSTEM FOR ETS-VI; S. Shimada, K. Satoh, Y. Gotoh, E. Nishida, I. Terukina, and T. Noro, Mitsubishi Electric Corporation, Japan; H. Takegahara, Tokyo Metropolitan Institute of Technology, Hino, Tokyo, Japan; K. Nakamaru and H. Nagano, National Space Development Agency of Japan, Minato-ku, Tokyo, Japan

1993-010: DESIGN, QUALIFICATION, AND ON-ORBIT PERFORMANCE OF THE ATLAS PLASMA CONTRACTOR; J. R. Beattie, Hughes Research Laboratories, Malibu, California; J. A. Marshall, J. L. Burch, and W. C. Gibson, Southwest Research Institute, San Antonio, Texas

1993-011: ELECTRIC PROPULSION INTEGRATION ACTIVITIES ON THE MSTI SPACECRAFT; D. A. Barnhart, J. M. McCombe, and D. L. Tilley, Air Force Phillips Laboratory, Edwards A.F.B., CA

1993-012: LOW POWER ARCJET SYSTEM DESCRIPTION FOR NORTH-SOUTH STATION KEEPING; W. D. Deininger, M. Vulpiani, E. Tosti, and R. Di Stefano, BPD Difesa e Spazio, Colleferro, Italy, E. Detoma and S. Ferrari, FIAT CIEI (SEPA), Torino, Italy, and M. F. Rossi, ASI, Rome, Italy

1993-013: ARCJET PROPULSION SYSTEM STUDY FOR NSSK; F. Scortecci, L d’Agostino, F. d’Auria, and M. Andrenucci, CENTROSPAZIO, Pisa 56014, Italy

1993-015: APPLICATION OF ION PROPULSION SYSTEM TO COMMUNICATIONS SATELLITES; F. Porte, P. Saint-Aubert, D. Mawby, and J. Hsing, Matra Marconi Space, Intelsat Washington D.C.

1993-016: SPACE-BORNE ASTRONOMICAL GRAVITY-WAVE INTERFEROMETER MISSION (SAGITTARIOUS): THE FIELD EMISSION ELECTRIC PROPULSION (FEEP) OPTION; C. Bartoli, J. Gonzalez, and G. Saccoccia, ESTC, Noordwijk, The Netherlands; M. Andrenucci, University of Pisa, Pisa, Italy; and S. Marcuccio and A. Genovese, CENTROSPAZIO, Pisa, Italy

1993-017: PLASMA THRUSTERS FOR LOW FLYING SATELLITES: A SPACE TELEPHONE SYSTEM APPLICATION; G. A. Dahlen, P. J. Baum, and D.Y. Cheng

1993-018: THE SELECTION FOR NSSK CONTROL SYSTEM OF GEOSYNCHRONUS SATELLITES; Han-Ji Wu, Xue-Zhang Feng, Center for Space Science & Applied Research, Academia Sinica, Beijing 100080, P. R. China

1993-019: ENGINEERING METHODS OF HOLLOW CATHODE CALCULATION; E. P. Vaulin, M. V. Kirushkina, L. A. Latyshev, V. B. Tikhonou, and E. A. Filatova

1993-020: EXTENDED TEST OF A XENON HOLLOW CATHODE FOR A SPACE PLASMA CONTACTOR; Timothy R. Sarver-Verhey, Sverdrup Technology, Inc., NASA Lewis Research Center Group, Brook Park, OH 44142

1993-021: ON THE MECHANISM AND SOME PECULIARITIES OF THE EROSION OF THE ACTIVE SURFACE IN CATHODE-COMPENSATOR OF ELECTRIC PROPULSION; I. M. Yartsev and V. P. Polistchook, Institute for High Temperatures Academy of Science, Moscow, Russia; and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-022: LOCAL EROSION OF THE CATHODE-COMPENSATOR IN ELECTRIC PROPULSION; V. P. Polistchook and I. M. Yartsev, Institute for High Temperatures, Academy of Science, Moscow, Russia; and V. A. Petrosov, The Scientific Research Institute of Thermal Processes, Moscow, Russia

1993-023: CHARACTERISTICS OF IONS EMITTED FROM HIGH-CURRENT HOLLOW CATHODES; Ikuya Kameyama and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1993-024: THEORETICAL MODELING OF ORIFICED, HOLLOW CATHODE DISCHARGES; A. Salhi and P. J. Turchi, The Ohio State University, Columbus, Ohio

1993-025: EXPERIMENTAL INVESTIGATION OF A HOLLOW CATHODE DISCHARGE; A. Salhi, R. M. Myers, and P. J. Turchi, The Ohio State University, Columbus, Ohio

1993-026: THE STUDY OF THE PHYSICS OF HOLLOW CATHODE DISCHARGES; A. K. Malik, Imperial College, London, UK; and D. G. Feam, Defence Research Agency, Farnborough, Hampshire, UK

1993-028: CATHODE EROSION RESEARCH ON MEDIUM TO HIGH POWER ARCJET THRUSTERS; W. J. Harris, E. A. O’Hair, L. L. Hatfield, and M. Kristiansen, Pulsed Power and Electric Propulsion Laboratory, Texas Tech University, Lubbock, TX 79409

1993-029: HIGH CURRENT CATHODE THERMAL BEHAVIOR, PART II: EXPERIMENTS; J. E. Polk, K. D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-030: HIGH CURRENT CATHODE THERMAL BEHAVIOR, PART I: THEORY; K. D. Goodfellow and J. E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-032: C60 MOLECULE AS A PROPELLANT FOR ELECTRIC PROPULSION; Haruki Takegahara and Yoshinori Nakayama, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo, 191, Japan

1993-033: EXPERIMENTAL INVESTIGATION OF FULLERENE PROPELLANT FOR ION PROPULSION; John R. Anderson and Dennis Fitzgerald, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-036: DEVELOPMENT OF A MICROWAVE RESONANT CAVITY ELECTROTHERMAL THRUSTER PROTOTYPE; D. J. Sullivan and M. M. Micci, Propulsion Engineering Research Center, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802, USA

1993-037: PLUME CHARACTERISTICS OF AN ECR PLASMA THRUSTER; D. A. Kaufman and D. G. Goodwin, California Institute of Technology, Pasadena, California

1993-038: ANALYSIS AND EXPERIMENTS OF A WHISTLER-WAVE PLASMA THRUSTER; E. B. Hooper, S. W. Ferguson, M. A. Makowski, and B. W. Stallard, Lawrence Livermore National Laboratory, Livermore, CA 94551; and John L. Power, NASA Lewis Research Center, Cleveland, OH 44135

1993-040: MICROWAVE PLASMA CONTRACTOR; Hitoshi Kuninaka, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan; Nobuo Hiroe, Kazuto Kitaoka, and Yoshio Ishikawa, Nihon University, Narashinodai, Funabashi, Chiba, Japan; and Kazutaka Nishiyama, University of Tokyo, Hongo, Bunkyo, Tokyo, Japan

1993-041: PLASMA CONTACTOR DEVICE BASED ON HOLLOW CATHODE TECHNOLOGY FOR SPACECRAFTS CHARGING NEUTRALIZATION AND TETHERED SYSTEM APPLICATIONS: REVIEW OF ITALIAN NATIONAL PROGRAM; G. F. Cirri, G. Matticari, M. Minucci, G. Noci, A. Severi, and P. Amatulli, Proel Tecnologie – Firenze (Italy); and F. Svelto, ASI (Italian Space Agency), Roma (Italy)

1993-042: HOLLOW CATHODE HEATER DEVELOPMENT FOR THE SPACE STATION PLASMA CONTACTOR; George C. Soulas, Sverdrup Technology, Inc., NASA Lewis Research Center Group, Brook Park, Ohio

1993-043: DESIGN OF A HIGH EFFICIENCY POWER PROCESSOR FOR THE RUSSIAN STATIONARY PLASMA THRUSTER (SPT); G. Fischer, T. Colbert, and M. Day, Space Systems/Loral, Palo Alto, CA, USA; J. Kahn and H. Kaufman, Front Range Research, Fort Collings, CO, USA; K. Kozubsky, and V. Sokolov, Fakel Enterprises, Kaliningrad Region, Russia

1993-044: POWER ELECTRONICS DEVELOPMENT FOR THE SPT-100 THRUSTER; John A. Hamley, Gerald M. Hill, and John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-045: ARCJET POWER CONDITIONING UNIT: DESIGN CHARACTERISTICS AND PRELIMINARY TESTS; G. Botto and M. Carpita, Ansaldo Ricerchi, Corso Perrone 118, 16161, Genova, Italy; G. Parisi and E. Detoma, FIAT-CIEI, Corso G. Cesare 294, 10154 Torino, Italy; and W. Deininger, BPD Difesa e Spazio, Corso Garibaldi 22, 00034 Colleferro, Roma, Italy

1993-046: A 1.8 kW STATIC ARCJET SIMULATOR; E. Detoma and G. Parisi, FIAT CIEI, SEPA, Corso Giulio Cesare, 300 – 10154 Torino To (Italy); and W. Deininger, BPD Difesa e Spazio, Corso Garibaldi, 22 – 00034 Colleferro Rm (Italy)

1993-047: DEVELOPMENT OF A LOW POWER CONTROL UNIT FOR LOW POWER ARCJET; H. Willenbockel, G. Matthaeus, and M. A. Kinnersley, ERNO Raumfahrttechnik GmbH, Deutsche Aerospace AG, Trauen, Germany

1993-048: THE DESIGN, FABRICATION, AND TEST OF A 26 KW ARCJET AND POWER CONDITIONING UNIT; C. E. Vaughan and R. J. Cassady, Rocket Research Company, Redmond, WA 98073; and J. R. Fisher, Pacific Electro Dynamics, Redmond, WA 98073

1993-049: ACHIEVING RELIABLE, REPEATABLE STARTS OF A 26 KW ARCJET; R. S. Aadland, W. A. Hoskins, and C. E. Vaughan, Rocket Research Company, Redmond, WA 98073; and R. J. Kay, Pacific Electro Dynamics, Redmond, WA 98073

1993-052: DEVELOPMENT OF A POWER ELECTRONICS UNIT FOR THE SPACE STATION PLASMA CONTACTOR; John A. Hamley, Gerald M. Hill and Michael J. Patterson, NASA Lewis Research Center, Cleveland, Ohio; Joseph Saggio Jr. and Fred Terdan, Analex Corporation, Cleveland, Ohio; and Justin D. Mansell, Case Western Reserve University, Cleveland, Ohio

1993-053: POWER PROCESSING UNITS FOR HIGH POWERED NUCLEAR ELECTRIC PROPULSION WITH MPD THRUSTERS; Robert H. Frisbee, Radhe S. L. Das, and Stanley Krauthamer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1993-054: SPACE SURVEILLANCE TRACK AND AUTONOMOUS REPOSITION (SSTAR) EXPERIMENT; Lt. Col. S. A. Sneegas, Phillips Laboratory, Kirtland AFB, New Mexico, R. A. Rosenthal, TRW, Redondo Beach, California, and Dr. R. J. Vondra, Phillips Laboratory/ UDRI, Kirtland AFB, New Mexico

1993-055: NEPSTP – AN INTERNATIONAL TESTBED FOR XENON ELECTRIC PROPULSION; Gregg A. Herbert and Glen E. Cameron, The Johns Hopkins University, Applied Physics Laboratory, Laurel, Maryland 20723; and Leonard H. Caveny, Ballistic Missile Defense Organization, Washington, DC 20301-7100

1993-056: DEVELOPMENT AND UTILIZATION OBJECTIVES OF A LOW-POWER ARCJET FOR THE P3-D (OSCAR) SATELLITE; Ernst W. Messerschmid, Dieter M. Zube, and Helmut l. Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Paffenwaldring 31, D-70550 Stuttgart, Federal Republic of Germany; and Kari Meinzer, AMSAT Deutschland e. V., Holderstrauch 10, D-35041 Marburg, Federal Republic of Germany

1993-057: OVERVIEW OF THE AIR FORCE ESEX FLIGHT EXPERIMENT; A. M. Sutton, Phillips Laboratory (AFMC), Edwards AFB, California, USA

1993-058: DEVELOPMENT OF AN MPD THRUSTER SYSTEM FOR THE EPEX SPACE TEST; K. Toki, Y. Shimizu, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan; H. Suzuki, Ishikawajima-Harima Heavy Industries Co., Ltd. Tokyo, Japan, and Y. Kunii, Mitsubishi Electric Corporation, Kanagawa, Japan

1993-059: ION PROPULSION: A KEY ENABLER ON ESA’S DRTM PROGRAMME, H. Bassner, Deutsche Aerospace AG, Ottobrunn; M. Silvi, Alenia Spazio, Rome; L. v. Holtz and C. Bartoli, ESTEC, Noordwijk

1993-061: ELECTRIC PROPULSION: THE NEXT REAL BREAKTHROUGH IN SPACE TRANSPORTATION; Robert L. Sackheim and Richard Rosenthal, TRW Space and Electronics Group, Redondo Beach, California

1993-063: TROPIX: A SOLAR ELECTRIC PROPULSION FLIGHT EXPERIMENT; J. Mark Hickman and G. Barry Hillard, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; Steven R. Oleson, Sverdrup Technology, Inc., Lewis Research Center Group, Brook Park, Ohio 44142

1993-064: NEP EARLY FLIGHT PROGRAM: SYSTEM PERFORMANCE AND DEVELOPMENT CONSIDERATIONS; Michael P. Doherty and Jeffrey A. George, NASA Lewis Research Center, Cleveland, Ohio

1993-065: POTENTIAL NASA EARLY FLIGHT NUCLEAR ELECTRIC PROPULSION MISSIONS; Harvey S. Bloomfield, NASA Lewis Research Center, Cleveland, Ohio

1993-066: NUMERICAL CALCULATIONS OF A CYLINDRICAL MPD THRUSTER; P. C. Sleziona, M. Auweter-Kurtz, and H. O. Schrade; Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart, FRG

1993-068: SPACE CHARGE INSTABILITY, CURRENT CHOPPING AND ANOMALOUS TRANSPORT IN STATIONARY MPD THRUSTER FLOWS; H. P. Wagner, M. Auweter-Kurtz, and E. W. Messerschmid, Institut fÃ¼r Raumfahrtsysteme (IRS), UniversitÃ¤t Stuttgart, FRG

1993-069: NONLINEAR DEVELOPMENT OF SPACE CHARGE INSTABILITY IN MPD-THRUSTER FLOWS; M. Maurer, MAN Technologie AG, Munich, Germany; H. J. Kaeppeler, Institut fÃ¼r Raumfahrtsysteme (IRS), UniversitÃ¤t Stuttgart, Germany

1993-071: IONIZATION RATE MODELS AND INLET IGNITION IN SELF-FIELD MPD THRUSTERS; E. J. Sheppard and M. Martinez-Sanchez, Space Power and Propulsion Lab, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139, U.S.A.

1993-072: NUMERICAL FLUID SIMULATION OF AN MPD THRUSTER WITH REAL GEOMETRY; G. Caldo, E. Y. Choueiri, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey 08544, USA

1993-073: ANALYTICAL STUDY ON NONEQUILIBRIUM FLOWS IN SELF-FIELD MPD THRUSTERS; T. Shoji, K. Ogiwara, and I. Kimura, Department of Aeronautics and Astronautics, School of Engineering, Tokai University, Hiratsuka, Kanagawa, Japan

1993-074: NUMERICAL SIMULATION OF CYLINDRICAL, SELF-FIELD MPD THRUSTERS WITH MULTIPLE PROPELLANTS; Michael R. LaPointe, Sverdrup Technology, Inc. LeRC Group, Brook Park, OH 44142

1993-076: RESEARCH OF PLASMA ACCELERATION PROCESSES IN SELF-FIELD AND APPLIED MAGNETIC FIELD THRUSTERS; V. B. Tikhonov and S. A. Semenihin, Moscow Aviation Institute; V. A. Alexandrov, G. A. Dyakonov, and G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics, Moscow Aviation Institute

1993-077: PLASMA FLOW INVESTIGATION IN MPD-THRUSTER; N. Barabanov, Moscow Aviation Institute, Russia

1993-078: DESIGN AND DEVELOPMENT OF A 3 TO 10 kW AMMONIA ARCJET; K. D. Goodfellow and J. E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-079: HIGH SPECIFIC POWER AMMONIA AND HYDROGEN ARCJET DEVELOPMENT; G. Aston, J. B. Kolts, and M. B. Aston, Electric Propulsion Laboratory, Inc., Monument, CO 80132

1993-081: A REVIEW OF THE ESA ASTP-3 MPD/ARCJET DEVELOPMENT PROGRAM (1988-1993); W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy; M. Andrenucci, Centrospazio, Pisa, Italy, and G. Saccoccia, European Space Agency (ESA/ESTEC), Noordwijk, The Netherlands

1993-082: PERFORMANCE TESTING OF A 1 kW ARCJET THRUSTER USING HYDRAZINE; R. Di Stefano, W. D. Deininger, and E. Tosti, BPD Difesa e Spazio, Colleferro, Italy; and K. Armbruster, Rocket Research Company, Redmond, WA, USA

1993-083: INTERMITTENT OPERATION OF A LOW POWER ARCJET; Tetsuya Yamada, Yoshihiro Iwamoto, Kazuhiko Ogiwara, Kyoichiro Toki, and Kyoichi Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1993-084: EXPERIEMENTAL INVESTIGATION ON ARCJETS PERFORMANCE AND POSSIBLE APPLICATION TO CURRENT MISSION CONCEPTS WITH LOW-POWER AVAILABILITY; F. Scorteci and F. Paganucci, Centrospazio, Pisa, Italy; G. Saccoccia and J. Gonzalez, ESA/ESTEC, Noordwijk, The Netherlands

1993-087: DEVELOPMENT AND DEMONSTRATION OF A 600 SECOND MISSION AVERAGE ARCJET; Paul G. Lichon, Rocket Research Company, Redmond, WA 98073; and John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135

1993-088: DEVELOPMENT OF A 10 kWe/N RADIATIVELY-COOLED ARCJET TECHNOLOGY; E. Tosti and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1993-091: PERFORMANCE EVALUATION AND LIFE TESTING OF THE SPT-100; Charles E. Garner, James E. Polk, Lewis C. Pless, Keith D. Goodfellow, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1993-092: EFFECT OF BACKGROUND NITROGEN AND OXYGEN ON INSULATOR EROSION IN THE SPT-100; J. Kahn and V. Zhurin, Front Range Research, Fort Collins, CO; K. Kozubsky, Fakel Enterprise, Kaliningrad on Baltic Sea, Russia; T. Randolph, Space System/Loral, Palo Alto, CA; V. Kim, RIAME at Moscow Aviation Institute, Moscow, Russia

1993-093: FACILITY EFFECTS ON STATIONARY PLASMA THRUSTER TESTING; T. Randolph and M. Day, Space Systems/Loral, Palo Alto, CA, USA; V. Kim, Research Institute of Applied Mechanics and Electrodynamics, Moscow, Russia; H. Kaufman and V. Zhurin, Front Range Research, Fort Collins, CO, USA; and K. Kozubsky, Fakel, Kaliningrad Region, Russia

1993-094: PERFORMANCE EVALUATION OF THE RUSSIAN SPT-100 THRUSTER AT NASA LeRC; John M. Sankovic, John A. Hamley, and Thomas W. Haag, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-095: DYNAMIC CHARACTERISTICS OF CLOSED DRIFT THRUSTER; V. Zhurin, J. Kahn, and H. Kaufman, Front Range Research, Fort Collins, Colorado; K. Kozubsky, Fakel Enterprise, Kaliningrad on Baltic Sea, Russia; and M. Day, Space Systems Loral, Palo Alto, California

1993-096: STATIONARY PLASMA THRUSTER PLUME CHARACTERISTICS; Roger M. Myers and David H. Manzella, Sverdrup Technology, Inc. NASA Lewis Research Center Group, Brookpark, OH 44142

1993-097: STATIONARY PLASMA THRUSTER PLUME EMISSIONS; David H. Manzella, Sverdrup Technology Inc., Lewis Research Center Group, Brook Park, Ohio 44142

1993-098: PRELIMINARY FAR-FIELD PLUME SPUTTERING CHARACTERIZATION OF THE STATIONARY PLASMA THRUSTER (SPT-100); Eric J. Pencil, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-099: PREDICTION OF ELECTRIC THRUSTER LIFETIME; V. I. Baranov, A. I. Vasin, A. A. Kalyaev, and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-100: ELECTRIC ROCKET ENGINE ACCELERATED TEST CONCEPT; V. I. Baranov, A. I. Vasin, A. A. Kalyaev, and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-101: STATIONARY PLASMA THRUSTER (SPT) DEVELOPMENT STEPS AND FUTURE PERSPECTIVES; A. J. Morozov, Kurchatov Institute, Moscow, Russia

1993-102: FLIGHT TEST RESULTS OF THE RITA EXPERIMENT ON EURECA; H. Bassner, H. P. Berg, R. Kukies, and H. MÃ¼ller, DASA, Munich, Germany

1993-104: A COMPREHENSIVE TEST AND EVALUATION PROGRAM FOR THE UK-10 ION ENGINE; M. W. Crofton, Technology Operations, Mechanics & Materials, M5/754, PO Box 92957, The Aerospace Corporation, Los Angeles, California 90009

1993-105: RECENT ION THRUSTER DEVELOPMENTS AT GIESSEN UNIVERSITY; K. H. Groh, P. Fahrenbach, and H. W. Loeb, Institute of Physics, University of Giessen, Heinrich-Buff-Ring 16, 6300 Giessen, Germany

1993-106: FLIGHT QUALIFICATION OF AN 10-mN XENON ION THRUSTER; J. R. Beattie, J. D. Williams, and R. R. Robson, Hughes Research Laboratories, Malibu, California 90265

1993-107: LOW THRUST ION PROPULSION: DEVELOPMENT ACTIVITIES AT PROEL TECNOLOGIE; G. F. Cirri, G. Matticari, and G. Noci, Proel Tecnologie, Firenze (Italy); G. Perrotta, Alenia Spazio, Roma (Italy), M. F. Rossi and J. Sabbagh, ASI (Italian Space Agency), Roma (Italy)

1993-108: PERFORMANCE OF THE NASA 30 CM ION THRUSTER; Michael J. Patterson and Thomas W. Haag, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; and Scot A. Hovan, Department of Mechanical Engineering, University of Dayton, Dayton, Ohio

1993-109: REVIEW OF QUALIFICATION ACTIVITIES ON THE NEUTRALIZER FOR THE RIT 10 ION THRUSTER; G. F. Cirri, A. Cipriani, G. Matticari, and A. Severi, Proel Tecnologie, Firenze (Italy); C. Bartoli, G. Saccoccia, and H. Von Rohden, ESA/ESTEC Electric Propulsion Unit, Noordwijk, The Netherlands

1993-110: OPERATING CHARACTERISTICS OF A 15-cm-dia. ION ENGINE FOR SMALL PLANETARY SPACECRAFT; John R. Brophy, Lewis C. Pless, Juergen Mueller, and John R. Anderson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-111: COMPARISON OF EROSION OF CARBON-CARBON AND MOLYBDENUM ION OPTICS; J. S. Meserole and D. E. Hedges, Boeing Defense & Space Group, Seattle, WA 98124

1993-112: FABRICATION OF CARBON-CARBON GRIDS FOR ION OPTICS; Juergen Mueller, David K. Brown, Charles E. Garner, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1993-115: PERFORMANCE OF HOT CATHODE MPD THRUSTERS; F. Paganucci and M. Andrenucci, Centrospazio, Pisa, Italy

1993-116: EVALUATION OF EXTERNALLY HEATED PULSED MPD THRUSTER CATHODES; Roger M. Myers, Sverdrup Technology, Inc. NASA Lewis Research Center Group, Brook Park, OH 44135; Matthew Domonkos, The University of New Mexico, Albuquerque, NM 87131; and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI 48109

1993-117: HIGH-CURRENT STATIONARY PLASMA ACCELERATOR OF HIGH POWER; V. P. Ageyev and V. G. Ostrovsky, Scientific-Production Association “Energiya,” Kaliningrad, Moscow Region, Russia; and V. A. Petrosov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-118: CONTROL AND MINIMIZATION OF ANODE FALL IN A QUASI-STEADY NOZZLE-BASED COAXIAL PLASMA THRUSTER; J. T. Scheuer, R. P. Hoyt, K. F. Schoenberg, R. A. Gerwin, R. W. Moses, and I. Henins, Los Alamos National Laboratory, Los Alamos, NM; R. M. Mayo and D. C. Black, North Carolina State University, Raleigh, NC

1993-119: DEVELOPMENT OF A SUPERCONDUCTING ELECTROMAGNET FOR APPLIED FIELD ARCJET THRUSTERS; F. Scortecci and G. Capecchi, CENTROSPAZIO, Pisa, Italy; M. Andrenucci, University of Pisa, Pisa, Italy; G. Mei and R. Garre, EUROPA METALLI-LMI, Fornaci di Barga, Lucca, Italy

1993-120: ROLE OF ANODE THROAT IN MPD ARCJET; I. Funaki, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1993-122: EXPERIMENTAL COMPARISON OF STEADY STATE NOZZLE TYPE AND CYLINDRICAL MPD THRUSTERS AT HIGH CURRENT LEVELS; Thomas Wegmann, Monika Auweter-Kurtz, Harald Habiger, Helmut L. Kurtz, and Herbert O. Schrade, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, FRG

1993-123: OPTICAL DIAGNOSTICS OF HIGH CURRENT PULSED ARC IN HIGH DENSITY GAS; A. M. Voronov and V. N. Zhuraviev, IPE RAS, 18 Dvortsovaya nab., St. Petersburg, 191065, Russia

1993-124: ELECTROSTATIC PROBES FOR THE INVESTIGATION OF ARC-DRIVEN ELECTRIC PROPULSION DEVICES; H. A. Habiger, M. Auweter-Kurtz, and H. Kurtz, UniversitÃ¤t Stuttgart, Stuttgart, Germany

1993-125: MICROINSTABILITES IN HIGH POWER MPD SYSTEMS: PRELIMINARY DIAGNOSTICS, Erik C. Bowman and Dennis L. Tilley

1993-126: CHAMBER EFFECTS ON PLUME EXPANSION FOR A LOW-POWER HYDROGEN ARCJET; Iain D. Boyd, Cornell University, Ithaca, NY 14853; Doug R. Beattie and Mark A. Cappelli, Stanford University, Stanford, CA 94305

1993-127: LASER-INDUCED FLUORESCENCE MEASUREMENTS ON THE PLUME FROM A 1 kW ARCJET OPERATED ON SIMULATED AMMONIA; W. M. Ruyten, University of Tennessee-Calspan, Center for Space Transportation and Applied Research, Tullahoma, Tennessee, 37388-8897; D. Burtner and D. Keefer, Center for Laser Applications; University of Tennessee Space Institute, Tullahoma, Tennessee, 37388-8897

1993-128: TIME RESOLVED MEASUREMENTS OF 1 kW ARCJET PLUMES USING CURRENT MODULATION VELOCIMETRY AND TRIPLE LANGMUIR PROBES; Jeffrey A. Pobst, John H. Schilling, and Daniel A. Erwin, University of Southern California, Department of Aerospace Engineering, Los Angeles, California 90089-1191; Ronald A. Spores, OL-AC Phillips Laboratory, Edwards Air Force Base, California 93524

1993-129: VIBRATIONAL NON-EQUILIBRIUM IN ARCJET FLOWS; V. Babu, S. Aithal, and V. V. Subramaniam, Department of Mechancial Engineering, The Ohio State University, Columbus, Ohio 43210

1993-130: THE USE OF PULSED ELECTRON BEAM FLUORESCENCE FOR ARCJET PLUME DIAGNOSTICS; John H. Schilling, Jeffrey A. Pobst, and Daniel A. Erwin, University of Southern California, Department of Aerospace Engineering, Los Angeles, CA 90089-1191

1993-131: LIF MEASUREMENTS OF SPECIIES VELOCITIES IN AN ARCJET PLUME; John G. Liebeskind, Ronald K. Hanson, and Mark A. Cappelli, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford University, Stanford, CA 94305

1993-132: ARCJET PLUME STUDIES USING MOLECULAR BEAM MASS SPECTROMETRY; James E. Polland, The Aerospace Corporation, Mechanics & Materials Technology Center, P.O. Box 92937-M5/754, Los Angeles, CA 90009

1993-133: OPTICAL MEASUREMENT AND NUMERICAL ANALYSIS OF MEDIUM-POWER ARCJET NON-EQUILIBRIUM FLOWFIELDS; H. Tahara, N. Uda, K. Onoe, Y. Tsubakishita, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1993-134: EMISSION SPECTROSCOPY OF 1 kWe ARCJET OPERATING WITH SIMULATED HYDRAZINE; E. Tosti and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy

1993-135: EFFECTS OF NOZZLE GEOMETRY ON PLUME EXPANSION FOR SMALL THRUSTERS; Donna Zelesnik, Ohio Aerospace Institute, Brook Park, Ohio; Paul F. Penko, NASA Lewis Research Center, Cleveland, Ohio; and Iain D. Boyd, Cornell University, Ithaca, New York

1993-136: INVESTIGATION OF A VERY LOW POWER PULSED ARCJET; Gary F. Willmes and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1993-137: NUMERICAL MODELLING OF RAREFIELD PLASMA PLUME IN NEUTRAL ENVIRONMENT GAS; A. M. Bishaev, V. K. Kalashnikov, and V. Kim, Research Institute of Applied Mechanics and Electrodynamics, Moscow, Russia

1993-138: PLASMA EXPANSION IN A LOW-POWER MPD THRUSTER WITH VARIABLE MAGNETIC NOZZLE; T. M. York and H. Kamhawi, The Ohio State University, Columbus, Ohio 43210

1993-141: MPD THRUSTER PLUME DIAGNOSTICS; M. Andrenucci, University of Pisa, Pisa, Italy; F. Paganucci and A. Turco, CENTROSPAZIO, Pisa, Italy

1993-142: MODELLING OF ION THRUSTER PLUME CONTAMINATION; R. I. Samanta Roy and D. E. Hastings, Space Power and Propulsion Laboratory, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139; N. A. Gatsonis, Applied Physics Laboratory, The Johns Hopkins University, Laurel, Maryland 20723

1993-143: OPTIONS AND TRADEOFFS FOR A SPACEBORNE ARCJET DIAGNOSTIC PACKAGE; S. Ferrari and E. Detoma, FIAT CIEI, SEPA, Corso Giulio Cesare, 300 – 10154 Tornino To (Italy); W. Deininger and E. Tosti, BPD Difesa e Spazio, Corso Garibaldi, 22 – 00034, Colleferro Roma (Italy); F. Scortecci and G. Capecchi, CONSORZIO PISA RICERCHI, CENTROSPAZIO, Via A. Gherardesca, 5-56014, Ospedaletto Pisa (Italy); J. J. Scialdone, NASA – Goddard Space Flight Center, Greenbelt, Maryland 20771 (U.S.A.)

1993-144: RADIO WAVE REFRACTION IN EXHAUST PLASMA PLUMES; F. F. Gabdullin, V. I. Garkusha, A. G. Korsun, and E. M. Tverdokhlebova, Central Research Institute of Machine-Building, Kaliningrad, Moscow Region, Russia

1993-145: RADIO WAVE REFRACTION IN EXHAUST PLASMA PLUMES; F. F. Gabdullin, V. I. Garkusha, A. G. Korsun, and E. M. Tverdokhlebova, Central Research Institute of Machine-Building, Kaliningrad, Moscow Region, Russia

1993-147: ELECTROMAGNETIC INTERFERANCE OF STATIONARY PLASMA THRUSTER; V. I. Brukhty, Scientific-Research Institute of Thermal Processes, Moscow, Russia; K. P. Kirdyashev, Institute of Radioengineering and Electronics, Russian Academy of Sciences, Fryazino, Moscow Region, Russia

1993-148: EXPERIMENTAL AND ANALYTICAL EVALUATION OF ELECTROMAGNETIC RADIATED EMISSIONS FROM ELECTRIC PROPOLUSION SYSTESM; K. P. Kidyashev, Russian Academy of Sciences, Institute of Radioengineering and Electronics, Fryasino, Moscow Region, Russia

1993-149: THE EFFECT OF ALKALI METAL ELECTRIC ROCKET ENGINES ON SPACECRAFT; V. I. Brukhty, V. N. Shutov, and A. B. Sminov, The Scientific-Research Institute of Thermal Processes, Moscow, Russia; M. P. Burgasov and A. A. Chirov, The Moscow Aviation Institute, Moscow, Russia

1993-150: A DOUBLE PENDULUM PRECISION THRUST MEASUREMENT BALANCE; T. F. Yang, Ping Liu, F. R. Chang-Diaz, Harvey Lander, R. A. Childs, H. D. Becker and S. A. Fairfax, MIT Plasma Fusion Center, Cambridge, MA 02139

1993-151: A LARGE HIGH VACUUM, HIGH PUMPING SPEED SPACE SIMULATION CHAMBER FOR ELECTRIC PROPULSION; Stanley P. Grisnik, NASA Lewis Research Center, Brookpark, OH; James E. Parkes, Sverdrup Technology, Inc., Brookpark, OH

1993-154: ION BEAM MODELING IN FEEP THRUSTERS; M. Andrenucci, University of Pisa, Pisa 56100, Italy; A. Ciucci and S. Marcuccio, CENTROSPAZIO, Pisa 56014, Italy

1993-155: EXPERIMENTAL PERFORMANCE OF CONTINUOUS AND PULSED FEEP THRUSTERS; S. Marcuccio and A. Genovese, CENTROSPAZIO, Pisa 56014, Italy; M. Andrenucci, University of Pisa, Pisa 56100, Italy

1993-156: FIELD EMISSION ELECTRIC PROPULSION (FEEP) SYSTEM STUDY; S. Marcuccio and A. Genovese, CENTROSPAZIO, Pisa 56104, Italy; M. Andrenucci, University of Pisa, Pisa 56100, Italy; C. Bartoli, J. Gonzalez, and G. Saccoccia, ESA/ESTEC, Noordwijk, The Netherlands

1993-157: FIELD EMISSION ELECTRIC PROPULSION: EXPERIMENTAL INVESTIGATIONS ON MICROTHRUST FEEP THRUSTERS; J. Gonzalez, G. Saccoccia, and H. von Rohden, ESA/ESTEC, Noordwijk, The Netherlands

1993-158: PROSPECTS OF MICROSTRUCTRED LIQUID METAL ION SOURCES (MILMIS) FOR FIELD EMISSION ELECTRIC PROPULSION (FEEP); J. Mitterauer, Technische UniversitÃ¤t Wien, Institut fÃ¼r Allgemeine Elektrotechnik und Elektronik, Gusshausstrasse 27-29, 1040 Wien, Austria

1993-159: EXPERIMENTAL ANALYSIS OF A COAXIAL SOLID-PROPELLANT MPD THRUSTER WITH SEGMENTED ANODES; G. Paccani, Universita’ di Roma “La Sapienza, Rome, Italy

1993-160: DEVELOPMENT AND LABORATORY TEST OF EROSION PULSED PLASMA THRUSTER, DESIGNED FOR THE ATTITUDE CONTROL OF A GEOSTATIONARY SATELLITE; N. N. Antropov, G. A. Popov, A. I. Rudikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, Russia

1993-165: SEMI-EMPIRICAL INTERIOR BALLISTICS SIMULATION MODEL OF ARC HEATED LIGHT GAS GUN; A. M. Glukhov, IPERAS, 18 Dvortsovaya, St. Petersburg, 191065, Russia

1993-166: USE OF HYDROGEN ARCJET THRUSTERS FOR DIAMOND SYNTHESIS; Mark A. Cappelli, Michaela H. Loh, and John G. Liebeskind, High Temperature Gasdynamics Laboratory, Stanford University, Department of Mechanical Engineering, Stanford, CA 94305-3032

1993-167: ATOMIC OXYGEN SIMULATION USING MPD THRUSTER TECHNOLOGY; S. B. Gabriel, N. J. Wood, G. T. Roberts, and A. R. L. Tatnall, Dept. of Aeronautics and Astronautics, University of Southampton, Southampton, Hampshire, UK

1993-168: APPLICATIONS OF QUASI-STEADY MPD ACRJETS TO MATERIAL PROCESSINGS-CERAMIC COATINGS BY MEANS OF MPD SPRAY; H. Tahara, T. Tsubaki, Y. Kagaya, Y. Tsubakishita, and T. Yoshikawa, Osaka University, Osaka, Japan

1993-169: ION THRUSTER ENDURANCE TEST USING DEVELOPMENT MODEL THRUSTER FOR ETS-VI; S. Shimada, K. Satoh, Y. Gotoh, E. Nishida and T. Nora, Mitsubishi Electric Corporation, Japan; H. Takegahara, Tokyo Metropolitan Institute of Technology, Tokyo, Japan; H. Nagano and K. Nakamaru, National Space Development Agency of Japan

1993-170: 500 HOUR TESTS OF THE T5 ION THRUSTER WITH DUAL AND TRIPLE GRID EXTRACTION SYSTEMS; S. D. Watson, P. Hurford, A. R. Martin, C. R. Banks, R. W. Eaton, M. S. Harvey, W. E. F.L. Moulford, and A. J. Pearce, AEA Technology Space Applications, Culham Laboratory, Abingdon, Oxfordshire, OX14 3DB

1993-171: EROSION MEASUREMENTS FOR TWO AND THREE GRID ION THRUSTER EXTRACTION SYSTEMS; A. R. Martin, C. R. Banks, R. W. Eaton, P. Hurford, W. E. F. L. Moulford and A. J. Pearce, AEA Technology, Space Applications, F4 Culham, Abingdon, Oxon OX14 3DB, UK

1993-172: TEST TO FAILURE OF A TWO GRID 30cm dia ION ACCELERATOR SYSTEM; John R. Brophy, James E. Polk, and Lewis C. Pless; Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-173: CHARGE-EXCHANGE GRID EROSION STUDY FOR GROUND-BASED AND SPACE-BASED OPERATIONS OF ION THRUSTERS; Xiaohang Peng, Wilhelmus M. Ruyten, and Dennis Keefer, University of Tennessee-Calspan Center for Space Transportation and Applied Research, Tullahoma, Tennessee 37388

1993-174: EFFECTS OF DESIGN AND OPERATING CONDITIONS ON ACCELERATOR-GRID IMPINGEMENT CURRENT; Jeff M. Monheiser and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1993-175: EROSION CHARACTERISTICS OF TWO-GRID ION ACCELERATING SYSTEMS; V. Rawlin, NASA Lewis, Cleveland, OH

1993-176: PROBABILISTIC ANALYSIS OF ION ENGINE ACCELERATOR GRID LIFE; J. E. Polk, N. R. Moore, L. E. Newlin, J. R. Brophy, and D. H. Ebbeler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1993-177: ION THRUSTER LIFETIME LIMITATIONS IMPOSED BY SPUTTERING PROCESSES; D. G. Fearn, Defence Research Agency, Farnborough, UK

1993-178: PARTICLE SIMULATION OF GRID EROSION FOR A THREE GRID ION THRUSTER; Quan Zhang, ERC, Inc., Tullahoma, Tennessee 37388; Xiaohang Peng and Dennis Keefer, University of Tennessee-Calspan Center for Space Transportation and Applied Research, University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1993-179: EXTRACTION SYSTEM DESIGN AND MODELLING USING COMPUTER CODES; R. A. Bond and P. M. Latham, AEA Technology, Space Applications, Culham Laboratory, Abingdon, Oxon OX14 3DB, UK

1993-181: NUMERICAL SIMULATION OF THE PERFORMANCE OF A RADIATION-COOLED 1KW DC ARCJET THRUSTER; Hiroyuki Okamota and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812, Japan; Ken-ichi Tanaka, Central Research Laboratory, Mitsubishi Electric Corporation, Amagasaki, Hyogo 661, Japan; and Alfred Beylich, Stosswellenlabor, Rheinisch-WestfÃ¤lische Technische Hochschule Aachen, 5100 Aachen, Germany

1993-182: DEVELOPMENT OF A NUMERICAL MODEL OF THE NOZZLE FLOW IN LOW POWER ARCJET THRUSTERS; A. Ciucci, Centrospazio, Pisa, Italy; L. d’Agostino and M. Andrenucci, University of Pisa, Pisa, Italy

1993-183: ON THE EFFECTS OF SWIRL IN ARCJET THRUSTER FLOWS; V. Babu, S. Aithal, and V. V. Subramaniam, Department of Mechanical Engineering, The Ohio State University, Columbus, Ohio 43210

1993-184: BEHAVIOR OF ARC COLUMN IN ARCJET CONSTRICTOR; Tetsuya Yamada, Kyoichiro Toki, and Kyoichi Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1993-185: ANODE HEAT LOSS AND CURRENT DISTRIBUTION IN DC ARCJETS; K. Fujita and Y. Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Tokyo, Japan

1993-186: EFFECT OF A PULSED MAGNETIC FIELD ON ARCJET OPERATION; Nicholas T. Tiliakos and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1993-187: PERFORMANCE CALCULATION OF ARCJET THRUSTERS – THE THREE CHANNEL MODEL; B. Glocker, H. O. Schrade, and M. Auweter-Kurtz; Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart

1993-189: THEORETICAL MODELING OF MAGNETOPLASMADYNAMIC ARCJETS; Pavlos G. Mikellides and Peter J. Turchi, Ohio State University, Columbus, OH; and Norman F. Roderick, University of New Mexico, Albuquerque, NM

1993-190: THRUST PRODUCTION THEORY OF ELECTROMAGNET/THERMAL HYBRID ARCJETS; A. Sasoh, Tohoku University, Sendai, Japan

1993-191: CALCULATION OF A NOZZLE TYPE MPD THRUSTER AND COMPARISON WITH MEASUREMENTS; P. C. Sleziona, M. Auweter-Kurtz, C. Boise, H. L. Kurtz, H. O. Schrade, and T. Wegmann, Institut fÃ¼r Raumfahrtsysteme UniversitÃ¤t Stuttgart, FRG

1993-194: MECHANISMA OF ANODE POWER DEPOSITION IN A LOW PRESSURE FREE BURING ARC; George C. Soulas, Ohio State University, Columbus, Ohio 43210; and Roger M. Myers, Sverdrup Technology, Inc. NASA Lewis Research Center Group, Brook Park, Ohio 44142

1993-196: AN EXPERIMENTAL STUDY OF LITHIUM DISPENSER CATHODES IN THE MPD THRUSTER; J. S. Fillmore, W. F. von Jaskowsky, A. J. Kelly, and R. G. Jahn, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ 08544, USA

1993-197: DIAGNOSTIC EXPERIMENT AND NUMERICAL ANALYSIS OF ONE-DIMENSIONAL MPD FLOWFIELDS; H. Tahara, T. Tsubaki, Y. Kagaya, Y. Tsubakishita, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1993-198: DEVELOPMENT OF ION THRUSTER SYSTEM FOR INTERPLANETARY MISSIONS; Hitoshi Kuninaka, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa, Japan; Nobuo Hiroe, Kazuto Kitaoka, and Yoshio Ishikawa, Nihon University, Narashinodai, Funabashi, Chiba, Japan; Kazutaka Nishiyama, University of Tokyo, Hongo Bunkyo, Tokyo, Japan; and Yasuo Horiuchi, NEC, Ikebe, Midori, Yokohama, Kanagawa, Japan

1993-200: A MISSION TO PLUTO USING NUCLEAR ELECTRIC PROPULSION; D. G. Feam, Defence Research Agency, Farnborough

1993-202: MISSION FACTORS AFFECTING COST OPTIMIZATION OF SOLAR ELECTRIC ORBITAL TRANSFER VEHICLES; Todd M. Miller and G. Brian Seaworth, McDonnell Douglas Aerospace, Huntington Beach, California

1993-203: OPERATIONAL REQUIREMENTS FOR COST EFFECTIVE PAYLOAD DELIVERY WITH SOLAR ELECTRIC PROPULSION; K. P. Zondervan and A. K. Chan, The Aerospace Corporation, P. O. Box 92957, M4/943, Los Angeles, CA 90009-2957; C. A. Feuchter, Office of Aerospace Studies, 3550 Aberdeen Ave SE, Kirtland AFB, Albuquerque, NM 87117-5776; and W. B. Smith, Space and Missile Systems Center, Los Angeles AFB, P. O. Box 92960, Los Angeles, CA 90009-2960

1993-204: CENTAUR-DERIVED PROPELLANT SUPPLY SYSTEM FOR A SOLAR ELECTRIC ORBIT TRANSFER VEHICLE; J. R. Schuster, J. R. LeMay, E. P. Morss, and G. E. Williams, General Dynamics Space Systems Division, San Diego, California

1993-205: HIGH ALTITUDE ORBIT RAISING WITH ON-BOARD ELECTRIC POWER; B. Free, Scionics, Inc.

1993-206: EFFECT OF VOLUME CONSIDERATIONS ON THE DESIGN OF AN ELECTRIC ORBITAL TRANSFER VEHICLE; G. Brian Seaworth and Todd M. Miller, McDonnell Douglas Aerospace, Space Systems, Huntington Beach, California

1993-207: THE EFFECT OF SOLAR ARRAY DEGRADATION IN ORBIT-RAISING WITH ELECTRIC PROPULSION; A. M. Fitzgerald, Orbital Sciences Corporation, Space Data Division, Chandler, AZ

1993-208: LOW POWER GROUND BASED LASER ILLUMINATION FOR ELECTRIC PROPULSION APPLICATIONS; M. LaPointe and S. Oleson, Sverdrup Technology, Inc., Brookpark, OH

1993-209: LIQUID SPACE OPTICAL THEORY OF MANNED STARFLIGHT WITH EARTHLY APPLICATIONS; J. H. Bloomer, Discraft Corp., Portland, OR, U.S.A.

1993-210: HIGH SPECIFIC IMPULSE EXPERIMENTS WITH 1.5 AND 5KW THERMAL ARCJETS; M. Riehle, H. L. Kurtz, and M. Auweter-Kurtz, IRS - Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1993-211: PERFORMANCE OF ADVANCED CONCEPT HYDROGEN ARCJET ANODES; G. W. Butler, R. J. Cassady, W. A. Hoskins, D. Q. King, and A. E. Kull, Rocket Research Company, Redmond, Washington

1993-213: PARAMETRIC TEST RESULTS OF A LOW POWER ARCJET; G. Capecchi, F. Scortecci, F. Repola, and M. Andrenucci, Centrospazio, Pisa 56104, Italy

1993-214: COMPARISON OF EXPERIMENTAL AND NUMERICAL RESULTS FOR RADIATION COOLED AND WATER COOLED HYDROGEN ARCJETS; Trevor M. Moeller, Dennis Keefer, and Robert P. Rhodes, Center for Laser Applications, The University of Tennessee Space Institute, Tullahoma, TN 37388-8897

1993-215: HYDROGEN ARCJET TECHNOLOGY STATUS; Francis M. Curran, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135; and Leonard H. Caveny, Ballistic Missile Defense Organization, Innovative Science and Technology, Washington, DC 20301-7100

1993-216: MEASUREMENT OF ENERGY DEPOSISTION MODES IN AN INTERMEDIATE POWER HYDROGEN ARCJET; W. A. Hoskins, A. E. Kull, W. M. Nesser, and G. W. Butler, Rocket Research Company, Redmond, WA 98073

1993-217: NON-EQUILIBRIUM MODELING OF HYDROGEN ARCJET THRUSTERS; Robert Rhodes and Dennis Keefer University of Tennessee Space Institute, Center for Laser Applications; Tullahoma, TN 37388-8897

1993-218: NONEQUILIBRIUM NUMERICAL SIMULATION OF RADIATION-COOLED ARCJET THRUSTERS; S. A. Miller and M. Martinez-Sanchez, Space Power and Propulsion Laboratory, Dept. of Aeronautics and Astronautics, MIT, Cambridge, MA 02139

1993-219: AXIAL EMISSION DIAGNOSTICS OF A LOW POWER HYDROGEN ARCJET THRUSTER; P. Victor Storm and Mark A. Cappelli, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford University, Stanford, California, USA

1993-220: A DIRECT COMPARISON OF HYDROGEN ARCJET THRUSTER PROPERTIES TO MODEL PREDICTIONS; M. A. Cappelli, J. G. Liebeskind, and R. K. Hanson, High Temperature Gasdynamics Laboratory, Department of Mechanical Engineering, Stanford University, Stanford, California; G. W. Butler and D. Q. King, Olin Rocket Research Company, Redmond, Washington

1993-221: DEVELOPMENT AND TESTING OF A 100 KW RADIATION COOLED THERMAL HYDROGEN ARCJET THRUSTER; Thomas M. GÃ¶lz, Monika Auweter-Kurtz, and Helmut L. Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Federal Republic of Germany

1993-222: DEVELOPMENT AND INVESTIGATION OF CHARACTERISTICS OF INCREASED POWER SPT MODELS; B. A. Arkhipov, N. A. Maslennikov, and V. M. Murashko, Design Buro “Fakel,” Kaliningrad (obl), Russia; A. N. Veselovzorov, A. I. Morozov, and I. B. Pokrovski, I. V. Kurchalov’s Research Institute of Atomic Energy, Moscow, Russia; V. M. Gavryushin and S. A. Khartov, Moscow Aviation Institute (MAI), Moscow, Russia; V. Kim and V. I. Kozlov, Research Institute of Applied Mechanics and Electrodynamics of MAI, Moscow, Russia

1993-223: DEVELOPMENT STATUS OF THE SPT MK II THRUSTER; D. Valentian, SEP, GPPE, Melun Villaroche, France; A. Bugrova, Mirea, Moscow, Russia; and A. Morozov, Institute of Atomic Energy, Moscow, Russia

1993-225: DEVELOPMENT OF A 4 KW HALL-TYPE ELECTRIC THRUSTER; A. S. Koroteev, V. A. Petrosov, V. I. Baranov, and A. I. Vasin, The Scientific-Research Institute of Thermal Processes, Moscow, Russia; J. R. Wetch, and S. P. Wong, International Scientific Products, San Jose, CA, USA

1993-226: THEORETICAL AND EXPERIMENTAL ANALYSIS OF STATIONARY PLASMA THRUSTER OPERATION; D. Valentian and J. P. Bugeat, SEP, GPPE, Melun Villaroche, France; R. Tchuyan, S. Khartov, L. Latyshev, and V. Sierovaiskiy, Moscow Aviation Institute, Moscow, Russia; G. Cirri, Proel, Florance, Italy

1993-228: ANODE LAYER THRUSTERS, STATE OF THE ART AND PERSPECTIVES; V. I. Garkusha, E. A. Lyapin, A. V. Semyenkin, and S. O. Tverdokhlebov, Central Research Institute of Machine Building, Kaliningrad (Moscow Region), Russia

1993-230: TWO-DIMENSIONAL NUMERICAL MODEL OF PLASMA FLOW IN A HALL THRUSTER; Kimiya Komurasaki, Nagoya University, Chikusa-ku, Nagoya 464-01, Japan; and Yoshihiro Arakawa, University of Tokyo, Bunkyo-ku, Tokyo 113, Japan

1993-231: INVESTIGATION OF EROSION IN ANODE LAYER THRUSTER AND ELABORATION HIGH LIFE DESIGN SCHEME; A. V. Semenkin, Central Research Institute of Machine Building, Kaliningrad (Moscow Region), Russia

1993-232: STUDY OF DOUBLE-STAGE ANODE LAYER THRUSTER USING INERT GASES; Sergey O. Tverdokhlebov, Central Research Institute of Machine Building Kaliningrad (Moscow Region), Russia

1993-233: ON USE OF ALKALI METALS AS SPT PROPELLANTS; V. A. Petrosov, V. I. Baranov, A. I. Vasin, and Yu S. Nazarenko, The Scientific-Research Institute of Thermal Processes, Moscow, Russia

1993-234: MEASUREMENTS OF THE ELECTROMAGNETIC EMISSIONS FROM THE T5 ION THRUSTER; S. Chanda and F. Mawdsley, ERA Technology Ltd., Leatherhead, UK; R. D. Brown, Matra Marconi Space UK Ltd., Portsmouth, UK; S. D. Watson, AEA Technology, Culham Laboratory, Abingdon, UK; A. K. Malik, Imperial College, London, UK; and D. G. Feam, Defence Research Agency, Farnborough, Hampshire, UK

1993-235: BEAM CHARACTERISTICS EVALUATION OF ETS-VI XENON ION THRUSTER; Haruki Takegahara and Yukikazu Kasai, Tokyo Metropolitan Institute of Technology; Yoshifumi Gotoh, Mitsubishi Electric Corporation; Katsuhiro Miyazaki, Yukio Hayakawa, and Shoji Kitamura, National Aerospace Laboratory; Hiroshi Nagano and Kunio Nakamaru, National Space Development Agency of Japan

1993-236: ELECTRIC PROBE MEASUREMENTS IN THE PLUME OF THE UK-10 ION THRUSTER; P.C.T. de Boer, The Aerospace Corporation, P. O. Box 92957, Los Angeles, CA 90009-2957

1993-237: MICROWAVE DIAGNOSTICS FOR ION ENGINES: S. W. Janson, Technology Operations, Mechanics and Materials Technology Center, The Aerospace Corporation, Los Angeles, California

1993-239: THE EFFECT OF PROPELLANT SELECTION ON THE PERFORMANCE OF SPACE MISSIONS USING THE UK-25 INERT GAS ION THRUSTER; C. H. Edwards and S. B. Gabriel, Dept. Aeronautics and Astronautics, University of Southampton, Southampton, Hampshire, S09 5NH, UK

1993-242: PLASMA PARTICLE SIMULATION IN CUSPED ION THRUSTERS; Miharu Hirakawa and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Tokyo, Japan

1993-243: PLASMA PROPERTIES AND IGNITION CHARACTERISTICS OF RF ION SOURCE; Haruki Takegahara, Takeshi Ohyama, Kosuke Iwakura, and Toshiaki Iwata, Department of Aerospace Engineering, Faculty of Engineering, Tokyo Metropolitan Institute of Technology, Hino, Asahigaoka 6-6, Tokyo, 191, Japan

1993-244: HIGH SPEED ION SOURCE FOR SPACE EXPERIMENT APPLICATION; V. G. Grigorian, S. A. Kalitin, V. A. Obukhov, and M. M. Shalamov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow Aviation Institute, Russia, 125871, Moscow, Volokolamskoe shosse, 4

1993-246: PLASMA CONTRACTOR DEVELOPMENT FOR SPACE STATION; M. J. Patterson, J. A. Hamley, and C. Sarmiento, NASA Lewis, Cleveland, OH; D. Manzella, T. Sarver-Verhey and G. Soulas, Sverdrup Technology, Brookpark, OH; A. Nelson, Purdue University, West Lafayette, IN

1993-247: MAIN FEATURES OF PHYSICAL PROCESSES IN STATIONARY PLASMA THRUSTERS; A. I. Bugrova, A. V. Desiatskov, V. K. Kharchevnikov, and A. I. Morozov, MIREA, Moscow, Russia

1993-249: NUMERICAL SIMULATIONS OF HYDROGEN ARCJET PERFORMANCE; G. W. Butler, A. E. Kull, and D. Q. King, Rocket Research Company, Redmond, Washington

1993-250: POWER CONSOLE DEVELOPMENT FOR NASA’S ELECTRIC PROPULSION OUTREACH PROGRAM; Luis R. Pinero, Michael J. Patterson, and Vincent E. Satterwhite, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1993-251: OPERATION OF A BRASSBOARD PCU WITH A LOW POWER ARCJET; R. Di Stefano and W. D. Deininger, BPD Difesa e Spazio, Colleferro, Italy; G. Parisi and E. Detoma, FIAT CIEI – SEPA, Torino, Italy

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IEPC1993-Index

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1995 INDEX

1995-01: ELECTRIC PROPULSION DEVELOPMENT AND APPLICATION IN THE UNITED STATES; R. Rhoads Stephenson, JPL California Institute of Technology, USA

1995-02: REVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Shoji Kitamura, National Aerospace Labortory, Japan

1995-04: ADVANCED INTERPLANETARY MISSION OF THE XXI CENTURY USING ELECTRIC PROPULSION; H. Loeb, Institute of Physics, Giessen University, Germany; G. Popov, Research Institute of Applied Mechanics and Electrodynamics, Russia

1995-05: ELECTRIC PROPULSION THRUSTERS AND PLASMODYNAMICS; Alexei Morozov, RSC, Kurchatov Institute, Russia

1995:06: SPT IN RUSSIA – NEW ACHIEVEMENTS; A. S. Bober and N. A. Maslennikov, EDB “Fakel” Kaliningrad, Russia

1995-07: MAI INVESTIGATIONS AND DEVELOPMENT IN THE ERT FIELD; M. P. Burgasov and L. A. Latyshev, MAI, Russia; V. P. Kim, G. A. Popov, and V. B. Tikhonov, RIAME MAI, Russia

1995-08: NIITP’S ACTIVITY IN THE FIELD OF ELECTRIC PROPULSION; A. S. Koroteev and V. A. Petrosov, NIITP, Russia

1995-09: ELECTRIC PROPULSION ACTIVITY IN TSNIMASH; T. I. Garkusha, A. V. Semenkin, and S. G. Mironov, TsNIIMASH, Russia; V. V. Savitsev, and D. Grishin, Moscow State Technology University, Russia

1995-010: VNIIEM ACTIVITY IN THE FIELD OF EPE; Yu. V. Trifonov and V. P. Khodnenko, NPP VNIIEM, Russia; R. S. Salikhov, G. A. Avatinyan, and Yu P. Rylov, NIIEM (Instra. Moscow Region), Russia

1995-011: EXPERIENCE OF FLIGHT OPERATION OF ELECTRIC PROPULSION SUBSYSTEMS WITH STATIONARY PLASMA THRUSTERS ON SPACECRAFTS DEVELOPED BY NPO PM; A. G. Kozlov, V. F. Petrusevitch, V. A. Rayevsky, A. V. Romashko, and Y. M. Yermoshkin, NPO PM (Krasnoyarsk), Russia

1995-012: THE REVIEW OF THE WORKS ON ELECTRICAL PROPULSION THRUSTERS DEVELOPMENT AND INVESTIGATION. CARRIED OUT AT THE DNEPROPETROVSK STATE UNIVERSITY; V. F. Prysniakov, A. N. Petrenko, A. M. Kapulkin, I. N. Statsenko, A. I. Kondratiev, and S. N. Kulagin

1995-014: HIGH POWER ARCJET EXPERIMENTS AND ANALYSIS; Thomas M. GÃ¶lz, Monika Auweter-Kurtz, Helmut L. Kurtz, and P. Christian Sleziona, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart FRG

1995-015: INVESTIGATION OF ELECTRON ENERGY DISTRIBUTIONS IN AN MPG ARCJET FLOW WITH ELECTROSTATIC PROBES; Harald A. Habiger, Monika Auweter-Kurtz, and Helmut Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

1995-016: PLASMA FEATURES IN A MEDIUM-POWER ARCJET; Hirokazu Tahara, Kazuhito Komiko, Lulu Zhang, Ken-Ichi Onoe, and Takao Yoshikawa, Osaka University, Japan

1995-017: DEVELOPMENT AND TESTING OF A 300W-CLASS ARCJET; Kazuhiko Ogiwara and Satoshi Hosoda, Tokai University, Japan; Takao Suzuki, Stanford University, Japan; Kyoichiro Toki and Kyoichi Kuriki, Institute of Space and Astronautics Sci., Japan; Shinobu Matsuo, Mitsubishi Heavy, Ind. LTD, Japan; Hideaki Nanri, and Hiroshi Nagano, National Space Develop. Agency of Japan

1995-018: LOW POWER ARCJET PERFORMANCE EVALUATION; Keith A. McFall, Dennis L. Tilley, and Frank S. Gulczinski III, Phillips Laboratory, Edwards AFB, CA 93524

1995-020: NUMERICAL AND EXPERIMENTAL STUDIES OF HYDROGEN AND NITROGEN FLOWS IN RESISTOJET; Iain D. Boyd and Douglas B. VanGilder, School of Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY, USA; Edward j. Beiting and Ronald B. Cohen, Aerospace Corporation, Los Angeles, CA, USA; Eric J. Pencil, NASA Lewis Research Center, Cleveland, OH, USA; and Steven D. Hirsch, Worcester Polytechnic Institute, Worcester, MA, USA

1995-022: SIMPLE ESTIMATION OF THE PERFORMANCE OF A LOW POWER ARCJET THRUSTER; Michio Nishida and Hiroyuki Okamoto, Kyushu University, Japan

1995-024: SEMIEMPIRICAL PREDICTION TECHNIQUE OF PERFORMANCE PARAMETERS FOR ARCJET PLASMA GENERATOR; E. P. Vaulin, E. A. Baranova, and J. V. Demonenko, Moscow Aviation Institute, Russia; V. A. Obukhov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, Russia; F. Scortecci, Centrospazio, Pisa, Italy

1995-025: NUMERICAL PREDICTION OF ARCJET PERFORMANCE BASED ON THE CHEMICAL KINETICS AND ELECTRON TEMPERATURE DISPARITY; Kazuhisa Fujita and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Hongo 7-3-1, Tokyo, 113 Japan

1995-026: NUMERICAL ANALYSIS OF NONEQUILIBRIUM PLUME OF AN ARCJET THRUSTER; N. Nishida, y. Yamamoto, Kyushu University, Japan; M. Matsumoto, Res. Inst. Ishikawajima-Harima Heavy Ind. Co. Ltd., Japan

1995-028: LASER INDUCED FLUORESCENCE OF GROUND STATE HYDROGEN ATOMS IN AN ARCJET PLUME; Jeffrey A. Pobst, and Ingrid J. Wysong, Ronald A. Spores, Propulsion Directorate, OL-AC Phillips Laboratory, Edwards AFB, CA 93524

1995-029: STUDY AND DIAGNOSTICS OF THE EFFECT OF LENGTH VARIATION IN HALL THRUSTERS; J. Ashkenazy, Y. Raitses, and G. Appelbaum, SOREQ NRC, Israel; and M. Guelman, Tech. I.I.T., Israel

1995-030: PERFORMANCE EVALUATION OF A 4.5 KW SPT THRUSTER; John M. Sankovic and Thomas W. Haag,NASA Lewis R. C. USA; and David H. Manzella, NYMA Inc. USA

1995-031: INVESTIGATION 4.5 KW HIGH EFFICIENCY HALL-TYPE T-160 ELECTRIC THRUSTER; V. A. Petrosov, A. I. Vasin, and V. I. Baranov, NIITP, Russia; J. R. Wetch, E. J. Britt, S. P. Wong, and R. Lin, Inter. Sci. Product, USA

1995-032: INVESTIGATION OF SMALL, CLOSED ELECTRON DRIFT, SPT.; G. Guerrini and M. Bacal, Ecole Polytechnique, France; A. N. Vesselovzorov, RSC “Kurchatov. Inst. “, Russia

1995-033: OPTIMIZATION OF CHANNEL CONFIGURATION OF HALL THRUSTERS; Kenji Mikami, Kimiya Komurasaki, and Toshi Fujiwara, Nagoya Unv., Japan

1995-034: SIMPLIFIED NUMERICAL DESCRIPTION OF SPT OPERATION; David H. Manzella, NYMA Inc. USA

1995-035: DEVELOPMENT OF A SECOND GENERATION OF SPT; J. P. Bugeat and C. Koppel, SEP, France

1995-036: PRESENT AND NEAR FUTURE APPLICATIONS OF SPT M-2 THRUSTERS; D. Valentian and C. Koppel, SEP, France

1995-037: DISSIPATIVE METHOD OF SUPPRESSION OF ELECTRON DRIFT INSTABILITY IN SPT; Aleksandr M. Kapulkin, and Valdimir F. Prisnyakov, Onepropetr. State Univ., Ukraine

1995-038: PHYSICAL AND TECHNICAL BASES OF THE MODERN SPT DEVELOPMENT; V. M. Gavryshin, MAI, Russia; V. Kim and V. I. Kozlov, RIAME MAI, Russia; and N. A. Maslennikov, EDB “Fakel”, Russia

1995-039: THE RESULTS OF 7000-HOUR SPT-100 LIFE TESTING; B. A. Arhipov, A. S. Bober, R. Y. Gnizdor, K. N. Kozubsky, A. I. Korakin, N. A. Maslennikov, and S. Y. Pridannikov, EDB “FAKEL”, Kaliningrad, Russia

1995-041: A 2000 HOURS LIFETIME TEST RESULTS OF 1.3 KW T-100 ELECTRIC THRUSTER; V. A. Petrosov, A. I. Vasin, and V. I. Baranov, NIITP MAI, Russia; J. R. Wetch, E. J. Britt, S. P. Wong, and R. Lin, Inter. Sci, Product, USA

1995-042: THE ELECTRON DYNAMICS IN SPT-CHANNEL AND THE PROBLEM OF ANOMALOUS EROSION; A. I. Morozov, RSC “Kurchatov Institute”, Russia; V. V. Savelyev, Inst. Appl. Mathem., Russia

1995-043: THE MECHANISM OF ANOMALOUS EROSION IN ACCELERATORS WITH CLOSED DRIFT OF ELECTRONS; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-044: NEW CONCEPTIONS OF OSCILLATION MECHANISMS IN THE ACCELERATOR WITH CLOSED DRIFT OF ELECTRONS; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashhnov, NIITP, Russia

1995-045: INVESTIGATION OF THE SPT PERFORMANCE IMPROVEMENT POSSIBLITITY; Vladimir Kim, Vitaly Egorov, Vyacheslav Kozlov, and Garry Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), Moscow, Russia; Theodor Colbert and Michael Day, Space Systems/Loral, Palo Alto, USA; Sergei Khartov, Moscow Aviation Institute, Moscow, Russia; Nicolay Maslennikov and Alexander Nesterenko, Design Bureau “Fakel”, Kalinningrad (obl.), Russia

1995-046: INFLUENCE OF VACUUM CONDITIONS ON THE SPT OPERATION; A. I. Bugrova, MIREA, Russia; A. I. Morozov, RSC “Kurchatov. Inst.”, Russia

1995-047: EXPERIMENTAL DETERMINIATION OF ION ENERGY AT THE OUTLET OF SPT-ATON; A. I. Bugrova, A. V. Desyatskov, and V. K. Kharchevnikov, MIREA, Russia

1995-048: THE POSSIBILITY OF NEARANODE PROCESS CONTROLLING FOR PERSPECTIVE SPT MODELS; A. Jakupov, S. Khartov and L. Latyshev, MAI, Russia

1995-050: ELECTRON-CURRENT GAIN IN DISCHARGE IN A TRANSVERSE MAGNETIC FIELD; A. V. Zharinov, V. I. Lenin All-Russian Electrotechnical Institute, Moscow, Russia

1995-051: EXPERIMENTAL STUDY OF EXHAUST BEAM OF ANODE LAYER THRUSTER; B. S. Borisov, K. K. Mikhaylov, A. V. Rusakov, A. V. Semenkin, and H. O. Chislov, Central Research Institute of Machine Building (TsNIIMASH), Kaliningrad, Moscow Region

1995-052: SOME RESULTS OF INVESTIGATION OF ANODE DESIGN INFLUENCE ON ANODE LAYER THRUSTER CHARACTERISTICS; Sergey N. Kulagin, Ivan N. Statsenko, Vladimir N. Serebryansky, Dnepropetr. State Univ., Ukraine; Alexandr N. Semenkin, TsMIIASH, Russia

1995-054: PROSPECTS FOR USING METALS AS PROPELLANT IN STATIONARY PLASMA ENGINES OF HALL-TYPE; V. G. Gnedenko and V. A. Petrosov, NIITP, Russia; A. V. Trofimov, RSC “Kurchatov Inst.”, Russia

1995-055: THE ENGINEERING METHOD OF THE SPT INTEGRAL PARAMETERS CALCULATIONS; A. Rudikov and V. Tikhonov, RIAME MAI, Russia

1995-056: ON PLASMA FLOW INSTABILILTY IN CDEA (FOR THE EXPERIMENT); E. B. Svirsky, RSC “Kurchatov Institute”, Russia

1995-057: STATIONARY PLASMA HALL THRUSTER LIFETIME PREDICTION; A. A. Kalyaev, V. A. Petrosov, and V. I. Baranov, NIITP, Russia

1995-058: DIFFUSION MODEL OF THE CONDUCTION IN THE IONIZATION ZONE OF THE CLOSED ELECTRON DRIFT ACCELERATOR; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-059: THE IONIZATION OSCILLATIONS MECHANISM IN ACD; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov; NIITP, Russia

1995-060: THE SPT CHANNEL EROSION MODEL; V. A. Petrosov, V. I. Baranov, A. I. Vasin, A. A. Kaliaev, and Y. S. Nazarenko; NIITP, Russia

1995-061: ELECTRON DISTRIBUTION FUNCTION IN ACCELERATOR WITH CLOSED ELECTRON DRIFT; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-062: ELECTRON DRIFT OSCILLATIONS OUTSIDE ACCELERATION ZONE OF ACCELERATOR WITH CLOSED ELECTRON DRIFT; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov; NIITP, Russia

1995-063: THERMOVISION STUDY OF TEMPERATURE FIELDS AND RADIATION CHARACTERISTICS OF ELECTRIC THRUSTER T0100 SURFACES; A. F. Anikin, S. M. Bednov, A. N. Golikov, and M. V. Yasinsky, NIITP, Russia

1995-064: OPTIMIZATION OF PLANS FOR ACCELERATED ENDURANCE TESTS FOR RELIABILITY; A. A. Kalyaev and V. G. Lebedev, NIITP, Russia

1995-065: STATIONARY PLASMA HALL THRUSTER ACCEPTANCE ACCELERATED TESTS; A. A. Kalyaev, NIITP, Russia

1995-066: INFLUENCE OF TARGET SPUTTERING ON THRUSTER PARAMETERS; A. I. Bugrova, A. S. Lipatov, and D. V. Churbanov, MIREA, Russia; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-067: SPT-ATON TESTS AT KURCHATOV INSTITUTE STANDS; A. I. Bugrova, A. C. Lipatov, V. K. Kharchevnikov, and D. V. Churbanov, MIREA, Russia; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-068: LIGHT SPECTRUM OF SPT-ATON PLASMA JET; J. A. Ermakov, M. V. Kozintzeva, and P. V. Kolenko, MIREA, Russia

1995-069: PROBE INVESTIGATIONS OF THE DISCHARGE RECONSTRUCTION AT THE DUSTING OF THE CHANNEL WORK SURFACES; A. I. Bugrova, A. V. Desyatskov, and V. K. Kharchevnikov, MIREA, Russia; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-070: CHEMICAL CHARACTERISTICS OF THE FILMS, APPEARED ON THE ANODE SURFACE OF SPT; A. I. Bugrova, A. S. Lipatov, Y. V. Titov, MIREA, Russia; D. Valentian, SEP, France

1995-071: THE INFLUENCE OF INPURITES ON SPT-ATON THRUSTER OPERATION; A. V. Desyatskov, M. V. Kozintzeva, and A. S. Lipatov, MIREA, Russia

1995-072: NEUTRAL DYNAMICS IN SPT CHANNEL; A. P. Ahubin, RSC “Kurchatov Institute”, Russia

1995-073: ELECTROMAGNETIC INTERFERENCE MEASUREMENTS WITHIN THE T-100 ENDURANCE TEST; V. I. Brukhty, NIITP, Russia; K. P. Kirdyashev, O. E. Svetlitskaya, Inst. Radioeng. and Electron. (Fryazino, Moscow Region), Russia

1995-074: OPTMIZATION OF THE PARAMETERS BY PROGRAM FOR (SSTC) OF EPS AND EPT; A. V. Rumiantsev, Kaliningrad State University, Russia

1995-075: LIFETIME OF THE STATIONARY PLASMA THRUSTER; N. A. Maslennikov, EDB “Fakel”, Russia

1995-077: AN OPERATION OPTIMIZING FOR BOTH ELECTRIC POWER AND PROPULSION SYSTEMS EQUIPPED WITH STATIONARY PLASMA THRUSTERS; P. O. Fedorov, A. N. Yatcina, Dnepropetr. State Univ., Ukraine

1995-078: STUDY OF ANODE LAYER THRUSTER OPERATION WITH GAS MIXTURES; A. V. Semenkin, H. O. Chislov, TsNIIMASH, Russia

1995-079: LOW-TEMPERATURE MODE OF ION ACCELERATION IN ANODE LAYER THRUSTER; A. G. Korsun TsNIIMASH, Russia

1995-080: TRANSVERSE EXPANSION OF PLASMA PLUMES AND PLASMOIDS INGECTED FROM ELECTRIC THRUSTERS; A. G. Korsun, TsNIIMASH, Russia

1995-86: A NEW FRENCH FACILITY FOR ION PROPULSION RESEARCH; P. Lasgorceix, M. Raffin, J. C. Lengrand, M. Dudeck, CNRS, France; A. Cadiou, CNES, France

1995-088: FUNDAMENTAL EXPERIMENTS OF C60 APPLICATION TO ION THRUSTER; Y. Nakayama, H. Takegahara, Tokyo Metropolitan Inst. of Tech., Japan

1995-089: 300 HOURS ENDURANCE TEST OF MICROWAVE ION THRUSTER; S. Satori, H. Kuninaka, K. Kuriki, Inst. of Space and Astr. Sci., Japan

1995-090: NUMERICAL SIMULATION OF GRID EROSION FOR ION THRUSTER; T. Shiraishi, Tokyo University, Japan; H. Kuninaka, S. Satori, and K. Kuriki, Inst. of Space and Astr. Sci., Japan

1995-091: EVALUATION OF THE T5 (UK-10) ION THRUSTER: SUMMARY OF PRINCIPAL RESULTS; M. W. Crofton, The Aerospace Corporation, USA

1995-092: PERFORMANCE OF THE PRIMARY RF-ION THRUSTER ESA-XX; P. Fahrenbach, K. H. Groh, and H. W. Loeb, Giessen University, Germany

1995-093: FABRICATION AND TESTING OF CARBON-CARBON COMPOSITE GRIDS FOR A 14 CM ION THRUSTER; S. Kitamura, K. Miyazaki, Y. Hayakawa, and Y. Nakamura, National Aerospace Laboratory, Japan; S. Yamaguchi, Hitachi Research Lab, Hitachi, Ltd., Japan

1995-094: AN ION ENGINE FOR SMALL SATELLITES; O. A. Gorshkov, V. A. Muravlev, NIITP, Russia; V. G. Grigoryan, S. V. Kanev, and V. I. Minakov, MAI, Russia

1995-095: THE NEW HIGH FREQUENCY ION THRUSTER (HFIT) DEVELOPMENT; V. B. Andreev, V. P. Kim, V. I. Kozlov, A. I. Skrylnikov, O. S. Sladkov, and V. N. Trusov, RIAME MAI, Russia; V. G. Grigoryan, MAI, Russia; G. F. Cirri, N. Kutufa, and G. Nocci, PROEL TECHN., Italy

1995-097: PULSED FEEP: NEW EXPERIMENTAL RESULTS; A. Genovese, S. Marcuccio, M. De Sio, CENTROSPAZIO, Italy; M. Andrenucci, Univ. Of Pisa, Italy

1995-098: FEEP THRUSTER PLUME INVESTIGATION WITH LANGMUIR PROBES; S. Marcuccio, A. Genovese, A. Turco, and H. J. Nick, CENTROSPAZIO, Italy; M. Andrenucci, Univ. of Pisa, Italy

1995-099: THE LOW POWER HF ION THRUSTER; T. B. Antonova, G. E. Burgrov, S. G. Kondranin, E. A. Kralkina, V. A. Obukhov, and N. F. Vorobjev, RIAME MAI, Russia; A. F. Alexandrov, Moscow State Univ., Russia; N. Kutufa, G. Noci, PROEL TECHN., Italy; A. A. Rukhadze, Inst. of General Phys. Russia

1995-100: LIFE-TIME TEST OF ESTEC OF THE RIT-10 THRUSTER FOR ARTEMIS; J. Gonzalez, G. Saccoccia, C. Bartoli, and F. van den Bos, ESA/ESTEC, The Netherlands; R. Kukies, H. Muller, Daimber Benz, Germany

1995-102: THE REVEALING OF OPTIMAL REGIMES OF HF LOW POWER UNPUT IN LIMITED MAGNETOACTIVE PLASMA FOR DEVELOPMENT OF HF ION THRUSTER OF THE NEW TYPE; T. B. Antonova, G. E. Bugrov, N. F. Vorobjev, S. G. Kondranin, E. A. Kralkina, and V. A. Obukhov, RIAME MAI, Russia; A. F. Alexandrov and A. V. Kalinin, Moscow State Univ., Russia; A. A. Rukhadze, Inst. of General Phys., Russia

1995-103: STATE OF THE ART AND FUTURE PROSPECTS OF COLLOIDAL ELECTRIC THRUSTERS; A. F. Shtyrlin, MAI, Russia

1995-104: INVESTIGATION OF ALKALI METAL MPD THRUSTERS; V. A. Petrosov, I. B. Safonov, Yu. A. Utkin, and V. N. Shutov, NIITP, Russia

1995-105: THE EXPERIMENTAL PERFORMANCES OF THE 100 KW LI MPD THRUSTER WITH EXTERNAL MAGNETIC FIELD; V. B. Tikhonov and S. A. Semenikhin, MAI, Russia; J. R. Brophy and J. E. Polk, JPL, USA

1995-106: POWERFUL QUASISTATIONARY PLASMA ACCELERATORS; V. V. Chebotarev, I. E. Garkusha, O. E. Kazakov, N. I. Mitina, D. G. Solyakov, V. I. Tereshin, S. A. Trubchaninov, and A. V. Tsarenko, Kharkov Inst. of Physics and Technology, Ukraine; A. I. Morozov, RSC “Kurchatov Institute”, Russia

1995-107: 2 MWE NEP SYSTEM WITH MPD-THRUSTER; Yu. A. Alexeev, M. N. Kazeev, A. S. Kaminski, V. S. Kuznetsov, and V. A. Pavshuk, RSC “Kurchatov Institute”, Russia

1005-108: ELECTROSTATIC INSTABILITIES OF A MAGNETOPLASMADYNAMIC THRUSTER IN THE INHOMOGENEOUS MEDIUM; K. P. Kirdyashev, Inst. Radioeng. and Electron. (Fryazino Moscow Region), Russia; J. V. Kubarev, Acad. of Eng. Sci., Russia

1995-109: EVALUATION OF CATHODE TEMPERATURE DISTRIBUTION IN A CYLINDRICAL MPD THRUSTER; M. W. Winter, M. Auweter-Kurtz, H. L. Kurtz, and P. C. Sleziona, Stuttgart University, Germany

1995-110: CATHODE HEATING EFFECTS ON THE CATHODE REGION PARAMETERS OF AN MPD THRUSTER; F. Paganucci, M. Andrenucci, and NP. Rossetti, CENTROSPAZIO, Italy

1995-111: SIX-COLOR VIDEO PYROMETRY WITH APPLICATION TO MPD THRUSTERS; E. Y. Choueiri, V. P. Chiravalle, G. E. Miller and R. G. Jahn, Princeton Univ., USA

1995-113: MAGNETIC CONTROL OF MPD ACCELERATOR JET PARAMETERS; Yu. V. Kubarev, Acad. of Eng. Sci., Russia; S. E. Rosinksy, Moscow State Acad. Instr. and Inform. Sci., Russia; I. B. Safonov and Yu. A. Utkin, NIITP, Russia

1995-114: PRELIMINARTY RESULTS ON SERVICE LIFE DEVELOPMENT OF PPT SCALE MODEL; N. N. Antropov, V. K. Gundobin, G. A. Popov, A. I. Rudikov, and S. Y. Shibanov, RIAME MAI, Russia

1995-115: PLASMA JET DYNAMIC OF COAXIAL PULSED PLASMA SOURCE OF EROSION TYPE; M. M. Orlov, A. I. Rudikov, L. A. Gomilka, I. G. Krivonosov, V. K. Gundobin, and V. N. Yakovlev, RIAME MAI, Russia

1995-116: PLASMA FEATURES IN QUASISTEADY MPD CHANNELS; H. Tahara, K. Mitsuo, L. Zhang, Y. Kagaya, and T. Yoshikaw, Osaka University, Japan

1995-118: BEHAVIOUR OF QUASI-STEADY ABLATIVE MPD THRUSTERS WITH DIFFERENT PROPELLANTS; G. Paccani and U. Chiarotti, University of Rome, Italy

1995-119: POWER PROPULSION SETS WITH PULSED PLASMA THRUSTER; V. L. Levtov, “Kompozit” Sci. and Prod. Assoc., Russia; V. V. Savitchev, Moscow State Techn. Univ., Russia

1995-120: PROPELLANT IONIZATION IN HIGH POWER MPD THRUSTERS; Ya. A. Alexeev, M. N. Kazeev, RSC “Kurchatove Institute”, Russia

1995-121: MPD THRUSTER WITH EXTERNAL MAGNETIC FIELD AND IONIZATION CHAMBER; V. B. Tikhonov and G. A. Dyakonov, RIAME MAI, Russia

1995-122: MATHEMATICAL SIMULATION FOR PPT OPERATION; L. A. Gomilka, G. A. Popov, and A. I. Rudikov, RIAME MAI, Russia

1995-123: RELEASE INTO THE SPACE OF EXCESS HEAT IN THE PERSPECTIVE HIGH POWER PLANTS; I. G. Panevin, MAI, Russia, B. N. Baushev and A. A. Koroteev, RIAME MAI, Russia

1995-124: POWER PROCESSING UNIT FOR ELECTRICAL PROPULSION THRUSTER SYSTEMS; A. I. Chernishev, Yu. A. Shinyakov, and N. M. Katasonov, GNPP “Polus” (Tomsk), Russia

1995-125: POSSIBLE STRUCTURAL-DESIGN SCHEMES OF SPACECRAFT WITH NUCLEAR-ELECTRIC PROPULSION SYSTEMS; P. V. Andreev, A. Ya. Galkin, G. M. Gryaznov, E. E. Zhabotinsky, and G. A. Zaritsky, “Krasnaya zvezda”, Russia; V. A. Kotin, R. S. Kremev, V. A. Kudryashov, and B. D. Yakovlev, Lavochkin ASSOC., Russia

1995-126: THE PROBLEM OF THE POWER PROCESSING AND TELEMETRY/CONTROL UNIT DESIGN FOR STATIONARY PLASMA THRUSTER; A. N. Petrenko, Dnepropetr. State Univ., Ukraine; J. A. Hamley and J. M. Sankovic, NASA Lewis R. C., USA

1995-128: PROJECT OF MULTIFUNCTION ELECTRIC PROPULSION PLANT FOR TRANSFERRING SPACE VEHICLES TO GEOSTATIONARY ORBIT; V. F. Prisniakov, A. I. Kondratyev, S. F. Lyagushin and I. N. Statsenko, Dnepropetr. State Univ., Ukraine; S. N. Konyukhov, DE “Pivdenne” (Dnepropetrovsk), Ukraine

1995-130: HIGH-TEMPERATURE SYSTEM OF THE ELECTRICAL CURRENT CONVERSION FOR POWERFUL ERT; V. V. Onufryev and S. D. Grishin, Moscow State Techn. Univ., Russia

1995-131: OPTIMAZTION OF THE PARAMETERS OF THE HIGH-TEMPERATURE RADIATION-RESISTANT CURRENT CONVERSION SYSTEMS FOR POWERFUL ERT; V. V. Onufryev, S. D. Grishin, and V. V. Savitchev, Moscow State Techn. Univ., Russia

1995-132: THE BMDO ELECTRIC PROPULSION FLIGHT READINES PROGRAM; L. H. Caveny, BMDO, USA; J. M. Sankovic, NASA Lewis RC, USA; D. M. Allen and G. Herbert, W. J. Shafer Ass., USA; C. E. Garner, JPL, USA

1995-133: THE NASA ELECTRIC PROPULSION PROGRAM; F. M. Curran, NASA Lewis RC, USA; L. W. Callahan, Office of Space Access and Techn., USA

1995-134: AN OVERVIEW OF THE CNES ELECTRIC PROPULSION PROGRAM; A. Cadiou and E. Gengembre, CNES, France

1995-135: ELECTRIC PROPULSION ACTIVITIES STATUS AND PLANS AT BPD. CENTROSPAZIO AND SEPA; W. D. Deininger, BPD Difesa e Spazio, Italy; M. Andrenucci, CENTROSPAZIO, Italy; E. Detoma, Div. SEPA, Italy

1995-136: TTE LEVERAGE OF ELECTRIC PROPULSION: SATELLITE PROPULSION SYSTEM TRADE-OFFS; W. D. Deininger and R. Nasi, BPD Difesa e Spazio, Italy

1995-139: ON-ORBIT PERFORMANCE OF ETS-VI ION ENGINE SUBSYSTEM; H. Hagano and K. Kajiwara, Nat. Space Devel. Agency, Japan; Y. Goton, E. Nishida, and Y. Fujita, Mitsubishi Elec. Corp. Japan

1995-142: THE PROSPECTS OF THE ELESTRIC ROCKET PROPULSION SYSTEM APPLICATIONS IN THE COMPOSITION OF THE SPACE VEHICLE TRANSPORT POWER MODULES; V. A. Menshikov, S. P. Zatserkovny, A. I. Kuzin, A. V. Malygin, K. A. Pavlov, and G. A. Shevtsov, Centr. Sci. Inst. of Space Force of Russia

1995-145: PROSPECTS FOR USE OF HIGH-POWER ION ENGINES IN THE OBJECTS OF DEVELOPING OF NEAR AND FAR SPACE; V. N. Akimov, O. A. Gorshkov, and Yu. M. Es’kov, NIITP, Russia

1995-147: SCALING LAWS FOR PULSED ELECTRIC PROPULSION WITH APPLICATION TO THE PLUTO EXPRESS MISSION; J. K. Ziemer, E. Y. Choueiri, and R. Jahn, Princeton Univ., USA

1995-148: THE CASE FOR SMALL SPACECRAFT: AN INTEGRATED PERSPECITIVE ON ELECTRIC PROPULSION; D. Barnhart, R. Wojnar, D. Tilley, and R. Spores, Phillips Laboratory, Edwards AFB, USA

1995-149: ACTIVE WAY OF REDUCING MICROACCELERATIONS OF SPACECRAFT BY USING ELECTRIC THRUSTERS; K. V. Evdokimov, V. G. Grigoryan, A. A. Izmaylov, S. A Khartov, L. A. Latyshev, and A. V. Shtyrlin, MIA, Russia; S. L. Ivanov and V. A. Kudryashov, NPO Lavochkin, Russia; V. V. Savichev, Moscow State Techn. Univ., Russia

1995-150: RF SHADOWS PRODUCED BY PLASMA PLUMES AND PLASMOIDS OF ELECTRIC THRUSTERS; F. F. Gabdullin, V. I. Garkusha, A. G. Korsun, and E. M. Tverdokhlebova, TsNIIMASH, Russia

1995-151: ELECTROMAGNETIC WAVES RADIATED BY ION BEAM INJECTED TO IONOSPHERE; G. G. Shishkin, RIAME MAI, Russia

1995-152: INTEGRATION OF ELECTROTHERMAL ENGINES WITH “ELECTRO” SPACECRAFT; V. P. Khodnenko, NPP VNIEM, Russia

1995-155: SELECTION OF ELECTRIC THRUSTER OF SUSTAINER PROPULSION SYSTEM FOR MARTIAN ORBITAL AND LANDING MISSION; M. N. Vatel, O. A. Gorshkov, and V. F. Semyonov, NIITP, Russia

1995-156: COMPARATIVE ANALYSIS OF THE PROPULSION SYSTEM FOR THE SMALL SATELLITES; G. Malyshev, V. Kulkov, A. Shtyrlin, I. Vyshedkevich, and R. Bychkov, RIAME MAI, Russia

1995-157: NUMERICAL INVESTIGATION OF COMPRESSION FLOWS IN A PLASMA ACCELERATOR CHANNEL; K. V. Brushlinsky, Inst. Appl. Mathem, Russia; G. A. Kalugin, Moscow Engin. Phys. Inst. Russia

1995-158: NUMERICAL SIMULATION OF MHD FLOWS WITH THE HALL EFFECT IN THE HIGH CURRENT QUASI-STEADY-STATE PLASMA ACCELERATOR (QSPA); K. V. Brushlinksy, K. P. Gorshenin, and T. A. Ratnikova, Inst. Appl. Mathem, Russia

1995-159: PROGRESS IN MODELING PLASMA THRUSTERS AND RELATD PLASMA FLOWS; P. J. Turchi, P. G. Mikellides, K. W. Hohman, R. J. Leiweke, I. G. Mikellides, and C. S. Schmahl, Ohio State University, USA; N. F. Roderick, University of New Mexico, USA; R. E. Peterkin, Phillips Lab., USA

1995-160: AXISYMMETRIC PIC-DSMC SIMULATIONS OF SPT PLUMES; D. Oh and D. Hastings, Massachusetts Inst. of Tech., USA

1995-161: NUMERICAL SIMULATION OF PLASMA FLOW DYNAMICS IN SPT; A. I Morozov, RSC “Kurchatov Institute”, Russia; V. V. Savelyev, Inst. Appl. Math., Russia

1995-162: NUMERICAL STUDY OF ION THRUSTER PLUME-SPACECRAFT INTERACTIONS; R. I. SAMANTA Roy, and D. E. Hastings, Massachusetts Inst. of Tech., USA; N. A. Gatsonis, Worcester Polytech. Inst., USA

1995-163: ION BEAM SIMULATION IN A SPACECRAFT ENVIRONMENT; K. K. Krupnikov, V. N. Mileev, L. S. Novikov, and V. V. Sinolits, Inst. of Nucl. Phys. Moscow State Univ., Russia

1995-164: PARTICLE SIMULATION OF PLASMA PHENOMENA IN HALL THRUSTERS; M. Hirakawa, Tokai University, Japan; Y. Arakawa, University of Tokyo, Japan

1995-168: NUMERICAL INVESTIGATION OF MPD THRUSTERS WITH UNSTRUCTURED MESH METHODS; C. Bole, M. Auweter-Kurtz, H. J. Kaeppeler, and P. C. Sleziona, Stuttgart University, Germany

1995-169: AN EFFICIENT NUMERICAL ANALYSIS OF FULLY IONIZED PLASMA FLOWS IN A SELF-FIELD MPD THRUSTER; T. Miyasaka and T. Fujiwara, Nagoya University, Japan

1995-170: THE NUMERICAL SIMULATION OF A JET OF RAREFIED PLASMA OUTFLOWING FROM THE AXIAL AND RING ORIFICES; L. A. Bazima, A. I. Oransky, and V. A. Pimkin, Khartov Aviation Inst., Ukraine

1995-171: PLUME MODEL OF HALL EFFECT PLASMA THRUSTERS WITH TEMPORAL CONSIDERATION; J. Dickens, M. Kristiansen, and E. O’Hair, Texas Tech. University, USA

1995-172: PROGRAM PACKAGE FOR THE CALCULATION OF SATELLITE ANTENNA PATTERN CHARACTERISTICS DURING THE OPERATION OF VERNIER ENGINES ON THE BASIS OF EP; V. G. Malko and A. P. Plokhikh, RIAME MAI, Russia; G. G. Shishkin, MAI, Russia; A. Soubeyran, Matra Marcony Space Comp., France

1995-173: THE THEORETICAL INVESTIGATION OF SURROUNDING GAS PRESSURE INFLUENCE ON THE SPT PLASMA JET PARAMETERS; A. M. Bishaev, V. K. Kalashnikov, V. Kim, and A. V. Shavikina, RIAME MAI, Russia

1995-174: THE INVESTIGATION OF THE TEMPERATURE FIELD IN THE SPT STRUCTURE ELEMENTS; S. Khartov, V. Serovaisky, A. Smakhtin, and R. Tchuyan, MAI, Russia; D. Valentian, SEP, France

1995-175: THE NUMERICAL MODELING OF PLASMA FLOW IN MPD THRUSTER; N. Barabanov, MAI, Russia

1995-176: NUMERICAL SIMULATION OF THE FLOW STRUCTURE OF THE HEAVY PARTICLES IN SPT; Yu. A. Ermakov, MIREA, Russia

1995-177: MATHEMATICAL MODELING OF CHARGED PARTICLES TRANSFER PROCESSES NEAR THE SURFACE IN JETS OF ELECTRIC PROPULSION ENGINES; M. V. Kotelnikov and A. V. Shankov, MAI, Russia

1995-178: CERAMIC COATINGS USING QUASISTEADY MPD ARCJETS; H. Tahara, K. Mitsuo, L. Zhang, T. Yasui, Y. Kagaya, and T. Yoshikawa, Osaka Univ., Japan

1995-179: A 5, 730-HR CYCLIC ENDURANCE TEST OF THE SPT-100; C. E. Garner, J. R. Brophy, J. E. Polk, and L. C. Pless, JPL, USA; Dan A. Starling, Navai Postgraduate School, USA

1995-180: LARGE RADIO-FREQUENCE ION BEAM SOURCES PRIS 10, RIM 20, RIM 25, RIM 35, AND RIM 12x50 FOR SURFACE TREATMENT; J. Freisinger, A. Kux, and H. W. Loeb, Giessen University, Germany

1995-181: LOW FLOW RATE IMPULSIVE PLASMA ACCELERATOR, ACDE-TYPE FOR TECHNOLOGY PURPOSES; A. N. Veselovzorov and A. A. Pogorelov, RSC “Kurchatov Institute”, Russia

1995-182: MPD-THRUSTER FOR TECHNOLOGY APPLICATIONS; Yu. A. Alexsev and M. N. Kazeev, RSC “Kurchatov Institute”, Russia

1995-185: SOURCE OF INTENSIVE OXYGEN PLASMA FLOWS OF LOW ENERGY FOR TECHNOLOGICAL APPLICATIONS; L. N. Devashova, V. V. Yegorov, B. A. Mednikov, and V. K. Shinin, RIAME MAI, Russia

1995-186: THE DEVELOPMENT OF PLASMA ACCELERATOR WITH INTENSE DIVERGENCE AND HIGH UNIFORMITY OF ION FLOW FOR TECHNOLOGICAL APPLICATIONS; L. N. Devashova, V. V. Yegorov, B. A. Mednikov, and V. K. Shinin, RIAME MAI, Russia

1995-188: IGNITION SYSTEM FOR AUTOMOBILE MOTOR WITH PULSED ACCELERATOR; I. N. Statsenko, V. N. Statsenko, Yu. N. Statsenko, V. I. Zaitsev, and A. A. Krylov, Dnepropetr. State Univ., Ukraine; V. V. Rybakov, MAI, Russia; B. N. Pyatko, Meltopol Motor-Building Plant, Ukraine

1995-189: PLASMA SOURCE USAGE IN VACUUM TECHNOLOGY; B. A. Arkhipov, N. A. Maslennikov, and A. N. Nesterenko, EDB “Fakel”, Russia; V. Kim, RIAME MAI, Russia

1995-190: PLASMA DIAGNOSTICS INSIDE A MICROWAVE DISCHARGE ION THRUSTER USING TUNABLE LASER DIODES; K. Nishiyama, S. Satori, H. Kuniinaka, and K. Kuriki, Inst. of Space and Astronat. Science, Japan; Th. Wegmnn, Stuttgart Univ. Germany

1995-191: NON-STATIONARY ELECTRIC PROBE FOR PLASMA DIAGNOSTIC OF ELECTRIC PROPULSION ENGINES; M. V. Koteinikov, MAI, Russia

1995-192: OPTICAL SPECTROSCOPY ANALYSIS OF A STATIONARY PLASMA THRUSTER; J. Bonnet, P. Leray, and D. Pigache, ONERA, France; J. Bretagne and A. Ricard, Universite Paris, France; M. Lyszyk, SEP, France

1995-194: MULTYPARAMETRIC ANALYZE OF THE EXPERIMENTAL DATA OBTAINED DURING ELECTRIC PROPULSION SYSTEMS TESTING; S. A. Andrianov, S. A. Khartov, and L. A. Latyshev, MAI, Russia; A. V. Malygin, K. A. Pavlov, Centr. Sci. Inst. of Space Forces of Russia

1995-195: LASER INTERFEROMETRY FOR PULSED PLASMA THRUSTER PERFORMANCE MEASUREMENT; E. A. Cubbin, J. K. Ziemer, E. Y. Choueiri, and R. G. Jahn, Princeton University, USA

1995-196: ANALYSIS OF ANODE LAYER THRUSTER GUARD RING EROSION; C. Marrese, L. B. King, and A. C. Galimore, Univ. of Michigan, USA; J. E. Polk and C. E. Garner, JPL, USA; A. Semenkin, V. Garkusha, and S. Tverdoklebov, TsNIIMASH, Russia

1995-197: A WAVEGUIDE IR LASER FOR NEUTRALS AND ION BEAMS DIAGNOSTICS; B. A. Kuzyakov, Inst. of High Temper., Russia

1995-198: REACTIVE PLASMA ACCELERATOR JET POTENTIAL MEASUREMENT BY EMISSIVE PROBE WITH PLASMA ELECTRON HEATING; V. N. Chernik, Inst. of Nuclear Phys., Moscow State Univ., Russia

1995-199: NEUTRALIZER/PLASMA CONTACTOR TECHNOLOGIES: REVIEW OF DEVELOPMENT ACTIVITIES AT PROEL TECHNOLOGIE; A. Severi, G. Matticari, A. Matucci, and M. Municci, PROEL TECHN., Italy; G. Saccoccia, ESTEC-YPE, The Netherlands; F. Svelto, Italian Space Agency, Italy

1995-200: AMPULE CATHODE-NEUTRALIZER; A. V. Khitko, N. V. Maslyany, and V. F. Pridantzev, Dnepropetr, State Univ., Ukraine

1995-201: APPLICATION OF HOLLOW CATHODE IN ARCJET PROPULSION AT LOW AND AVERAGE POWER; E. P. Vaulin, L. V. Feoktistov, and N. V. Petukhov, MAI, Russia; V. A. Obukhov, RIAME MAI, Russia; F. Scortecci, CENTROSPAZIO, Italy

1995-202: HIGH FREQUENCY OSCILLATIONS IN THE HOLLOW CATHODE AND THEIR INFLUENCE ON ITS OPERATION; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, V. I. Vasin, and Yu. M. Yashnov, NIITP, Russia

1995-203: ENERGY SPECTRUM OF ELECTRONS IN A NEAR-CATHODE LAYER; B. B. Rodnevich, NIITP, Russia

1995-204: MONITORING OF ELECTRIC THRUSTER CATHODE-NEUTRALIZER EROSION USING SPECTRAL AND PROBE MEASUREMENTS IN PLASMA; V. I. Baranov, A. I. Vasin, V. A. Petrosov, NIITP, Russia; E. I. Asinovsky, V. V. Markovets, V. P. Polishchuk, I. M. Yartsev, and Yu. V. Vizilter, Inst. High. Temper., Russia

1995-205: THE HIGH EMISSION SELFHEATED ARC DISCHARGE HOLLOW CATHODES; A. I. Oransky, Kharkov Aviation Inst., Ukraine

1995-206: NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEMPERATURE FIELDS AND HEAT FLUXES IN ELECTRIC THRUSTERS; A. F. Anikin, S. M. Bednov, V. I. Baranov, and A. N. Golikov, NIITP, Russia

1995-207: THE MODIFIED BALANCE METHOD OF NEAR-CATHODE PROCESSES CALCULATION CHARACTERISTICS; Y. V. Bruevich, I. P. Nazarenko, and I. G. Panevin, MAI, Russia

1995-208: THE METHOD OF EXPRESS ESTIMATION OF GAS HOLLOW CATHODE EROSION RATE AND RESULTS OF IT APPROBATION; Ye. A. Isayev and A. I. Oransky, Kharkov Aviation Inst., Ukraine

1995-209: THE PECULARITIES OF HOLLOW CATHODES EROSION AT NON-INCANDESCENT SWITCHING ON; N. N. Koshelev, A. V. Loyan, and A. I. Oransky, Kharkov Aviation Institute., Ukraine

1995-210: THE MODEL AND CALCULATION OF HOLLOW CATHODE EROSION; A. S. Dolgov, A. V. Zaharchenko, S. Yu. Nesterenko, and A. I. Oransky, Kharkov Aviation Inst., Ukraine

1995-211: INFLUENCE OF MASS FLOW RATE OF ACTIVATOR ON WORK OF GAS HOLLOW CATHODE; A. V. Khitko, Dnepropetr. State Univ., Ukraine

1995-212: NOVEL ORBIT RAISING STRATEGY MAKES LOW THRUST COMMERCIALLY VIABLE; A. Spitzer, Hughes Aircraft Company, USA

1995-213: ESTIMATE OF THE OPTIMAL MERCURY-RENDEZVOUS LOW-THRUST TRAJECTORY WITH VENUS SWINGBY; M. S. Konstantinov, MAI, Russia

1995-214: ASSOCIATED OPTIMIZATION OF THE LOW-THRUST TRAJECTORY AND PARAMETERS OF THE NUCLEAR POWER PLANT; P. V. Andreev, A. Y. Galkin, G. M. Gryaznov, G. A. Zaritsky, and E. E. Zhabotinsky, “Krasnaya zvezda”,Russia; G. G. Fedotov, M. S. Konstantinov, and V. G. Petukhov, MAI, Russia

1995-215: INTERPLANETARY TRAJECTORY OPTIMISATION CODES FOR ELECTRIC PROPULSION RESEARCH; M. Nakano, Y. Ishijma, and Y. Arakawa, Tokyo Univ., Japan

1995-217: THE PLUTO RENDEZVOUS MISSION WITH SOLAR-NUCLEAR ELECTRIC PROPULSION; R. Z. Akhmetshin, T. M. Eneev, and G. B. Efimov, Inst. of Appl. Mathem., Russia

1995-220: APPLICATION OF THE POWER-LIMITED PROBLEM TO THE ELECTRIC PROPULSION MISSION DESIGN; G. G. Fedotov, M. S. Konstantinov, and V. G. Petukhov, MAI, Russia

1995-221: ONE NUMERICAL METHOD TO CALCULATE OPTIMAL POWER-LIMITED TRAJECTORIES; V. G. Petukhov, MAI, Russia

1995-222: OPTIMIZATION OF ORBITAL TRANSFERS AND INTERPLANETARY MISSIONS WITH ELECTRIC PROPULSION; Yu. A. Zakharov, MAI, Russia

1995-226: MATHEMATICAL SIMULATION OF ELECTROMAGNETIC PLASMA AND SOLID ARMATURES ACCELERATION IN RAILGUN BORE; M. P. Galanin, E. V. Mayakova, Yu. P. Popov, and S. Khramtsovsky, Inst. Applied Math., Russia; A. V. Plekhanov, “Soyuz”, Russia; V. V. Savitchev, Moscow State Techn. Univ., Russia

1995-228: THE ROLE OF ANALYSIS AND TESTING IN THE SERVICE LIFE ASSESSMENT OF ION ENGINES; J. E. Polk, N. R. Moore, J. R. Brophy, and D. H. Ebbeler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

1995-229: PLASMA SOURCE USAGE IN VACUUM TECHNOLOGY; B. A. Arkhipov, N. A. Maslennikov, and A. N. Nesterenko, EDB “Fakel”, Russia; V. Kim, RIAME MAI, Russia

1995-230: THE DEVELOPMENT INVESTIGATION OF THE CATHODE-COMPENSATOR OF STATIONARY PLASMA THRUSTERS FOR DISCHARGE CURRENTS OF TO 50 A; B. A. Arkhipov, S. S. Kudriavtsev, N. A. Maslennikov, V. M. Murashko, and I. A. Turgeneva, EDB “Fakel”, Russia

1995-231: ELECTRIC PROPULSION SYSTEM FOR SPACECRAFT ACCELERATION AND MANOUEVRING DURING FLIGHT TO ASTEROIDS; B. A. Arkhipov, A. S. Bober, N. A. Maslennikov, EDB “Fakel”, Russia; G. A. Popov, RIAME MAI, Russia

1995-232: FACILITY FOR TESTING ELECTRIC THRUSTERS AND PROPULSION SYSTEMS; A. S. Bober, N. A. Maslennikov, V. A. Ivanov, EDB “Fakel”, Russia

1995-234: THE ROLE OF SPOT MODE TRANSITION IN THE ANODE FALL OF PULSED MPD THRUSTERS; K. D. Diamant, E. y. Choueiri, and R. G. Jahn, Princeton Univ., USA

1995-235: ELECTRIC PROPULSION SYSTEM ON THE SPACEBUS SPACECRAFT FAMILY; M. Perdu, P. Borie, and T. Grassin, Aerospatiale, France

1995-236: A STUDEY OF ALKALI-SEEDED HYDROGEN ARCJET PERFORMANCE; F. Oyerokun, M. Martinez-Sanchez, Massach. Inst. Tech., USA

1995-237: DEVELOPMENT OF A 500 WATT CLASS ARCJET THRUSTER SYSTEM; P. G. Lichon, G. H. McLean, and C. E. Vaughan, OLIN Aerospace Comp., USA; J. M. Sankovic, NASA LeRC, USA

1995-239: ELECTRIC PROPULSION FOR AN INTERPLANETARY ASTROPHYSICS MISSION; B. T. Patel, M. Martinez-Sanchez, and G. R. Ricker, Massach. Inst. of Technology, USA; D. Tilley and D. Barnhart, Phillips Lab., USA; H. Alexander, Orbital Sci. Corp. USA; R. Myers, E. Pencil, G. Horvart, and J. Samella, NASA Lewis RC, USA

1995-240: TWO-DIMENSIONAL HYBRID PARTICLE-IN-CELL (PIC) MODELING OF HALL THRUSTERS; J. M. Fife and M. Martinez-Sanchez, Massach. Inst. of Tech., USA

1995-241: THE EFFECT OF POWER SUPPLY OUTPUT CHARACTERISTICS ON THE OPERATION OF THE SPT-100 THRUSTER; J. A. Hamley and J. M. Sancovic, NASA Lewis RC, USA; A. N. Petrenko, Dnepropetr. State Univ., Ukraine; D. H. Manzella, NYMA Inc., USA; K. C. Cartier, ANALEX Inc., USA

1995-242: PRELIMINARY INVESTIGATION OF THE ORIGINAL 1 KW ARCJET MODEL; V. D. Gratchev, A. G. Klimenko, S. V. Pavlov, and G. Ya. Saveliev, NIITP, Russia

1995-244: THE USA AIR FORCE ELECTRIC PROPULSION PROGRAM; R. A. Spores, Phill. Lab., USA; M. Birkan, AFOSR/NA, USA; R. Cohen, Aerospace Corp., USA; R. Einhorm, US Air Force, USA

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IEPC1995-135.pdf 19:48 3.7M

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IEPC1995-Index

IEPC1995-Vol.1.Index.pdf 18:26 10M

IEPC1995-Vol.2.Index.pdf 19:31 8.1M

IEPC1995-Vols1-2_Index.pdf 13:46 5.9M

notes.txt 19:35 28

1997 INDEX

1997-001: THE USAF ELECTRIC PROPULSION PROGRAM; Ronald A. Spores, Phillips Laboratory/RKES, Edwards AFB, CA 93524; Ronald B. Cohen, Aerospace Corporation, El Segundo, CA 90009; and Mitat Birkan, AFOSR/NA, Bolling AFB, Washington, DC 20332

1997-002: ELECTRIC PROPULSION IN EUROPE: DEVELOPMENT AND APPLICATIONS; Giorgio Saccoccia, Head of Electric Propulsion Unit, ESA Technical and Operational Support Directorate, ESTEC, Keplerlaan 1, 2200 AG, Noordwijk, The Netherlands

1997-003: NASA’S ELECTRIC PROPULSION PROGRAM; Francis M. Curran and Timothy E. Tyburski, National Aeronautics and Space Administration, Lewis Research Center, 21000 Brookpark Road, Mail Stop 301-3, Cleveland, Ohio, USA, 44135

1997-004: DEVELOPMENT AND APPLICATION OF ELECTRIC THRUSTERS AT EDB “FAKEL”; B. A. Arhipov, V. N. Vinogradov, K. N. Kozubsky, S. S. Kudriavtsev, N. A. Maslennikov, and V. M. Murashko, Experimental Design Bureau “Fakel”, Kaliningrad, Russia

1997-005: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; K. Toki, Associate Professor, Institute of Space and Astronautical Science, Sagamihara, Kanagawa, Japan; A. Sasoh, Associate Professor, Institute of Fluid Science, Tohoku University, Sendai, Miyagai, Japan

1997-006: AN OVERVIEW OF ELECTRIC POWER: A KEY TECHNOLOGY FOR ELECTRIC PROPULSION; Gary L. Bennett, Metaspace Enterprises; 5000 Butte Road, Emmett, Idaho 83617-9500, USA; Henry W. Brandhorst, Jr., Space Power Institute, 231 Leach Center, Auburn University, Alabama 36849-5320; C. P. Bankston, Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, California 91109-8099, USA; and R. J. Sovie, Lewis Research Center, 21000 Brookpark Road, Cleveland, Ohio 44135-3191, USA

1997-007: 100 kW CLASS HYDROGEN ARCJET THRUSTER; Monika Auweter-Kurtz, Thomas GÃ¶lz, Harald Habiger, Frank Hammer, Helmut Kurtz, Martin Riehle, and Christian Sleziona; Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Federal Republic of Germany

1997-008: 1 kW HYDRAZINE ARCJET SYSTEM DEVELOPMENT; Martin Riehle, Helmut L. Kurtz, and Monika Auweter-Kurtz; Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany; and York E. Viertel, Daimler-Benz Aerospace AG, Space Infrastructure Division, HÃ¼nefeldstrabe 105, D-28361, Bremen, Germany

1997-010: TESTING OF A 1.8 kW, FLIGHT QUALIFIED HYDRAZINE ARCJET SYSTEM; Gaetano De Lorenzo and William D. Deininger, FiatAvio – Comprensorio BPD, 00034, Colleferro (Rm), Italy; Richard D. Smith, PRIMEX Aerospace Company, Redmond, WA 98076-9709, USA

1997-011: NUMERICAL SIMULATION OF A LOW POWER ARCJET THRUSTER; Andrea Santovincenzo, William D. Deininger, and Gaetano De Lorenzo, FiatAvio – Comprensorio BPD, 00034, Colleferro (Rm), Italy; Vito Salvatore and Annamaria Russo Sorge, DISIS – Dipartimento di Scienza ed Ingegneria dello Spazio, Universita degli Studi “Federico II”, Napoli, Italy

1997-012: STABILITY OF ALKALI-SEEDED HYDROGEN ARCJETS; Folusho Oyerokun, Darrel Robertson, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts

1997-013: MEASUREMENTS OF ANODE HEAT TRANSFER IN A 1 KW ARCJET; Nicholas T. Tiliakos, Rodney L. Burton, and Herman Krier, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1997-014: METHANE ARCJET DEVELOPMENT; V. Hruby and J. Kolencik, Busek Co. Inc., Natick, MA 01760-1023; M. Martinez-Sanchez, MIT, Cambridge, MA 02139; D. Dvore, Consultant, Rowe, MA 01367; K. D. Annen and R. C. Brown, Aerodyne Research, Inc., Billerica, MA 01821-3976

1997-015: DEVELOPMENT OF AN EFFICIENT THREE-DIMENSIONAL OPTICS CODE; M. Nakano and Y. Arakawa, The University of Tokyo, Hongo 7-3-1, Bunkyo-ku, 113 Japan

1997-016: THE DEVELOPMENT OF THE ESA-XX ION THRUSTER; Helmut Bassner, Space Infrastructure, Diamler-Benz Aerospace AG, Postfach 80 11 69, D-81663 MÃ¼nchen, Germany; Robert Bond and Vaughan Thompson, AEA Technology plc, Culham Science and Technology Centre, Abingdon, Oxon OX14 3 DB, United Kingdom; and Klaus Groh, University of GieBen, Heinrich-Buff-Ring 16, D. 35392 GieBen, Germany

1997-017: MAPPING THE MAGNETIC FIELD OF THE DERA T5 KAUFMAN-TYPE ION THRUSTER; S. N. Moore, Space Dept. Defence Evaluation & Research Agency, Farnborough, Hampshire, GU14 0LX, United Kingdom

1997-018: COMMERCIALIZED ION PROPULSION FOR NORTH/SOUTH STATIONKEEPING OF COMMUNICATION SATELLITE; H. Bassner and K. Bohnhoff, Diamler-Benz Aerospace AG, Munich, Germany; A. Trivulzio, FIAR S.p.A., Space Division, Milano, Italy

1997-019: PROFILING THE BEAM OF THE T5 ION ENGINE; James E. Pollard, The Aerospace Corporation, P. O. Box 92957, M5-754, Los Angeles, CA 90009

1997-020: MONTE CARLO SIMULATION OF NEUTRAL XENON FLOWS OF ELECTRIC PROPULSION DEVICES; Iain D. Boyd, Douglas B. VanGilder, and Xiaoming Liu, Cornell University, Ithaca, NY 14853

1997-021: ELECTRON TRANSPORT MECHANISM IN A HALL THRUSTER; Miharu Hirakawa, Tokai University, Hiratsuka-shi, Kanagawa, Japan

1997-022: SCALING LAWS FOR HALL THRUSTER PERFORMANCE; A. Fruchtman, Center for Technological Education Holon, 52 Golomb St., P.O. Box 305, Holon 58102, Israel; N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, P.O. Box 451, Princeton, NJ 08543, USA; J. Ashkenazy and Y. Raitses, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

1997-023: HIGH-VOLTAGE MODE OF THE TAL THRUSTER OPERATION; S. O. Tverdokhlebov and V. I. Garkusha, Central Research Institute of Machine Building, 14170, Korolev, Moscow Region, Russia

1997-024: SOME RESULTS OF THE SPT JET CHARACTERISTICS COMPARISON; Mikhail V. Zikeyev, Moscow State Aviation Institute, Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 12571, Russia

1997-025: CALCULATION OF CHARACTERISTICS OF THE ELECTRIC PROPULSION PLUME INTRINSIC RADIATION; A. P. Plokhikh and G. G. Shishkin, Research Institute of Applied Mechanics and Electrodynamcis of Moscow Aviation Institute, Moscow, Russia

1997-026: EFFECT OF THE PLASMA POTENTIAL OSCILLATIONS AT A THRUSTER OPERATION; A. V. Zharinov, State Researche of Energy Institute, Moscow, Russia; and V. I. Garkusha, Central Researce Institute of Machine Building, Moscow reg., Russia

1997-027: THE I.S.P. SOFTWARE: CALCULATION OF THE SPT JET INFLUENCE; D. Borie, AÃ©rospatiale, Cannes, V. Perrin, Principia, S. Khartov, and A. Nadiradze, MAI Institute, Russia

1997-028: GEOMAGNETIC FIELD PERTURBATION BY A PLASMA PLUME; A. G. Korsun and E. M. Tverdokhlebova, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow region, Russia

1997-031: OPERATIONAL CHARACTERISTICS OF MICROWAVE DISCHARGE NEUTRALIZER; Shin Satori and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa, Japan; Motoyuki Ohtaki and Yoshio Ishikawa, Nippon University, 7-24-1, Narashino dai, Funabashi, Chiba, Japan

1009-033: DESIGN AND DEVELOPMENT OF AN ELECTRONIC PRESSURE REGULATOR FOR USE ON ION PROPULSION SYSTEMS; Dr. H. L. Gray, Matra Marconi Space UK, Ltd., Anchorage Road, Portsmouth, Hampshire PO3 5PU, England

1997-035: IEPC 97-035 ELECTROMAGNETIC ACCELRATION IN PLUSED PLASMA THRUSTERS; D. Keefer and R. Rhodes, University of Tennessee Space Institute, Tullahoma, Tennessee 37388

1997-036: NUMERICAL INVESTIGATION OF PULSED PLASMA THRUSTER PLUMES; Xuemin Yin and Nikos A. Gatsonis, Computational Gas & Plasma Dynamics Laboratory, Mechanical Engineering Department, Worcester Polytechnic Institute, Worcester, MA 01609

1997-037: THEORETICAL STUDIES OF A PULSED PLASMA MICROTHRUSTER; P. G. Mikelldes, P. J. Turchi, R. Leiweke, C. S. Schmahl, and I. G. Mikellides

1997-038: DIRECTIONS FOR IMPROVING PPT PERFORMANCE; P. J. Turchi, The Ohio State University, Columbus, Ohio USA

1997-041: THEORECTICAL AND COMPUTATIONAL ANALYSIS OF PULSED PLASMA THRUSTER PLUMES; Nikos A. Gatsonis and Xuemin Yin, Computational Gas & Plasma Dynamics Laboratory, Mechanical Engineering Department, Worcester Polytechnic Institute, Worcester, MA 01609

1997-042: ELECTRICAL POTENTIALS IN THE NSTAR CHARGE EXCHANGE PLUME; Ira Katz and V. A. Davis, Maxwell Technologies Federal Division, 8888 Balboa Ave., San Diego, CA 92123; Joseph Wang and David Brinza, Jet Propulsion Laboratory, 4800 Oak Grove, Pasadena, CA 91109

1997-043: PREDICTIONS OF NSTAR CHARGE EXCHANGE IONS AND CONTAMINATION BACKFLOW; V. A. Davis, Barbara Gardner, and Ira Katz, Maxwell Technologies Federal Division, Inc. 8888 Balboa Ave., San Diego, CA 92123-1506; David Brinza, Jet Propulsion Laboratory, MS 125-177, 4800 Oak Grove Drive, Pasadena, CA 91109

1997-044: NSTAR ION ENGINE XENON FEED SYSTEM: INTRODUCTION TO SYSTEM DESIGN AND DEVELOPMENT; Edward D. Bushway III, Moog, Inc., East Aurora, NY; Carl S. Engelbrecht and Dr. Gani B. Ganapath, Jet Propulsion Laboratory, Pasadena, CA

1997-047: IN SITU, TIME-RESOLVED ACCELERATOR GRID EROSION MEASUREMENTS IN THE NSTAR 8000 HOUR ION ENGINE WEAR TEST; J. E. Polk, J. R. Anderson, J. R. Brophy, V. K. Rawlin, M. J. Patterson and J. Sovey

1997-049: SERVICE LIFE ASSESSMENT FOR ION ENGINES; John R. Anderson, James E. Polk, and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

1997-051: THERMAL ENVIRONMENTAL TESTING OF NSTAR ENGINEERING MODEL ION THRUSTERS; Vincent K. Rawlin and Michael J. Patterson, NASA Lewis Research Center, Cleveland, OH; and Raymond A. Becker, Jet Propulsion Laboratory, Pasadena, CA

1997-052: DEVELOPMENT OF A STATIONARY PLASMA THRUSTER MATHEMATICAL MODEL ON THE BASE OF EXPERIMENTAL DATA; Olexandre N. Petrenko and Olexandre N. Yatcina; Dnepropetrovsk State University, Institute of Physics and Technology, Naukovy Line, 13, 320625 Dnepropetrovsk-10, Ukraine

1997-053: CHARACTERIZATION OF PLASMA INSIDE THE SPT-50 CHANNEL BY ELECTROSTATIC PROBES; G. Guerrini, C. Michaut, and M. Bacal, Laboratoire de Physique des Milieux IonisÃ©s, Laboratoire du C.N.R.S., Ecole Polytechnique, 91128 Palaiseau Cedex, France; M. Dudeck, Laboratoire d’AÃ©othermique, Meudon and UniversitÃ© Paris 6, France; and A. N. Vesselovzorov, RCC Kurchatov Institute, Moscow, Russia

1997-054: SPATIALLY RESOLVED EMISSION SPECTROSCOPY ALONG A SPT CHANNEL INTERPRETATION OF DATA BY A COLLISIONAL-RADIATIVE MODEL; Philippe Leray, Jean Bonnet, and Daniel Pigache, ONERA (Office National d’Etudes et de Recherche AÃ©rospatiale), BP n72 92322 ChÃ¡tillon cedex, France; Tiberiu Minea, Jean Bretagne, and Michael Touzeau, Laboratoire de Physique des Gaz et des Plasmas, U. A. CNRS, Bat. 212, UniversitÃ© Paris-Sub, 91405 ORSAY Cedex, France

1997-055: EXTERNAL ANODE LAYER THRUSTER PARAMETERS AT A HIGH SPECIFIC IMPULSE REGIMES; A. Semenkin, Central Research Institute of Machine Building, Korolev, Russia

1997-056: EXPERIMENTAL INVESTIGATION OF THE EFFECT OF CHANNEL MATERIAL ON HALL THRUSTER CHARACTERISTICS; Y. Raitses, J. Ashkenazy, and G. Appelbaum, Propulsion Physics Laboratory, Soreq, Yavne 81800, Israel; and M. Guelman, Faculty of Aerospace Engineering, Technion, IIT, Haifa

1997-058: A STUDY OF A LOW POWER HALL THRUSTER TRANSIENT BEHAVIOR; W. A. Hargus, Jr., N. B. Meezan, and M. A. Cappelli, Mechanical Engineering Department, Thermosciences Division, Stanford University, Stanford, CA 94305

1997-059: PERFORMANCE EVALUATION OF THE SPT-140; David Manzella, NYMA, Inc., Engineering Services Division, Brook Park, Ohio 44142; Charles Sarmiento, John Sankovic, and Tom Haag, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

1997-060: ENERGY BALANCE AND ROLE OF WALLS IN ACDE; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, A. I. Vasin, and Yu. M. Yashnov, Keldysh Research Center, Moscow, Russia

1997-061: PLASMA DIAGNOSTICS INSIDE A MICROWAVE DISCHARGE ION THRUSTER; K. Nishiyama, The University of Tokyo, Japan; S. Satori, H. Kuninaka, and K. Kuriki, Institute of Space and Astronautical Science, Japan; and Y. Arakawa, The University of Tokyo, Japan

1997-063: NONEQUILIBRIUM HYDROGEN/NITROGEN PLASMAS STUDIES USING A CASCADE ARC; Trevor Moeller, Dennis Keefer, and Robert Rhodes, University of Tennessee Space Institute, B. H. Goethert Parkway, Tullahoma, TN 37388

1997-064: PLUME DIAGNOSTICS OF AN APPLIED FIELD ACRJET BY USING A DIODE-LASER ABSORPTION TECHNIQUE; Kimiya Komurasaki, Teruhito Iida, Daisuke Kusamoto, Feng Yuan Zhang, Department of Aerospace Engineering, Nagoya University, Furo-cho, Chikusa, Nagoya 464-01, Japan; and Shin Satori, The Institute of Space and Astronautical Science, Yoshinodai, Sagamihara 229, Japan

1997-065: FLAT ORIENTED PROBE IN THE RAREFIELD PLASMA FLOW; Vladimir Kim, Research Institute of Applied Mechanics and Electrodynamics of Moscow State Aviation Institute (RIAME MAI), Moscow, Russia; Vadim A. Kotelnikov and Michael V. Kotelnikov, Moscow State Aviation Institute – Technical University (MAI), Moscow, Russia

1997-066: DEVELOPMENT OF A SINGLE-ORIFICE RETARDING POTENTIAL ANALYZER FOR HALL THRUSTER PLUME CHARACTERIZATION; Colleen M. Marrese, Neha Majumdar, James M. Haas, George Williams, Lyon B. King and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL) Dept. of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan

1997-067: OPTICAL DIAGNOSIS OF PLASMA IN A CHANNEL OF HALL THRUSTERS; Daisuke Kusamoto and Kimiya Komurasaki, Department of Aerospace Engineering, Nagoya University, Chikusa, Nagoya 464-01, Japan

1997-068: A REVIEW OF LOW ENERGY SPUTTERING THEORY AND EXPERIMENTS; Olivier B. Duchemin, California Institute of Technology, Pasadena, CA 91125; John R. Brophy and Charles E. Garner, Jet Propulsion Laboratory, Pasadena, CA 91109; Pradosh K. Ray and V. Shutthanandan, Tuskegee University, Tuskegee, AL 36088; and Maris A. Mantenieks, Lewis Research Center, Cleveland, OH 44135

1997-069: ON THE MEASUREMENT OF LOW-ENERGY SPUTTERING YIELD USING RUTHERFORD BACKSCATTERING SPECTROMETRY; V. Shutthanandan and Pradosh K. Ray, College of Engineering, Architecture and Physical Sciences, Tuskegee University, Tuskegee, AL 36088; N. R. Shivaparan and Richard J. Smith, Physics Department, Montana State University, Bozeman, MT 59717; S. Thevuthasan, Environmental Molecular Sciences Laboratory, Pacific Northwest National Laboratory, Richland, WA 99352; and Maris A. Mantenieks, NASA-Lewis Research Center, Cleveland, OH 44135

1997-070: BATCH-FABRICATED RESITOJETS: INITIAL RESULTS; Siegfried W. Janson, Technology Operations, Mechanics and Materials Technology Center, The Aerospace Corporation, Los Angeles, California

1997-071: MICRO-FABRICATED ACCELERATOR GRID SYSTEM FEASILITY ASSESSMENT FOR MICRO-ION ENGINES; Juergen Mueller, William C. Tang, Wen Li, and Andrew P. Wallace, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1997-072: DESIGN CONSIDERATIONS FOR ION MICROTHRUSTERS; G. J. Yashko, G. B. Giffin, and D. E. Hastings, Massachusetts Institute of Technology, Cambridge, Massachusetts

1997-073: CHANNEL ION SOURCE; Graeme Aston and Martha B. Aston, Electric Propulsion Laboratory, Inc., Monument, CO 80132

1997-074: FULLERENE ION THRUSTER DEVELOPMENT; V. Hruby, J. Monheiser, and J. Kolencik

1997-075: AN INVESTIGATION OF FULLERENE PROPELLANT FOR RF ION THRUSTERS; J. Steven Snyder and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523; John R. Anderson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1997-076: C60 APPLICATION TO ION THRUSTER – INSPECTION OF IONIZED AND EXTRACTED PARTICLE; Yoshinori Nakayama and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Asahigaoka 6-6, Hino, Tokyo 191, Japan

1997-077: PRELIMINARY EXPERIMENTAL EVALUATION OF A MINIATURIZED HALL THRUSTER; Vadim Khayms and M. Martinez-Sanchez, Space Systems Laboratory, MIT Department of Aeronautics and Astronautics

1997-078: THE LOW POWER HELIUM PULSED ARCJET; Gary F. Willmes and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, IL 61801

1997-079: NEW GENERATION OF ELECTRIC THRUSTERS; Vladimir Grigorian, Konstantin Evdokimov, Avil Izmailov, Sergey Khartov, Leonid Latyshev, and Alexander Shtyrlin, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d.4, Moscow, 125871, Russia

1997-081: FLIGHT QUALIFICATION OF THE 1.8 KW MR-509 HYDRAZINE ARCJET SYSTEM; R. D. Smith, C. R. Roberts, and R. S. Aadland, PRIMEX Aerospace Company, Redmond, WA, USA; D. A. Lichtin and K. Davies, Lockheed Martin Corporation

1997-082: FLIGHT QUALIFICATION OF THE 2.2 KW MR-510 HYDRAZINE ARCJET SYSTEM; R. D. Smith, R. S. Aadland, and C. R. Roberts, PRIMEZ Aerospace Company, Redmond, WA, USA; D. A. Lichtin, Lockheed Martin Corporation

1997-084: NUMERICAL SIMULATION OF A NONEDQUILIBRIUM PLASMA FLOW IN A NITROGEN ARCJET THRUSTER USING A THREE-TEMPERATURE KINETIC MODEL; Shigeru Kuchi-ishi and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-81, Japan

1997-085: GRAPHITE NOZZLE PERFORMANCE INVESTIGATIONS WITH HIGH POWER ARCJETS; Martin Riehle, Helmut L. Kurtz, Frank Hammer and Monika Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1997-087: SPECTROSCOPIC MEASUREMENT AND NUMERICAL ANALYSIS OF MEDIUM-POWER HYDROGEN/NITROGEN-MIXTURE ARCJET FLOWFIELDS; H. Tahara, T. Yonezawa, Y. Andoh, K. Onoe and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1997-088: 500-WATT ARCJET SYSTEM DEVELOPMENT AND DEMONSTRATION; Paul G. Lichon, Dennis L. Tilley, and Ron Anderson, PRIMEX Aerospace Company, Redmond, WA 98073; John M. Sankovic, NASA-Lewis Research Center, Cleveland, OH 44135

1997-089: LOW-POWER MICROWAVE ARCJET PERFORMANCE TESTING; D. Nordling and M. M. Micci, Department of Aerospace Engineering and Propulsion Engineering Research Center, The Pennsylvania State University, University Park, PA, USA

1997-090: INTEGRATED DESIGN ARCJETS FOR HIGH PERFORMANCE; G. Aston and M. B. Aston, Electric Propulsion Laboratory, Inc., Monument, CO 80132

1997-091: CENTRALIZED PULSED PLENUM GAS DELIVERY SYSTEM FOR HYDRAZINE ARCJETS; Mary M. Kriebel, Christopher H. McLean, and Ian F. Murray, TRW, Space and Technology Division, Redondo Beach, CA

1997-092: EFFECTS OF PROPELLANT FEED AND MAGNETIC FIELD ON ION THRUSTER PERFORMANCE; Haruki Takegahara, Yasushi Okawa, Takeru Ikeda, and Jun Takahashi, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Asahigaoka 6-6, Hino, Yokyo 181, Japan

1997-093: FABRICATION OF CARBON-CARBON COMPOSITE ION THRUSTER GRIDS – IMPROVEMENT OF STRUCTURAL STRENGTH; S. Kitamura and Y. Hayakawa, National Aerospace Laboratory, Chofu, Tokyo, Japan; Y. Kasai and T. Ozaki, Mitsubishi Electric Corporation, Kamakura, Kanagawa, Japan

1997-095: FACTORS AFFECTING THE BEAM DIVERGENCE OF A T5 ION ENGINE; David H. Mundy, Space Department, Defence Evaluation and Research Agency, Farnborough, Hampshire, GU14 0LX, UK

1997-096: T5 ION ENGINE PLUME ANALYSIS USING A TIME OF FLIGHT MASS SPECTROMETER; David H. Munday, Space Department, Defence Evaluation and Research Agency, Farnborough, Hampshire, GU14 0LX, UK

1997-098: SCALING OF ION THRUSTERS TO LOW POWER; Michael J. Patterson and Stanley P. Grisnik, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; George C. Soulas, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, Ohio

1997-099: DEVELOPMENT OF POWER ELECTRONICS FOR A 0.2KW-CLASS ION THRUSTER; Luis R. PiÃ±ero and Michael J. Patterson, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; Glen E. Bowers, Gilcrest Electric, Brook Park, Ohio

1997-100: ELECTRIC PROPULSION DEMONSTARTION MODULE (EPDM) FLIGHT HALL THRUSTER SYSTEM; Peter R. Lynn Jr. and Michael F. Osborn II, Naval Research Laboratory, Washington, D.C.; John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; and Leonard H. Caveny, Ballistic Missile Defence Organization, Washington, D.C.

1997-102: RHETT2/EPDM DEVELOPMENT TESTING; John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; David H. Manzella, NYMA Engineering Services Co., Lewis Research Center Group, Brook Park, Ohio; and Michael F. Osborn II, Naval Research Laboratory, Naval Center for Space Technology, Washington, D.C.

1997-103: RHETT/EPDM FLIGHT HOLLOW CATHODE; David Manzella, NYMA, Inc., Engineering Services Division, Brook Park, Ohio 44142; Michael Patterson, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135; and Michael Pastel, Gilcrest Electric and Supply Company, Brook Park, ,Ohio 44142

1997-104: RHETT/EPDM POWER PROCESSING UNIT; Peter T. Skelly and Robert J. Kay, PRIMEX Aerospace Company, Redmond, WA

1997-105: RHETT/EPDM FLIGHT XENON FLOW SYSTEM DEVELOPMENT; Michael F. Osborn II, Peter R. Lynn Jr., and Ronald L. Sutton, US Naval Research Laboratory (NRL), Washington, D.C. and Charles G. Sota, PRIMEX Aerospace Company, Redmond, WA

1997-106: RHETT/EPDM FLIGHT ANODE LAYER THRUSTER DEVELOPMENT; A. Semenkin, A. Kochergin, V. Garkusha, G. Chislov, and A. Rusakov, Central Research Institute of Machine Building (TsNIIMASH), Russia; S. Tverdokhlebov, TsNIIMASH-EXPORT; C. Sota, Teledesic Corporation, Seattle Wash.

1997-107: RHETT/EPDM PERFORMANCE CHARACTERIZATION; T. Haag, NASA Lewis Research Center and M. Osborn, Naval Research Laboratory

1997-108: RHETT2/EPDM HALL THRUSTER PROPULSION SYSTEM ELECTROMAGNETIC COMPATIBILITY EVALUATION; Charles J. Sarmiento and John M. Sankovic, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; Joseph Freitas and Peter R. Lynn, Naval Research laboratory, Naval Center for Space Technology, Washington, D.C.

1997-109: RHETT2/RPDM MAGNETIC FIELD INTEGRATION IMPACTS; John M. Sankovic and Eric J. Pencil, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; and David T. Jacobson, NYMA Engineering Services Co., Lewis Research Center Group, Brook Park, Ohio

1997-111: EXPERIMENTAL AND ANALYTICAL STUDY OF QUASI-STEADY MPD CHANNEL FLOW; K. Mitsuo, H. Tahara, H. Okutani, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1997-112: NONEQUILIBRIUM FLOW ANALYSIS OF A TWO-DIMENSIONAL MPD ARCJET; I. Funaki, K. Toki, and K. Kuriki, Institute of Space and Astronautical Science, Kanagawa, Japan

1997-113: EXPERIMENTAL AND NUMERICAL INVESTIGATION OF STEADY STATE MPD THRUSTERS; Michael Winter, Christian Boie, Monkia Auweter-Kurtz, and Helmut L. Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1997-115: APPLICATION OF ADAPTIVE NUMERICAL SCHEMES FOR MPD THRUSTER SIMULATION; C Boie, H. J. Kaeppeler, P. C. Sleziona and M. Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany

1997-116: THE INVESTIGATION OF APPLIED-FIELD MPD THRUSTERS ON THE INTERNATIONAL SPACE STATION; Monika Auweter-Kurtz, Gerd KrÃ¼lle, and Helmut Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

1997-117: PERFORMANCE OF 130 KW MPD THRUSTER WITH AN EXTERNAL MAGNETIC FIELD AND LI AS A PROPELLANT; V. B. Tikhonov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Moscow, Russia; S. A. Semenikhin, Moscow Aviation Institute, Moscow, Russia; J. R. Brophy, and J. E. Polk, Jet Propulsion Laboratory, California Institute of Technology, USA

1997-118: PLASMA FEATURES NEAR QUASISTEADY MAGNETOPLASMADYNAMIC ARCJET CATHODES; H. Tahara, N. Yamasaki, K. Mitsuo, Y. Kagaya, and T. Yoshikawa, Faculty of Engineering Science, Osaka University, Toyonaka, Osaka, Japan

1997-119: TEMPERATURE EFFECTS ON CURRENT EMISSION IN AN ARTIFICIALLY HEATED MPD CATHODE; F. Paganucci, P. Rossetti, and M. Andrenucci, Centrospazio, Via A. Gheradesca, 5-56014 Pisa, Italy

1997-120: ELECTRIC PROPULSION EXPERIMENT (EPEX) OF A REPETITIVELY PULSED MPD THRUSTER SYSTEM ONBOARD SPACE FLYER UNIT (SFU); K. Toki, Associate Professor, Y. Shimizu, Research Engineer and K. Kuriki, Professor, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229, Japan

1997-121: ON THE THRUST OF SELF-FIELD MPD THRUSTERS; Edgar Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University

1997-122: A COMPACT THRUST STAND FOR PULSED PLASMA THRUSTERS; Michael J. Wilson, Stewart S. Bushman, and Rodney L. Burton, Department of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign, Urbana, Illinois

1997-123: A SIMPLE MARX POWER SYSTEM FOR PULSED PLASMA THRUSTERS; Ivana Hrbud, M. Frank Rose, and Stephen A. Merryman, Space Power Institute, 231 Leach Center, Auburn University, AL

1997-124: DEVELOPMENT OF EQUATION-OF-STATE AND TRANSPORT PROPERTIES FOR MOLECULAR PLASMAS IN PULSED PLASMA THRUSTERS PART I: A TWO-TEMPERATURE EQUATION OF STATE FOR TEFLON; C. S. Schmahl and P. J. Turchi, The Ohio State University, Columbus, Ohio, USA

1997-125: PPT THERMAL MANAGEMENT; H. Kamhawi and P. J. Turchi, The Ohio State University, Columbus, Ohio USA

1997-126: EXPERIMENTAL INVESTIGATION OF THE LES 8/9 PULSED PLASMA THRUSTER PLUME; Robert Eckman and Nikos A. Gatsonis, Mechanical Engineering Dept., Worcester Polytechnic Institute, Worcester, MA 01609; Roger M. Myers, Primex Aerospace, Redmond, WA 98073; and Eric J. Pencil, NASA Lewis Research Center, Cleveland, OH 44135

1997-127: A PERFORMANCE COMPARISON OF PULSED PLASMA THRUSTER ELECTRODE CONFIGURATIONS; Lynn A. Arrington, NYMA, Inc., Tom W. Haag and Eric J. Pencil, NASA Lewis Research Center, and Nicole J. Meckel, Primex Aerospace, Inc.

1997-128: INVESTIGATION OF PULSED PLASMA THRUSTERS FOR SPACECRAFT ATTITUDE CONTOL; N. J. Meckel, R. J. Cassady, R. D. Osborne, W. A. Hoskins, R. M. Myers, PRIMEX Aerospace Company, Redmond, WA

1997-129: THE EXTREME CONTROL SYSTEM OF ELECTRICAL PROPULSION ENGINE MODULE ON THE BASIS OF SPT-100; Olexandre N. Petrenko and Olexandre N. Yatcina, Dnepropetrovsk State University, Institute of Physics and Technology, Naukovy Line, 13, 320625 Dnepropetrovsk-10, Ukraine

1997-130: MULTIPLE THRUSTER PROPULSION SYSTEMS INTEGRATION STUDY; A. V. Rusakov, A. V. Kochergin, A. V. Semenkin, S. O. Tverdokhlebov, and V. I. Garkusha, Central Research Institute of Machine Building (TsMIIMASH), Korolev, Moscow Region, Russia

1997-131: INVESTIGATION OF TAL OPTICAL EMISSIONS; G. F. Karabadzhak and A. V. Semenkin, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow Region, Russia; S. O. Tverdokhlebov, TsNIMMASH-EXPORT, Korolev, Moscow Region, Russia; and D. H. Manzella, NYMA Inc., NASA LeRC, OH, USA

1997-132: INVESTIGATION OF SPT-200 OPERATING CHARACTERISTICS AT POWER LEVELS UP TO 12 KW; B. Arhipov, L. Krochak, N. Maslennikov, and F. Scortecci, Experimental Design Bureau “Fakel”, Kaliningrad (regional), Russia, CENTROSPAZIO, Pisa, Italy

1997-133: COMPLETE COMPUTATIONAL MODEL OF A HALL THRUSTER FROM THE ACCELERATION CHANNEL THROUGH THE PLUME; Salma Qarnain and Daniel E. Hastings, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA

1997-134: THE PPS 1350 PROGRAM; D. Valentian and N. Maslennikov, SEP, Groupe Petite Propulsion et Equipements, Melun Villaroche, France, Fakel, Kaliningrad, Russia

1997-135: DEVELOPMENT OF A HELIUM CRYOPUMPED FACILITY TO EVALUATE HALL EFFECT THRUSTERS; Christopher H. McLean and Olaf Lesky, TRW, Space and Technology Division, Redondo Beach, CA

1997-137: ENDURANCE TEST OF MICROWAVE DISCHARGE ION THRUSTER SYSTEM FOR ASTEROID SAMPLE RETURN MISSION MUSES-C; Hitoshi Kuninaka, Shin Satori, Ikko Funaki, Yukio Shimizu, and Kyoichiro Toki, Institute of Space and Astronautical Science, Yoshinodai, Sagamihara, Kanagawa 229, Japan

1997-138: THE OPTIMISATION OF THE UK-10 ION THRUSTER EXTRACTION GRID SYSTEM; Robert A. Bond, AEA Technology plc, Culham Science and Technology Centre, Abingdon, Oxon, OX14 3DB, United Kingdom; David G. Fearn, Neil C. Wallace and David H. Mundy, Defence Evaluation and Research Agency, Farnborough, Hants, GU14 0LX, United Kingdom

1997-140: THE FLOW MODELING OF CHARGE EXCHANGE IONS IN THE ION THRUSTER; Ivan V. Gavryushin and Vladimir G. Grigoryan, Department of Spacecraft Electric Propulsion and Powerplants, Moscow State Aviation Institute, Russia, 125871 Moscow, Voloklamskoe shosse, d.4

1997-142: EFFECTS OF DISCHARGE CHAMBER CONFIGURATION ON RF PLASMA PROPERTIES; Toshiaki Iwata and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191, Japan

1997-144: ELECTRIC PROPULSION OPTIONS FOR A MAGNETOSPHERIC MAPPING MISSION; Steven Oleson, NYMA Inc., NASA Lewis Research Center, Brookpark, OH 44142; Chris Russell, University of California, Los Angeles, Institute of Geophysics and Planetary Physics, Los Angeles, CA 90095; Kurt Hack and John Riehl, NASA Lewis Research Center, Cleveland, OH 44135

1997-146: ANALYSIS OF PPT POTENTIALITIES IN SOLVING THE SATELLITE ORBIT CONTROL TASKS; V. Akimov, I. Nagel, and I. Ogloblina, Keldysh Research Center, Moscow; N. Antropov, A. Pokryshkin, G. Popov, and A. Rudikov, Research Institute of Applied Mechanics and Electrodynamics, Moscow

1997-147: POWER PLANT CONTROL SYSTEM OPERATION DURING CHANGING SPACECRAFT POSITION; Avil A. Ismailov, Leonid A. Latyshev, and Evgeniy E. Polovcev, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 125871, Russia

1997-149: RESEARCH OF PERFORMANCE OF SMALL THRUST THRUSTERS WITH A CLOSED DRIFT OF ELECTRONS; Sergey N. Kulagin, Olexandre N. Petrenko, and Andrey V. Khitko, Dnepropetrovsk State University, Naukovy Line 13, 320625 Dnepropetrovsk-10, Ukraine

1997-150: THERMAL ANALYSIS OF THE ANODE LAYER THRUSTER OPERATION; V. Garkusha, S. Semenkin, and S. Tverdokhlebov, Central Researche Institute of Machine Building, Moscow reg., Russia

1997-151: SOME RESULTS OF THE SMALL POWER SPT MODELS CREATION; Aidar B. Jakupov, Sergey A. Khartov, and Achmet M. Yakubov, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 125871, Russia

1997-152: SOME REMARKS ABOUT PUBLISHED DATA CONCERNING THE SPT-100 JET PARAMETERS DISTRIBUTION; Sergey A. Khartov, Andrey B. Nadiradze, Achmet M. Yakubov, and Yulia V. Zikeeva, Moscow State Aviation Institute (MAI), Department “Spacecraft Electric Propulsion and Powerplants”, Volokolamskoe shosse, d. 4, Moscow, 125871, Russia

1997-153: RESEARCH OF THE DYNAMIC PRESSURE DISTRIBUTION IN THE PLUME OF THE SPT; R. Y. Gnizdor, K. N. Kozubsky, A. I. Koryakin, Y. M. Lysikov, A. N. Nesterenko, and S. Y. Pridannikov, Experimental Design Bureau “Fakel”, Kaliningrad, Russia

1997-154: INVESTIGATION OF THE POSSIBILITY TO REDUCE SPT PLUME DIVERGENCE BY OPTIMIZATION OF THE MAGNETIC FIELD TOPOLOGY IN THE ACCELERATING CHANNEL; Michael Day, International Space Technology, Inc., Palo Alto, USA; Vladimir Kim, Vyacheslav Kozlov, Alexei Lazurenko, Garry Popov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, (RIAME MAI), Moscow, Russia

1997-156: COMPLEX NUMERIC ANALYSIS OF GAS-DISCHARGE CHAMBER PARAPMETERS; S. V. Kanev, L. A. Latyshev, Moscow State Aviation Institute (MAI), Volokolamskoe sh. 4, MAI, Department 208, 125871, Moscow, Russia

1997-157: INVESTIGATION OF A FULLY INTEGRATED SOLAR STATIONARY PLAZMA PROPULSION SYSTEM FOR GEOSTATIONARY ORBIT INSERTION; M. Konstantinov, V. Kim, and F. Scortecci, Moscow Aviation Institute, Russia, Research Institute of the Applied Mechanics and Electrodynamics, Russia, Centrospazio, Piza, Italy

1997-158: TRAJECTORY ANALYSIS OF ELECTRIC PROPULSION SYSTEM WITH THRUST MISALIGNMENT; M. Nakano and Y. Arakawa, The University of Tokyo, Hongo 7-3-1, Bunkyo-ku, 113, Japan

1997-159: LOW THRUST ION PROPULSION FOR ADVANCED APPLICATIONS ON SMALL SATELLITE CONSTELLATIONS; G. Matticari and G. Noci, LABEN Proel Tecnologie Division, Firenze, Italy; G. Perrotta, Alenia Aerospazio, Roma, Italy, and D. G. Fearn, DERA Space Department, Farnborough, UK

1997-160: SIMPLIFIED APPROACH FOR ASSESSMENT OF LOW-THRUST ELLIPTICAL ORBIT TRANSFERS; James E. Pollard, The Aerospace Corporation, P.O. Box 92958, M5-754, Los Angeles, CA 90009

1997-161: CONCEPT OF ELECTRODYNAMCI PROPULSION SYSTEM FOR STATION KEEPING OF LARGE SPACE STRUCTURES; V. A. Strashinksy, Central Research Institute of Machine Building, (TsNIIMASH), Korolev, Moscow Region, Russia

1997-163: PERFORMANCE CHARACTERISTICS OF A SPACE PLASMA SIMULATOR USING AN ELECTRON CYCLOTRON RESONANCE PLASMA ACCELERATOR AND ITS APPLICATIONS TO MATERIAL AND PLASMA INTERACTION RESEARCH; H. Tahara, L. Zhang, T. Yasui, and T. Yoshikawa, Faculty of Engineering Science, Osaka, University, Toyonaka, Osaka, Japan

1997-164: NON-PROPULSIVE APPLICATION OF THE TAL TECHNOLOGY; Alexander V. Semenkin, Sergey O. Tverdokhlebov, and Valerii I. Garcousha, Central Research Institute of Mashine Building (TSNIIMASH), 141070, Korolev, Moscow Region, Russia and Sergey D. Grishin, Moscow State Bauman Technical University

1997-165: HIGH POWER ABLATIVE PULSED PLASMA THRUSTER FOR TECHNOLOGY APPLICATIONS; Yu. A. Alexeev and M. N. Kazeev, RRC “Kurchatov Institute”, Institute of Nuclear Fusion, Kurchatov sq., 1, Moscow, 123182

1997-166: INTERNATIONAL SPACE STATION CATHODE LIFE TESTING; George C. Soulas and Timothy R. Sarver-Verhey, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, OH 44142

1997-167: SPACE STATION CATHODE IGNITION TEST STATUS AT 32,000 CYCLES; James S. Zakany, PE, NYMA, Inc., Brook Park, OH; Luis R. Pinero, PE, NASA Lewis Research Center, Cleveland, OH

1997-168: 28,000 HOUR XENON HOLLOW CATHODE LIFE TEST RESULTS; Timothy R. Sarver-Verhey, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, OH 44142

1997-170: SPACE STATION CATHODE DESIGN, PERFORMANCE, AND OPERATING SPECIFICATIONS; Michael J. Patterson, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio; Timothy R. Verhey, George Soulas, and James Zakany, NYMA, Inc., NASA Lewis Research Center Group, Brook Park, Ohio

1997-171: THE BEHAVIOR OF HOLLOW THERMO-EMISSION LANTHANUM HEXABORIDE ELEMENTS IN SPT CATHODES IN CONNECTION WITH THE MANUFACTURING METHOD; B. Arhipov, Experimental Design Bureau “Fakel”, Kaliningrad, Russia; V. Paderno, Y. Paderno, and V. Filippov, Institute for Problems of Materials of National Academy Sciences of Ukraine, Kiev, Ukraine

1997-173: EFFECTS OF EXTERNAL FLOW NEAR HIGH-CURRENT HOLLOW CATHODES ON ION-ENERGY DISTRIBUTIONS; Ikuya Kameyama and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1997-175: DEVELOPMENT AND RESEARCH OF HEATERLESS CATHODE-NEUTRALIZER FOR LINEAR HALL THRUSTERS (LHD) AND PLASMA ION THRUSTERS (PIT); B. A. Arkhipov, EDB “Fakel”, Kaliningrad, Russia

1997-176: MAKING FULLERENE ION ENGINES WORK; M. W. Crofton and B. B. Brady, Technology Operations, Mechanics & Materials Technology Center, The Aerospace Corporation, P.O. Box 92957, Los Angeles, California 90009

1997-178: EARTH’S MAGNETIC FIELD EFFECT UPON PLASMA PLUMES EXPANSION; A. G. Korsun, E. M. Tverdokhlebova, and F. F. Gabdullin, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow region, Russia

1997-179: COMPUTATIONAL MODELING OF EXPANDING PLASMA PLUMES IN SPACE USING A PIC-DSMC ALGORITHM; David Y. Oh and Daniel E. Hastings, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA

1997-180: A NUMERICAL MODEL OF THRUSTER-EXHAUST PLUMES; Ikuya Kameyama, Jeffrey M. Monheiser, and Paul J. Wilbur, Colorado State University, Fort Collins, CO 80523

1997-181: ION THRUSTER PLUME PLASMA INTERACTIONS IN THE SOLAR WIND, Joseph Wang, Jet Propulsion Laboratory, California Institute of Technology, Pasadena

1997-182: HYBRID MONTE CARLO – PARTICLE-IN-CELL SIMULATION OF AN ION THRUSTER PLUME; Douglas B. VanGilder, Gabriel I. Font, and Iain D. Boyd, Cornell University, Ithaca, NY 14853, USA

1997-183: THE EXPRESS/T-160E SPACE FLIGHT TEST PROGRAM; J. K. Koester and C. E. Lazarovici, Space Power Incorporated, San Jose, CA; J. M. Sankovic, NASA Lewis Research Center, Cleveland, OH; G. A. Herbert, Schafer Corporation, Arlington, VA; V. A. Petrosov and V. I. Baranov, Keldysh Research Center, Moscow, Russia; A. Romashko and V. Petrusevitch, NPO-PM, Krasnoyarsk, Russia

1997-184: CONSTRAINTS ON ELECTRICAL POWER SYSTEM DESIGN FROM IPS OPERATION; L. Croci, P. Galantini, and A. Trivulzio, FIAR S.p.A. Space Division – a Finmeccanica Company, Via Montefeltro, 8-20126 Milano; H. Bassner, Daimler-Benz Aerospace AG, Space Infrastructure, Postfach 801168-81663 Munich, Germany

1997-185: NUMERICAL THERMAL MODEL OF A 30-CM NSTAR ION THRUSTER; Jon Van Noord and Alec Gallimore, University of Michigan, Ann Arbor, MI 48109-2118; and Vincent K. Rawlin, National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH 44135

1997-186: FEEP THRUSTER PERFORMANCE AT HIGH BACKGROUND PRESSURE; Angelo Genovese, Salvo Marcuccio, Davide Dal Pozzo, and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, 56014 Ospedaletto, Pisa, Italy

1997-189: AN EVALUATION OF HOLLOW CATHODE SCALING TO VERY LOW POWER AND FLOW RATE; Matthew T. Domonkos and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), The University of Michigan, Ann Arbor, MI 48109; and Michael J. Patterson, NASA Lewis Research Center, Cleveland, OH 44135

1997 FILE DIRECTORY

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1999 INDEX

1999-001: ELECTRIC PROPULSION ACTIVITIES IN U.S. INDUSTRY; Dr. Frank M. Curran, Schafer Corportation, Arlington, VA, USA

1999-002: EUROPEAN ELECTRIC PROPULSION ACTIVITIES AND PROGRAMMES; G. Saccoccia, ESA Technical and Operational Support Directorate, ESTEC, Noordwijk, The Netherlands

1999-003: AN OVERVIEW OF CURRENT NASA ACTIVITIES IN ELECTRIC PROPULSION TECHNOLOGY; John M. Sankovic and John W. Dunning Jr., National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, Ohio USA, 44135

1999-004: MODERN TRENDS OF ELECTRIC PROPULSION ACTIVITIY IN RUSSIA; Vladimir Kim, Garry Popov, and Victor Tikhonov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), Moscow, Russia; Valery Garkusha, The Central Institute of Mashinebuilding, Korolev of Moscow Region, Russia; Vyacheslav Murashko, Design Bureau Fakel, Kaliningrad (obl.), Russia

1999-006: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; Hirokazu Tahara, Area of Aerospace Engineering, Division of Mechanical Science, Department of Systems and Human Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

1999-007: RESEARCH AND DEVELOPMENT ON PLASMA THRUSTERS IN FRANCE; Anne Cadiou, CNES 18 Avenue Edouard Belin 31401 TOULOUSE CEDEX 4, France; Michael Lyszyk, SNECMA, Division SEP Aerodrome de Melun-Villaroche 77550 MOISSY-CRAMAYEL, France; Michael Dudeck, CNRS Laboratoire d’ Aerothermique 4 ter route des Gardes 92190 Meudon, France

1999-008: ELECTRIC PROPULSION ACTIVITIES AT ONERA; Nelly Dorval, Jean Bonnet, Jean-Pierre Marque, and Daniel Pigache, ONERA – Department de Mesures Physiques, 29 Avenue de la Division Leclerc – 92320 Chatillon, France

1999-010: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN CSSAR; Hanji Wu and Anjie Li, Center for Space Science & Applied Research, Chinese Academy of Sciences, Beijing 100080, P. R. China

1999-012: AN EXPERIMENTAL RESEARCH ON A CW CO2 LASER THRUSTER; Kazuhiro Toyoda, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Tokyo, Hongo, Bunkyo-ku, 113-8656, Tokyo, Japan

1999-013: THEORETICAL DESIGN OF A GIGAWATT-LEVEL MPD PLASMA SOURCE FOR STUDIES OF MAGNETIC-NOZZLE CONFINEMENT IN FUSION PROPULSION SYSTEMS; Peter J. Turchi and Pavlos G. Mikellides, Department of Aerospace Engineering, Applied Mechanics and Aviation, The Ohio State University, Columbus, Ohio, USA

1999-014: RESEARCH ON COLLOID THRUSTERS; Manuel Martinez-Sanchex, J. Fernandez de la Mora, V. Hruby, M. Gamero-Castano and V. Khayms

1999-017: PLASMA DIAGNOSTICS OF LASER-SUSTAINED PLASMA IN A CW LASER THRUSTER; Satoshi Hosoda, Kazuhiro Toyoda, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-018: CFD ANALYSIS OF PLASMA FLOW IN A LASER THRUSTER; P. Molina-Morales, K. Komurasaki, and Y. Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-019: DEVELOPMENT OF A MHD CODE USING CIP METHOD AND ITS APPLICATION TO A LASER FUSION ROCKET; Toshifumi Kawasaki, Takanobu Muranaka and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1, Kasuga-Kouen, Kasuga, Fukuoka 816-8580, Japan

1999-020: ANALYSIS OF PLASMA BEHAVIOR FOR A MAGNETIC THRUST CHAMBER OF LASER FUSION ROCKET BY USING 3D HYBRID CODE; Hideyuki Uchimura, Takanobu Muranaka and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-Kouen, Fukuoka 816-8560, Japan

1999-021: RESEARCHES FOR REACHING MINIMUM THRUSTS IN REGULATES MONOFUEL MICRO LIQUID PROPULSION THRUSTERS; N. M. Vertakov, EDB “FAKEL”, Kaliningrad, Russia

1999-022: XENON RESISTOJET DESIGN AND DEVELOPMENT; Kent T. Chojnacki and Robert Reinicke, Space Products Division, Moog, Inc., East Aurora, NY 14052-0018

1999-023: EXPERIMENTS OF ARC-HEATED PLASMA FLOW CHARACTERISTICS; Makoto Hirakawa, Keisuke Ichige, Ken-ichi Abe, and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-024: THE OUTPUT PARAMETERS AND ANGULAR PLUME CHARACTERISCTICS OF LOW-POWER HALL THRUSTERS; M. B. Belikov, O. A. Gorshkov, and R. N. Rizakhanov, Keldysh Research Center, 8 Onezhskaya, Moscow 125438, Russia

1999-025: DETECTION OF ABLATOR SPALLATION PHENOMENA AT ARC WIND TUNNEL TESTS; Toshinari Yoshinaka, Masahito Mizuno, and Yoshiki Morino, National Space Development Agency of Japan (NASDA), 2-1-1 Sengen, Tsukuba, Ibaraki, 305, Japan

1999-026: PLASMA JET ENHANCED COMBUSTION OF HYDROGEN IN SUPERSONIC AIR FLOW; Toichi Niyama, Hiroshi Itoh, and Toshio Nagashima, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-028: DEVELOPMENT OF AN ENGINEERING MODEL OF 1 KW HYDRAZINE ARCJET SYSTEM; H. Suzuki, M. Ishii, T. Ohtsuka, K. Kato, K. Uematsu and S. Morimoto, Ishikawajima-Harima Heavy Industries Co., Ltd., 2-2-1, Otemachi, Chiyoda-ku, Tokyo, 100-8182, Japan; T. Yoshikawa and K. Onoe, Osaka University, 1-12, Machikaneyama-cho, Toyonaka-shi, Osaka, Japan

1999-029: THERMO-CHEMICAL NONEQUILIBRIUM MODELING FOR A NITROGEN ARCJET THRUSTER; Shigeru Kuchi-ishi and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-030: FLOW ESTABLISHMENT OVER CONSTRUCTOR IN ARCJET OPERATION; A. Sasoh, Shock Wave Research Center, Institute of Fluid Science, Tohoku University, 2-1-1 Katahira, Aoba-ku, Sendai 980-8577, Japan

1999-031: OBSERVATION AND MODELING OF DC ARCJET FLOWFIELD IN STABLE OPERATION; Hironori Sahara and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; and Kyoichi Kuriki, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Japan, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan

1999-032: PERFORMANCE EVALUATION OF A SMALL SIZE ARCJET THRUSTER; Keisuke Ichige, Makoto Hirakawa, Hisashi Kihara, Ken-ichi Abe, and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; Masashi Matsumoto, Fluid Dynamics & Combustion Department, Research Institute, Ishikawajima-Harima Heavy Ind. Co. Ltd., Yokohama, 235-0031, Japan

1999-033: THRUST PERFORMANCE AND THERMAL ANALYSIS OF A LOW POWER ARCJET THRUSTER; Shinsuke Hiratsuka, Ken-ichi Onoe, Hirokazu Tahara, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan; Hiroshi Suzuki and Kazuo Uematsu, Ishikawajima-Harima Heavy Industries Co., Ltd, 3-1-15, Toyosu, Koto, Tokyo 135-8732, Japan

1999-034: TWO-DIMENSIONAL NUMERICAL SIMULATIONS OF A CESIUM SEEDED HYDROGEN ARCJET; Darrel Robertson and Manuel Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts

1999-036: A STUDY ON NOZZLE FLOW QUALITY OF LOW POWER ARCJET THRUSTER FOR IMPROVEMENT OF PROPULSION EFFICIENCY; S. Aso, K. Takayanagi, S. Kuti-Ishi, and K. Sugimoto, Department of Aeronautics and Astronautics, Kyushu University

1999-037: EFFECT OF STRONG MAGNETIC FIELD ON PLASMA JET AT A LOW PRESSURE; Kazuo Koike, Eiji Konno, Norifumi Ono, and Ryoichiro Oshima, Department of Mechanical Engineering, Tohoku Gakuin University, 13-1, Chuo-1, Tagajo, Miyagi, 985-8537, Japan

1999-038: CONTAMINATION ANALYSIS FROM THE ESEX 26 KW AMMONIA ARCJET FLIGHT EXPERIMENT; G. G. Spanjers, J. H. Schiling, S. F. Engelman, M. J. Dulligan, and D. R. Bromaghim, Propulsion Directorate, Air Force Research Laboratory, Edwards AFB, CA

1999-039: DIRECT-CURRENT ARCJET PLASMA FEATURE USING AMMONIA AND MIXTURE OF NITROGEN AND HYDROGEN; Sakae Mitsufuji, Hirokazu Tahara, Tomoki Taniguchi, Ken-ichi Onoe, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-040: SIMULTANEOUS MEASUREMENTS OF PLUME TEMPERATURE AND ATOMIC NUMBER DENSITY WITH OPTICAL ABSORPTION TOMOGRAPHY; F. Y. Zhang, T. Fujiwara, T. Miyasaka, and J. Harada, Nagoya University, Nagoya, 464-8603, Japan; K. Komurasaki, University of Tokyo, Tokyo, 113-8656, Japan

1999-041: PLUME MASS SPECTROMETRY AND CALORIMETRY WITH A HYDRAZINE ARCJET THRUSTER; James E. Pollard, The Aerospace Corporation, P.O. Box 92957 – 5/754, Los Angeles, CA 90009, USA; Ideo Masuda, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki, 304-8505, Japan; Yoshifumi Gotoh, Mitsubishi Electric Corporation, 325, Kamimachiya Kamakura, Kanagawa 247, Japan

1999-042: NEAR-FIELD MEASUREMENT AND MODELING RESULTS FOR A FLIGHT-TYPE ARCJET: NH MOLECULE; Mark W. Crofton and Teresa A. Moore, Technology Operations, The Aerospace Corporation, M5/754, P.O. Box 92957, Los Angeles, California, 90009, U.S.A.; Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan, 48109-2140, U.S.A.; Ideo Masuda, DRTS Project Team, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki, 305-8505, Japan; Yoshifumi Gotoh, Space Systems Department, Mitsubishi Electric Corporation, 325, Kamimachiya Kamakura, Kanagawa 247, Japan

1999-043: A SIMPLIFIED MODEL FOR THE PREDICTION OF ARCJET PLUMES; Duane A. Nelson, The Aerospace Corporation, P.O. Box 92957, Los Angeles, CA 90009-2957, USA; Yoshifumi Gotoh, Mitsubishi Electric Corp., Kamakura Works, Japan; Ideo Masuda, National Space Development Agency of Japan, Tsukuba, Ibaraski, Japan

1999-044: AN APPROACH TO ARCJET THRUSTER COMPUTATIONS FOR FASTER CONVERGENCE; Shigeru Kuchi-ishi and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-045: SIMPLE ESTIMATION OF THE PERFORMANCE OF A LOW POWER ARCJET THRUSTER WITH DIATOMIC GAS AS PROPELLANT; Masahiko Hayatani and Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan

1999-046: PRELIMINARY TEST OF A LOW-POWER DC ARCJET ANODE; I. Funaki, K. Toki, and Y. Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Y. Suwana and H. Takegahara, Tokyo Metropolitan Institute of Technology, 6-6 Asahigaoka, Hino, Tokyo 191-0065, Japan; S. Satori, Hokkaido Institute of Technology, 15-4-1 Macdananayo, Teine, Sapporo, Hokkaido, 006-8585, Japan

1999-047: FLOWFIELD OBSERVATION USING A TWO-DIMENSION-LIKE LOW-POWER DC ARCJET; Hironori Sahara, Satoshi Hosoda, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Yasuyuki Suwama, Kyoichi Kuriki and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, Japan, 6-6, Asahigaoka, Hino, Toyko 191-0065, Japan; Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-048: NEAR-FIELD MEASUREMENT AND MODELIG RESULTS FOR A FLIGHT-TYPE ARCJET: HYDROGEN ATOM; Mark W. Crofton and Teresa A. Moore, Technology Operations, The Aerospace Corporation, M5/754, P.O. Box 92957, Los Angeles, California, 90009, U.S.A.; Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, 1320 Beal Avenue, Ann Arbor, Michigan, 48109-2140, U.S.A.; Ideo Masuda, DRTS Project Team, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki, 305-8505, Japan; Yoshifumi Gotoh, Space Systems Department, Mitsubishi Electric Corporation, 325, Kamimachiya Kamakura, kanagawa 247, Japan

1999-049: PERFORMANCE IMPROVEMENT OF VERY LOW POWER ARCJETS; Hideyuki Horisawa, Department of Precision Mechanics, Tokai University, 1117 Kitakaname, Hiratsuka-shi, Kanagawa 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, and Nara Textile Inc., 4-19-4 Nakahara, Isogo, Yokohama 235-0036, Japan

1999-050: OPERATIONAL CHARACTERISTICS OF 1 KW HYDRAZINE DC ARCJET SYSTEM; Masahiro Ishii, Koichiro Kato, and Hiroshi Suzuki, Ishikawajima-Harima Heavy Industries Co., Ltd., 299, Tnogaya, Mizuho-machi, Nishitama-gun, Tokyo 190-1297, Japan; Ken-ichi Kajiwara and Akito Hattori, National Space Development Agency of Japan, 2-4-1, Hamamatsu-cho, Minato-ku, Tokyo 105-6126, japan

1999-051: PLASMIC PROPULSION SYSTEM ON S.T.E.N.T.O.R. Program, Thierry Grassin and Luc Petitjean, Alcatel Space Industries, CNES, Centre Spatial de Toulouse

1999-053: DEVELOPMENT OF XENON ION ENGINE SUBSYSTEM FOR ETS-VIII, Eiji Nishida, Toshiyuki Ozaki, Yukikazu Kasai, and Yoshifumi Gotoh, 325 Kamimachiya, Kamakura, Kanagawa, Japan 247-8520, Mitsubishi Electric Corporation (MELCO); Masafumi Ikeda and Ken-ichi Kajiwara, National Space Development Agency of Japan (NASDA)

1999-054: ELECTRIC PROPULSION SYSTEM FOR ARTEMIS; Rainer Killinger, Helmut Bassner, and Gunther Kienlein, Space Infrastructure; Johann Muller, Dornier Satellite Systems, DaimlerChrysler Aerospace AG, Postfach 80 11 69, D-816633 Munchen, Germany

1999-055: XENON GROUND SUPPORT EQUIPMENT FOR PLASMIC PROPULSION SYSTEM; Patrick Bravais, Alain Teissier, and Frederic Ribas, Air Liquide, DTA; Olivier Dulau, Eric Montfort, and Thierry Grassin, Alcatel Space Industries

1999-056: XENON LOADING DEVICE FOR MUSES-C ION ENGINE SYSTEM; Yukio Shimizu, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-057: ION THRUSTER POINTING MECHANISM (ITAM) FOR ARTEMIS: DESIGN & PERFORMANCE; Manfred Falkner, Austrian Aerospace, Stachegasse 16, A-1120 Vienna, Austria

1999-058: PLASMIC PROPULSION LIFETEST; Nunzia Mattei (ASPI), Xavier Ragot (ASPI), Pierre Dumazert (SNECMA), Eric Klinger (SNECMA), Alcatel Space Industries, 100 Bvd du Midi 06150, Cannes la Bocca Cedex, France, SNECMA division SEP Aerodome de Melun-Villaroche, 77055 Moissy Cramayel Cedex, France

1999-059: POWER PROCESSING UNIT FOR STATIONARY PLASMA THRUSTER; H. Declercq, E. Bourguignon, and T. Scalais, Alcatel ETCA, B.P. 4008, B-6000 Charleroi (BELGIUM); J. J. Digoin, Alcatel Space Industries, BP 99, 06322 Cannes La Bocca Cedex, France

1999-060: PERFORMANCE OF HIGH POWER CAPACITORS FOR PULSED PLASMA THRUSTER APPLICATIONS; Zheng Chen and Henry Brandhorst, Space Power Institute, 231 Leach Center, Auburn University, AL 36849-5320, USA

1999-061: DC-DC CONVERTER FOR HALL THRUSTER PLASMA DISCHARGE; V. Hruby, W. Connolly, J. Monheiser, B. Pote, and C. Freeman, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

1999-064: A DIGITAL XENON FLOW CONTROLLER BASED ON ChEMS TECHNOLOGY; Joe Cardin, Director, Business Development, Ben Otsap, Chief Engineer, VACCO Industries, South El Monte, CA 91733

1999-065: DEVELOPMENT OF AN ION THRUSTER CONTROL UNIT FOR THE MUSES-C MISSION; Kazutaka Nishiyama and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-066: DEVELOPMENT OF A “SMART” POWER PROCESSING UNIT FOR HALL EFFECT THRUSTERS; J. Dickens and M. Kristiansen, Texas Tech University, Electrical Engineering Department, Lubbock, TX 79409-3102

1999-069: ONE MILLINEWTON FEEP THRUSTER TESTS; Salvo Marcuccio, Marco Saviozzi, Fabrizio Rugo, and Mariano Andrenucci, Centrospazio, 56014 Ospedaletto, Pisa, Italy

1999-070: BACKFLOW CONTAMINATION OF INDIUM-METAL ION EMITTERS (LMIE): NUMERICAL SIMULATIONS; M. Tajmar, Vienna University of Technology, Institut fur Angewandte Elektronik und Quantenelektronik, GuBhausstrasse 27-29, A-1040 Vienna, Austria; F. Rudenauer and M. Fehringer, Austrian Research Center, A-2444, Seibersdorf, Austria

1999-071: EXPERIMENTAL PERFORMANCE OF A LOW POWER NEUTRALIZER FOR A MICRONEWTON FEEP THRUSTER; Salvo Marcuccio, Gabriele Lorenzi, and Mariano Andrenucci, Centrospazio, 56014 Ospedaletto, Pisa, Italy

1999-072: MICRONEWTON INDIUM ION THRUSTERS; Michael Fehringer, Friedrich Rudenauer, and Wolfgang Steiger, Austrian Research Centre Seibersdorf, A-2444 Seibersdorf

1999-073: PLUME STUDY OF MULTIMODE THRUSTER SPT-140; K. Kozubsky, S. Kudriavtzev, and S. Pridannikov, Fakel, Moskovsky pr. 181, Kaliningrad, 236001, Russia

1999-074: SPT100 PLASMA JET EFFECTS ON GEOSTATIONARY SATELLITE COMMUNICATIONS; Claude Berthou and Denis Pogarieloff, Alcatel Space Industries, 100 Bd du Midi 06156 Cannes la Bocca Cedex, France

1999-076: ANALYSIS OF COLLISION PHENOMENA IN HALL THRUSTER PLUMES; Douglas B. VanGilder and Iain D. Boyd, Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY 14853, U.S.A.

1999-078: CHARACTERIZATION OF THE INTERNAL PLASMA STRUCTURE OF A 5 KW HALL THRUSTER; James M. Haas and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

1999-079: EXPERIMENTAL AND NUMERICAL STUDY OF DISTURBANCE FORCES INDUCED BY A SPT100 PLASMA JET; Stephane d’Halewyn, Claude Berthou, Danielle Borie (Alcatel Space Industries), Pascal Lasgorceix, Stephane Bechu, Alain Hauser (Laboratoire d’Aerothermique – CNRS Orleans), Alcatel Space Industries 100 Bd du Midi 06156 Cannes la Bocca Cedex, France

1999-080: PERFORMANCE OF AN 8 KW HALL THRUSTER; B. Pote, V. Hruby, and J. Monheiser, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023, USA

1999-082: EXPERIMENTAL INVESTIGATION NEGATIVE IONS IN SPT THRUSTER CHANNEL; A. I. Bugrova, A. V. Desiatskov, A. I. Morosov, and V. K. Kharchevnikov, MIREA, Russia

1999-083: INVESTIGATION OF XENON ION SPUTTERING OF ONE CERAMIC MATERIAL USED IN SPT DISCHARGE CHAMBER; Y. Garnier, V. Viel, and J-F. Roussel, ONERA-DESP, 2 avenue Belin, BP 4025, 31055 Toulouse Cedex, France; D. Pagnon, L. Magne, and M. Touzeau, LPGP – Universite Paris-Sud, Bat, 210, 91405 Orsay Cedex, France

1999-084: INVESTIGATION OF THE STATIONARY PLASMA THRUSTER (SPT) OUTGASSING AND ITS THERMAL STATE IMPACT ON THRUSTER PERFORMANCE VARIATION IN TIME; Vladimir Kim, Vyacheslav Kozlov, Garry Popov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 4, Volokolamskoe shosse, Moscow, 125810, Russia; Konstantin Kozubsky, Design Bureau Fakel, 181, Moskovski Prospect, Kaliningrad, 236001, Russia; and Michal Lyszyk, Societe Europeenne de Propulsion (SEP), division of SNECMA, Aerodrome de Melun-Villaroche-F77550, Moissy-Cramayel-France

1999-086: PERFORMANCE OF STATIONARY PLASMA THRUSTER PPS1350 AND ITS QUALIFICATION STATUS IN RUSSIA; V. Gopantchuk, K. Kozubsky, N. Maslennikov, and S. Pridannikov, Fakel, Moscovsky pr. 181, Kaliningrad 236001, Russia

1999-087: PPS 1350 QUALIFICATIONS STATUS; M. Lyszyk, E. Klinger, O. Secheresse, JP. Bugeat and D. Valentian, SNECMA, Division SEP, Aerodrome de Melun-Villaroche, Moissy-Cramayel, France; A. Cadiou, Th. Beltan and C. Gelas, CNES, Centre Spatial de Toulouse, 18 Avenue Edouard Belin, Toulouse, France

1999-090: PERFORMANCE AND QUALIFCATION STATUS OF MULTIMODE STATIONARY PLASMA THRUSTER SPT-140; R. Gnizdor, K. Kozubsky, N. Maslennikov, V. Murashko, and S. Pridannikov, Fakel, Moscovsky pr. 181, Kaliningrad 236001, Russia; V. Kim, RIAME, Volokolamskoe sh. 4, Moscow 125871, Russia

1999-092: LOW POWER, HALL THRUSTER PROPULSION SYSTEM; V. Hruby, J. Monheiser, B. Pote, C. Freeman, and W. Connolly, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

1999-094: THE OUTPUT PARAMETERS AND ANGULAR PLUME CHARACTERISTICS OF LOW-POWER HALL THRUSTERS; M. B. Belikov, O. A. Gorshkov, and R. N. Rizakhanov, Keldysh Research Center, 8 Onezhskaya, Moscow 125438, Russia

1999-097: NUMERICAL SIMULATION OF FACILITY EFFECTS ON HALL THRUSTER PERFORMANCE, John Michael Fife and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts

1999-098: COMPUTATION OF HALL THRUSTER PERFORMANCE; L. Garrigues and J.P. Boeuf, Centre de Physique des Plasmas et Applications de Toulouse, Universite Paul Sabatier, 118 route de Narbonne, 31062 Toulouse Cedex 4, France; I. D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA

1999-099: FUNDATMENTAL DESIGN OF HIGHLY EFFECTIVE HALL THRUSTERS; Yuri M. Yashnov, Consultant, Moscow, Russia; J. Kent Koester, John B. McVey, and Edward J. Britt, Space Power, Inc., 1253 Reamwood Ave., Sunnyvale, CA 94089

1999-100: PARTICLE-IN-CELL MODELING OF THRUSTER WITH ANODE LAYER (TAL); James J. Szabo Jr., Manuel Martinez-Sanchez, and Oleg Batishchev, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139

1999-101: SEGMENTED ELECTRODE HALL THRUSTER OPERATION IN SINGLE AND TWO STAGE REGIMES; N. J. Fisch, Y. Raitses, A. A. Litvak, and L. A. Dorf, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ 08540

1999-102: CHARACTERISTICS OF THE SPT100-ML COMPARISONS BETWEEN EXPERIMENTS AND MODELS; L. Garrigues and J. P. Boeuf, Centre de Physique des Plasmas et Applications de Toulouse, Universite Paul Sabatier, 118 route de Narbonne, 31062 Toulouse Cedex 4, France; C. Perot, N. Gascon, S. Bechu, P. Lasgorceix, and M. Dudeck, Laboratoire d’Aerothermique, 2 rue du crital, 45100 Orleans, France

1999-103: THE PRINCIPLE OF CURRENT MAXIMALITY FOR DISCHARGE SIMULATION IN ACD; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, and A. I. Vasin, Keldysh Research Center, Onezhskaya 8, Moscow, 12548, Russia

1999-104: CHARACTERIZATION OF FMT-2 DISCHARGE CATHODE PLUE; George J. Williams Jr., Timothy B. Smith, Travis A. Patrick, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, 1919 Green Rd., Ann Arbor, MI 48105, USA

1999-105: LINEAR 1-D ANALYSIS OF ASCILLATIONS IN HALL THRUSTERS; Reid Noguchi, Graduate Student, MIT, Cambridge, MA, USA; Manuel Martinez-Sanchez, Professor of Aeronautics/Astronautics, MIT, Cambridge, MA, USA; and Eduardo Ahedo, Polytechnical University of Madrid, Spain

1999-106: MEMBRANE OSCILLATIONS IN SPT CHANNEL; A. I. Bugrova, A. S. Lipatov, A. I. Morosov, and V. K. Kharchevnikov, MIREA, Russia

1999-108: STEADY ACCELERATION IN THE HALL THRUSTER; A. Cohen-Zur, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; A. Fruchtman, Center for Technological Education Holonn, 52 Golomb St., P.O. Box 305 Holon 58102, Israel; and J. Ashkenazy, Propulsion Pysics Laboratory, Soreq NRC, Yavne 81800, Israel

1999-112: ELECTRON CONDUCTIVITY IN ACD; V. I. Baranov, Yu. S. Nazarenko, V. A. Petrosov, and A. I. Vasin, Keldysh Research Center, Onezhskaya 8, Moscow, 125438, Russia

1999-113: DEVELOPMENT OF A 45-DEGREE PARALLEL-PLATE ELECTROSTATIC ENERGY ANALYZER FOR HALL THRUSTER PLUME STUDIES: PRELIMINARY DATA; Richard R. Hofer, James M. Haas, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), Department of Aerospace Engineering, College of Engineering, University of Michigan, Ann Arbor, MI 48109, USA

1999-114: COMPUTATIONAL MODELING OF PLASMA PLUMES IN A VACUUM TANK; Bernard Asare, MIT, Cambridge, MA, USA; and Manuel Martinez-Sanchez, Aeronautics/Astronautics, MIT, Cambridge, MA, USA

1999-117: INVESTIGATION OF POSSIBILITY TO INCREASE THE TRUSTIER EFFICIENCY, DISCHARGE EFFICIENCY AND THE SPD LIFE-TIME BY INFLUENCE TO THE SPEED OF THE NEUTRAL PROPELLANT GAS STREAM; A. V. Loyan and S. A. Oghienko. Scientific & Technological Center of Space Power & Engines at State Aerospace University nm. N. E. Gukovsky “KhAI”, (STC SPE “KhAI”) Kharkov, 310070, Chcalova St., 17, Ukraine

1999-118: STUDY OF PLASMA DYNAMICS IN THE VARIABLE SECTION CHANNEL OF STATIONARY PLASMA THRUSTER; Boris Arhipov, Design Bureau Fakel, Kaliningrad (obl.), Russia; Elena Goghaya, Kaliningrad State University, Kaliningrad (obl.), Russia; and Nikolay Nikulin, Kaliningrad State University, Kaliningrad (obl), Russia

1999-119: INVESTIGATION OF THE STATIONARY PLASMA THRUSTER SCALE IMPACT ON THE ELECTRIC FILTER PARAMETER CHOICE; Vladimir Kim, Vyacheslav Kozlov, Garry Popov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 4, Volokolamskoe shosse, Moscow, 125810, Russia

1999-121: RESEARCH AND DEVELOPMENT OF HALL EFFECT THRUSTERS AT OSAKA UNIVERSITY; Daisuke Goto, Hirokazu Tahara, Yohei Nikai, Toshiaki Yasui, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Service, Graduate School of Engineering Science, Osaka University, 103, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-123: THE OPTIMAL CONTROL OF THRUST VECTOR OF HALL-THRUSTERS; Yuri M. Yashnov, Consultant, Moscow, Russia; J. Kent Koester, John B. McVey, and Edward J. Britt, Space Power Inc., 1253 Reamwood Ave., Sunnyvale, CA, 94089

1999-124: AN EXPERIMENTAL INVESTIGATION OF THE HOLLOW CATHODES FOR LOW-POWER ION THRUSTER; O. A. Gorshkov and V. A. Muravlev, Keldysh Research Center, 8/10, Onezhskaya, Moscow, 12548, Russia

1999-125: THE GENERATION OF HIGH ENERGY IONS IN HOLLOW CATHODE DISCHARGES; Stephen W. Patterson, Plasma Physics Group, Imperial College, London, UK; David G. Fearn, Space Department, Defence Evaluation and Research Agency, Farnborough,, Hants, UK

1999-126: SCENARIO FOR HOLLOW CATHODE END-OF-LIFE; Timothy R. Sarver-Verhey, Dynacs Engineering Co., Inc., NASA Glenn Research Center Group, 2001 Aerospace Parkway, Brook Park, OH 44142

1999-127: PHYSIC-MATHEMATICS MODEL OF A SELF-HEATED HOLLOW CATHODE ELECTRIC DISCHARGE EVOLUTION; Sergiy A. Lobov and Andriy V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-128: HEAT BALANCE IN A NEUTRALIZER CATHODE OF STATIONARY PLASMA THRUSTER (SPT); Dr. B. Arkhipov, EDB FAKEL, Moskovski pr. 181, Kaliningrad 236000, Russia

1999-131: RESEARCHING OF RUNNING-IN, STARTING, TRANSITION THERMAL PROCESSES OF SELF-HEATED HOLLOW CATHODE IN ELECTRIC CURRENT RANGE FROM 5 UP TO 25 A; Sergiy A. Lobov and Andriy V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-133: THE COMPATIBILITY OF HOLLOW CATHODE CHARACTERISTICS WITH A VARIETY OF ION THRUSTER DESIGNS; David G. Fearn, Space Department, Defence Evaluation and Research Agency, Farnborough, Hants, GU14 0LX, UK; Stephen W. Patterson, Plasma Physics Group, Imperial College, London, SW7 2BZ, UK

1999-135: INVESTIGATION OF SELF-HEATE HOLLOW CATHODES OPERATION POSSIBILITY IN WATER MOIST STREAM OF HIGH-PRESSURE CONDITION; N. N. Koshelev and A. V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine; V. P. Sklarov and A. A. Tarelin, Machine Problem Institute of Ukrainian Engineer Sciences Academy, ‘MPI UESA”, Ukraine

1999-137: EXPERIMENTAL INVESTIGATION OF A GAS PROPELLANT CONSUMPTION OSCILLATION WHEN SELF-HEATED HOLLOW CATHODE IS STARTING FROM A COLD STATE; Nikolay N. Koshelev, Sergiy A. Lobov, and Andriy V. Loyan, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-138: ANALYZE OF GAS PROPELLANT CONSUMPTION OSCILLATION WHEN THE SELF-HEATED HOLLOW CATHODE IS STARTING “COLD” STATE; Andriy V. Loyan, Scientific and Technological Center of Space Power and Engines at Kharkov Aviation Institute, 17, Chkalova st., Kharkov, 310070, Ukraine

1999-139: DEVELOPMENT STATUS OF A MICROWAVE ION ENGINE SYSTEM FOR THE MUSES-C MISSION; Kyoichiro Toki, Hitoshi Kuninaka, Ikkoh Funaki, Kazutaka Nishiyama, and Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-140: DEVELOPMENT OF AN RF-ION THRUSTER FOR COMMERCIAL APPLICATION; Rainer Killinger and Helmut Bassner, Space Infrastructure; Johann Muller, Dornier Satellite Systems, DaimlerChrysler Aerospace AG, Postfach 80 11 69, D-816633 Munchen, Germany

1999-141: ROLE OF MAGNETIC FIELD IN KAUFMAN TYPE ELECTROSTATIC ION THRUSTERS; A. K. Malik, Plasma Physics, Blackett Laboratory, Imperial College, London, SW7 2AZ

1999-142: 1000-HOUR TEST OF A 35-CM DIAMETER XENON ION THRUSTER; S. Kitamura, Y. Hayakawa, and K. Miyazaki, National Aerospace Laboratory, 7-44-1 Jindaijihigashi-machi, Chofu, Tokyo 182-8522, Japan; H. Yoshida, Y. Yamamoto and K. Akai, Toshida, Y. Yamamoto and K. Akai, Toshiba Corporation, 1 Komukai, Toshiba-cho, Saiwai-ku, Kawasaski, Kanagawa 210-0863, Japan

1999-143: A XENON PROPELLANT MANAGEMENT SUB-UNIT FOR ION PROPULSION; Keith Dyer, VACCO Industries, South El Monte, CA 91733; Anthony Dien, Stanford Mu Corporation, Harbor City, CA 90710; Eiji Nishida and Yukikazu Kasai, Mitsubishi Electric Corp., Kanagawa, Japan; Masafumi Ikeda and Kenishi Kajiwara, NASDA, Japan

1999-144: BEAM INTENSTIY DISTRIBUTION OF A RING-CUSP ION THRUSTER; H. Yoshida, Y. Yamamoto, and K. Akai, Toshiba Corporation, 4-1, Ukishimacho, Kawasakiku, Kawasaki, Kanagawa 210-0862, Japan; Y. Hayakawa, K. Miyazaki and S. Kitamura, National Aerospace Laboratory, 7-44-1, Jindaiji-higashicho, Chofu, Tokyo 182-8522, Japan

1999-145: ION THRUSTER LIFETIME ESTIMATION AND MODELING USING COMPUTER SIMULATION; Masakatsu Nakano, Satellite Venture Business Laboratory, Kyushu Institute of Technology, 1-1, Sensuicho, Tobata-ku, Kitakyushu-Shi, Fukuoka 804-8550, Japan; Yoshihiro Arakawa, Department of Aeronautics and Astronautics, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

1999-146: PARTICLE SIMULATION ON ION BEAM EXTRACTION PHENOMENA IN AN ION THRUSTER; Yasushi Okawa and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan

1999-147: VALIDATION OF A GRID-EROSION SIMULATION BY SHORT-TIME EROSION MEASUREMENTS; M. Tartz, E. Hartmann, R. Deltschew, and H. Neumann, Institut fur Oberflachenmodifizierung (IOM) e. V., Permoserstr, 15, D-04318 Leipzig, Germany

1999-148: APPLICATION OF AMORPHOUS-CARBON GRIDS TO AN ION THRUSTER; Hirohiko Satow and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Takeshi Tachibana, Department of Mechanical and Control Engineering, Kyushu Institute of Technology, 1-1, Sensuityo, Tobata, Kitakyushu, Fukuoka 804-0015, Japan; Katsumi Kawata, Astec Irie Corporation, 1-3-1, Otani, Yahatahigashi, Kitakyushu, Fukuoka 805-0053, Japan

1999-149: TITANIUM OPTICS FOR ION THRUSTERS; George C. Soulas, Dynacs Engineering Co., Inc., NASA Glenn Research Center Group, 2001 Aerospace Parkway, Brook Park, OH 44142, U.S.A.; Thomas W. Haag, Michael J. Patterson, and Vincent K. Rawlin, NASA Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

1999-150: SIMULATION OF ELECTROMAGNETIC INTERFERENCE INDUCED BY ION THRUSTER PLUME, Masahiro Kajikawa and Mengu Cho, Department of Electrical Engineering, Kyushu Institute of Technology, Tobata-ku, Kitakyushu, Japan 804-8550

1999-151: DEEP SPACE ONE INVESTIGATIONS OF ION PROPULSION PLASMA ENVIRONMENT: INITIAL RESULTS; J. Wang, D. E. Brinza, J. E. Polk, and M. D. Henry, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

1999-153: IMPROVEMENT OF 20 MN XENNON ION THRUSTER; Toshiyuki Ozaki, Yukikazu Kasai, and Eiji Nishida, Space Engineering Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa 247-8520, Japan

1999-154: PERFORMANCE IMPROVEMENT OF RADIOFREQUENCY ION THRUSTERS – THE EVOLUATION OF THE RIT 15 ION ENGINE; H. J. Leiter, H. W. Loeb and K. H. Schartner, 1^st Institute of Physics, Heinrich-Buff-Ring 16, 35392 Giessen, Germany

1999-156: C60 PLASMA AND ION BEAM DIAGNOSTICS IN AN ELECTRON BOMBARDMENT ION THRUSTER; Satoru Sugaya and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Yoshinori Nakayama, Department of Aerospace Engineering, National Defense Academy, Hashirimizu 1-10-20, Yokosuka 239-8686, Japan

1999-157: PLASMA PROPERTIES AROUND THE BAFFLE APERTURE REGION OF THE UK25 ION THRUSTER; David J. Milligan and Stephen B. Gabriel, Astronautics Research Group, School of Engineering, University of Southampton, Highfield, Southampton SO17 1BJ, UK

1999-158: DEVELOPMENT AND PERFORMANCE TESTING OF AN RF-ION THRUSTER FOR PRIMARY PROPULSION; Helmut Bassner, Space Infrastructure, Daimler-Benz Aerospace AG, Postfach 80 11 69, D-81663, Germany; Robert Bond and Vaughan Thompson, AEA Technology plc, Cullham Science and Technology Centre, Abingdon, Oxon OX14 3DB, United Kingdom

1999-159: ENHANCED DISCHARGE PERFORMANCE IN A RING CUSP PLASMA SOURCE; John E. Foster and Michael J. Patterson, NASA Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135

1999-160: ELECTION EMISSION MECHANISM OF MICROWAVE DISCHARGE NEUTRALIZER; Noriyoshi Onodera and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan; Kazutaka Nishiyama, Ikko Funaki, and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan

1999-162: NUMERICAL MODELING OF EXTRACTION SYSTEMS IN ION THRUSTERS; V. A. Muravlev and A. A. Shagayda, Keldysh Research Center, Onezhskaya 8/10, Moscow, 125438, Russia

1999-163: INVESTIGATION OF NEAR-CATHODE AREA OF 5-CM ION THRUSTER: A CURRENT STATE OF WORK; O. A. Gorshkov and M. V. Zikeyev, Keldysh Research Center, Onezhskaya 8/10, Moscow, 125438, Russia

1999-164: VERIFICATION TESTS OF 10-CM-DIAM. CARBON-CARBON COMPOSITE GRIDS FOR MICROWAVE DISCHARGE ION THRUSTER; I. Funaki, H. Kuninaka, Y. Shimizu, K. Toki, S. Satori, and K. Nishiyama, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan

1999-165: SCALING LAW APPLICABLE TO DESIGN OF MPD ARCJET; Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Kyoichi Kuriki, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan

1999-166: THERMAL ANALYSIS OF A LORENTZ FORCE ACCELERATOR WITH AN OPEN LITHIUM HEAT PIPE; G. Emsellem, A. D. Kodys, and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), MAE Dept., Princeton University, Princeton, NJ 08544

1999-167: CHARACTERISATION OF A STEADY STATE MPD THRUSTER WITH RADIATION COOLED ANODE; Michael Winter, Monika Auweter-Kurtz, Christian Boie, Jorg Heiermann, and Helmut L. Kurtz; Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D70550 Stuttgart, Germany

1999-168: NUMERICAL STUDY OF ONSET PHENOMENA IN A 2-DIMENSIONAL AXISYMMETRIC MPD THRUSTER; Takeshi Miyasaka and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo-cho Chikusa-ku, Nagoya, 464-8603, Japan

1999-169: RECENT IMPROVEMENTS OF NUMERICAL METHODS FOR THE SIMULATION OF MPD THRUSTER FLOW ON ADAPTIVE MESHES; J. Heiermann, M. Auweter-Kurtz, and H. J. Kaeppeler, Institute for Space Systems, Stuttgart University, 70550 Stuttgart, Germany; A. Eberle, DaimlerChrysler Aerospace AG, Military Aircraft MT-63, 81663 Munich, Germany; U. Iben, Robert Bosch GmbH, 70049 Stuttgart, Germany; and P. C. Sleziona, Institute of Industrial Mathematics, University of Kaiserslautern, 67663 Kaiserslautern, Germany

1999-170: LOW TEMPERATURE CATHODE OPERATION: A SPOT MODEL-PART I; Paola Rossetti, Fabrizio Paganucci, and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, 1-56014, Pisa, Italia

1999-171: ONE-DIMENSIONAL NUMERICAL SIMULATION OF TWO-FLUID NONEQUILIBRIUM PLASMA FLOW IN MPD THRUSTERS; Nobuyuki Fukuoka, Takeshi Miyasaka, and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo-cho Chikusa-ku, Nagoya, 464-8603, Japan

1999-172: ELECTRODE POWER LOSS AND THRUSTER PERFORMANCE OF A PULSED MPD ACCELERATOR; Yoichi Kagaya, Hirokazu Tahara, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka, 560-8531, Japan

1999-173: CATHODE JET OF MAGNETOPLASMADYNAMIC THRUSTERS; Kazunori Mitsuo, Hirokazu Tahara, Hiroshi Hamano, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, Machikaneyama 1-3, Toyonaka, Osaka 560-8531, Japan

1999-174: TEMPERATURE AND MATERIAL EFFECTS ON THE OPERATION OF MPD CATHODES; Fabrizio Paganucci, Paola Rossetti, and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, 1-56014, Pisa, Italia

1999-175: SUPERSONIC PLASMA FLOW IN A MAGNETIC NOZZLE; Masaki Inutake, Kunihiko Hattori, Akira Ando, Fumio Hori, Taku Sugimura, Kenji Fukushi, Tsutomu Ochiai, Masaya Yamamoto, Tsuyoshi Yagai, Atsushi Imasaki, and Mikirou Yoshinuma, Department of Electrical Engineering, Tohokuu University, Aoba, Sendai, 980-8579, Japan

1999-176: OWN MAGNETIC FIELD IMPACT ON MPD THRUSTERS PERFORMANCE WITH EXTERNAL MAGNETIC FIELD; Victor B. Tikhonov and Sergei A. Semenikhin, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, Russia, 4, Volokolamskoe shosse, Moscow, 125810, Russia; James E. Polk, Jet Propulsion Laboratory, 4800 Oak Grove Drive, Mail Stop 125-224, Pasadena, CA 91109

1999-177: NUMERICAL ANALYSES OF MHD FLOWS IN AN APPLIED-FIELD MPD ACRJET THRUSTER; Hiroshi Katsurayama, Takeshi Miyasaka, and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa-ku, Nagoya, 464-8603, Japan

1999-179: ARC STRUCTURE IN A COAXIAL MAGNETOPLASMADYNAMIC CHANNEL; Kazunori Mitsuo, Hirokazu Tahara, Taro Kimura, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, Machikaneyama 1-3, Toyonaka, Osaka 560-8531, Japan

1999-180: MACH-PROBE CHARACTERISTICS IN A MAGNETIZED PLASMA FLOW; Akira Ando, Kunihiko Hattori, Masaaki Inutake, Taku Sugimura, Fumio Hori, Kenji Fukushi, Tsutomu Ochiai, Masaya Yamamoto, Tsuyoshi Yagai, Atsushi Imasaki, and Mikirou Yoshinuma, Department of Electrical Engineering, Tohoku University, Aoba, Sendai, 980-8579, Japan

1999-181: DESIGN OF A SOLAR ELECTRIC PROPULSION TRANSFER VEHICLE FOR A NON-NUCLEAR HUMAN MARS EXPLORATION ARCHITECTURE; Leonard A. Dudzinski, Kurt J. Hack, Leon P. Gefert, Thomas W. Kerslake, and Alen W. Hewston NASA John H. Glenn Research Center, 21000 Brookpark Rd, Cleveland, OH USA

1999-182: AN OVERVIEW OF THE ON-ORBIT RESULTS FROM THE ELECTRIC PROPULSION SPACE EXPERIMENT (ESEX), D. R. Bromaghim, J. R. LeDuc, R. M. Salasovich, J. A. Zimmerman, D. C. Matias, A. M. Sutton, G. G. Spanjers, J. M. Fife, W. H. Hargus, and R. A. Spores, USAF Research Laboratory, Edwards AFB, CA; M. J. Dulligan and S. F. Engelman, ERC, Inc., USAF Research Laboratory, Edwards AFB, CA; J. H. Schiling and D. C. White, W. E. Research, LLC, Rosamond, CA; and L. K. Johnson, The Aerospace Corporation, El Segundo, CA

1999-183: TORGUE CONTROL OF HALL PROPELLED SMALL SPACECRAFT; Joseph Ashkenazy and Gabi Appelbaum, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel; Moshe Guelman and Alex Kogan, Asher Space Research Institute, Technion I.I.T. Haifa 32000, Israel

1999-185: ADVANCED ELECTRIC PROPULSION FOR RLV LAUNCHED GEOSYNCHRONOUS SPACECRAFT; Steven R. Oleson, National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, OH 44135

1999-186: FEASIBILITY STUDY OF NANOSATELLITE BASED ON COMMERICIAL TECHNOLOGY; Shin Satori, Masahiro Suzuki, Masami Sasaki, Ryuichi Mitsuhasi, and Satoshi Takezawa, Hokkaido Institute of Technology; Hiroyuki Okamoto, Astro Research Company; Shin’ichi Nakasuka, University of Tokyo; Nobutada Sako, Graduate School of Engineering, University of Tokyo; Tomohiro Isikawa and Atsushi Nagata, Graduate School of Engineering, Hokkaido Institute of Technology

1999-187: TWO NEW SPACECRAFT ARCHITECTURES AND THEIR IMPACTS ON ELECTRIC PROPULSION; Shinichi Nakasuka, Yuichi Tsuda, and Takashi Eijima, Department of Aeronautics and Astronautics, University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo 113-8656, Japan; Yasuhiro Kawakatsu and Ryuichi Nagashima, Tsukuba Space Center, NASDA, Sengen 2-1-1, Tsukuba, 305-8505, Japan

1999-188: A METHOD OF PLACING A SPACECRAFT ON HIGH ORBIT; V. N. Vinogradov, V. M. Murashko, and A. G. Nattyn, Fakel, Moskovsky pr. 181, Kaliningrad 236001, Russia

1999-189: VERY LONG RANGE EXPLORATION BY MEANS OF ELECTRIC PROPULSION AND COMETARY RESOURCE UTILIZATION; P. J. Turchi and C. A. Scharlemann, Aerospace Engineering, Applied Mechanics and Aviation Department, The Ohio State University, Columbus, Ohio, USA

1999-190: THE PRELIMINARY STUDY ON THE EFFECTIVE UTILIZATION OF A LUNAR-DERIVED PROPELLANT (LOX); R. Nagashima, Y. Kawakatsu, and T. Yokoyama, National Space Development Agency of Japan, Tsukuba Space Center, 2-1-1, Sengen, Tsukuba-City, Ibaraki, 305-0047, Japan; S. Nakasuka, University of Tokyo, Department of Aeronautics and Astronautics, 7-3-1, Hongo, Bunkyo-ku, Tokyo, 113-8656, Japan

1999-191: APPLICATION OF DC ARCJET FOR LOW EARTH ORBIT SPACECRAFT; Yoshinori Kunii, Space Systems Department, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, 247-8520, Japan; Kyoichiro Toki, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, 229-8510, Japan

1999-192: PULSED PLASMA THRUSTERS FOR SPACECRAFT ATTITUDE AND ORBIT CONTROL SYSTEM; N. N. Antropov, G. A. Diakonov, V. Kim, G. A. Popov, and A. I. Pokryshkin, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; M. N. Kazeev, Russian Research Centre “Kurchatov Institute”, 1, Kurchatov sq., Moscow, 123182, Russia; and V. P. Khodnenko, All-Russian Research Institute of Electromechanics, 10100, P.O. Box 496, Moscow, Russia

1999-194: EVALUATION OF ELECTRODYNAMIC TETHER PROPULSION TO OTV; Masaya Kozakai and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan; Yoshiki Yamagiwa and Ryosuke Tuyuki, Shizuoka University, 3-5-1, Johoku, Hamamatsu-shi, Shizuoka 432-8561, Japan; Ryoichiro Yasumitsu, University of Tokyo, 7-3-1, Hongo, Bunko-ku, Tokyo 113-8654, Japan; Atsushi Nakajima, National Aerospace Laboratory, 7-44-1, Jindaiji Higashi-machi, Chofu, Tokyo 182-8522, Japan

1999-195: NON-CHEMICAL PROPULSION ABILITIES FOR NEAR-EARTH MISSIONS; V. A. Nevrovsky, Moscow State University of Aircraft Technology, Orshanskaya str. 3, 121552 Moscow, Russia

1999-196: NITRATING BY MPD THRUSTER – IS THE ECOLOGICAL CLEAN ALTERNATIVE TO CHEMICAL-THERMAL METHODS OF STRENGTHENING; Nikolay V. Bilan, Andriy V. Loyan, Sergey V. Muchin, and Oleg P. Rubalov, STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

1999-197: DEVELOPMENT OF AN ELECTROMAGNETIC ACCELERATION PLASMA GENERATOR FOR ZIRCONIA AND TITANIUM NITRIDE COATINGS; Tetsuji Shibata, Hirokazu Tahara, Toshiaki Yasui, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-198: HIGH TEMPERATURE PLASMA FURNACE USING GAS TUNNEL TYPE PLASMA JET AND ITSIAPPLICATION TO SURFACE MODICIFICATION; Akira Kobayashi, Joining and Welding Research Institute, Osaka University, 11-1 Mihogaoka, Ibaraki, Osaka 567-0047, Japan

1999-199: DEVELOPMENT OF 30-CM LONG LINEAR SPUTTERING SOURCE USING ECR DISCHARGE; Toshiaki Yasui, Tomohiro Matsumoto, Hirokazu Tahara and Takao Yoshikawa, Division of Mechanical Engineering, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3 Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-201: EFFECTS OF ADDITION OF HYDROGEN TO NITROGEN PLASMA DURING NITRIDING OF TITANIUM AND SACM645 STEEL USING SUPERSONIC EXPANDING PLASMA JETS; Y. Ando, S. Tobe, H. Tahara, and T. Yoshikawa, Ashikaga Institute of Technology, 268-1 Omae, Ashikaga, Tochigi 326-8558, Japan; Osaka University, 1-3 Machikaneyama, Toyonaka, Osaka, 560-8531, Japan

1999-202: DEVELOPMENT OF LARGE SIZE ION SOURCE FOR ION SHOWER DOPING; H. Kuwabara, I. Nakamoto, Y. Kawaskai, Electric System Development Department Mechatronics Development Center, Ishikawajima-Harima Heavy Industries Co. Ltd., Japan, 1-15, Toyosu 3-Chome, Koto-ku, Tokyo 135-8732, Japan

1999-203: A STUDY OF PULSED PLASMA ACCELERATOR WITH METAL PROPELLANT FOR SPACE AND TECHNOLOGY APPLICATION; Leonid N. Lesnevsky and Vladimir N. Tyurin, Moscow State Aviation Institute (MAI), 4 Volokolamskoye shosse, Moscow, 125871, Russia

1999-205: QUANTITATIVE RADIATION MEASUREMENTS OF THE PULSED PLASMA MICROTHRUSTER; Tomokazu Umeki and Peter J. Turchi, The Ohio State University, Columbus, Ohio, USA

1999-206: VISUALIZATION OF CURRENT SHEET CANTING IN A PULSED PLASMA ACCELERATOR; T. E. Markusic and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

1999-207: PERFORMANCE STUDY OF HIGH POWER ABLATIVE PULSED PLASMA THRUSTER; Y. A. Alexeev and M. N. Kazeev, Institute of Nuclear Fusion of RRC “Kurchatov Institute”, 1. Pl. Kurchatova, Moscow, 123182, Russia

1999-208: AN ACCURATE CHARACTERISTICS-SPLITTING SCHEME FOR NUMERICAL SOLUTION OF MHD EQUATIONS; K. Sankaran and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

1999-209: COMPARING THE PERFORMANCE OF CO-AXIAL AND PARALLEL-PLATE GAS-FED PPTS; J. K. Ziemer and E. Y. Choueiri, MAE Dept., Princeton University, Princeton, New Jersey 08544; D. Birx, Science Research Laboratory Inc., Sommerville, MA 02143

1999-210: DESIGN OPERATION, AND INVESTIGATION OF AN INDUCTIVELY-DRIVEN, COAXIAL PULSED PLASMA THRUSTER; H. Kamhawi, P. J. Turchi, I. G. Mikellides, and P. G. Mikellides, The Ohio State University, Columbus, Ohio USA

1999-211: OPTIMIZATION OF PULSED PLASMA THRUSTERS IN RECTANGULAR AND COAXIAL GEOMETRIES; I. G. Mikellides and P. J. Turchi, The Ohio State University, Columbus, Ohio, USA

1999-213: PARTICULATE INTERACTION WITH PLASMA IN A PULSED PLASMA THRUSTER; Michael Keidar and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Tel Aviv University, P. O. B. 39040, Tel Aviv 69978, Israel

1999-214: A MODEL OF AN ELECTRICAL DISCHARGE IN A CO-AXIAL PULSED PLASMA THRUSTER; Michael Keidar and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Department of Interdisciplinary Studies, Fleischman Faculty of Engineering, Tel Aviv University, P. O. B. 39040, Tel Aviv 69978, Israel

1999-216: PLASMA AND FIELD RESPONSES TO HIGH POTENTIAL SYSTEM IN SPACE; Hideyuki Usui, Hiroshi Matsumoto, and Yoshiharu Omura, Radio Atmospheric Science Center, Kyoto University, Gokasho, Uji, Kyoto 611-0011, Japan

1999-217: COMPUTATION OF CURRENT TO A MOVING BARE TETHER; Tatsuo Onishi and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, USA; David L. Cooke, Air Force Research Laboratory, Space Vehicle Directorate, Hanscom AFB, MA, USA

1999-218: HOLLOW-CATHODE PLASMA CONTACTING INSIGHTS GAINED FORM THE ELCTRODYNAMIC TETHHER MISSION; P. J. Wilbur and D. Burtner, Colorado State University, Fort Collins, Colorado 80523

1999-219: PERFORMANCE OF ELECTRODYNAMIC TETHER ORBIT TRANSFER SYSTEM WITH CONSIDERATION OF LIFETIME BY THE IMPACT OF DEBRIS; Yoshiki Yamagiwa, Yukitaka Sakata, and Tatsuya Hashimoto, Faculty of Engineering, Shizuoka University, 3-5-1, Johoku, Hamamatsu, Shizuoka, 432-8561, Japan

1999-220: SYSTEM CONSIDERATIONS OF ELECTRODYNAMIC-TETHER PROPULSION TECHNOLOGY AND FUTURE PLANS; Brian E. Gilchrist, Sven G. Bilen, and Nestor R. Voronka, Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109-2143; Les Johnson, NASA Marshall Space Flight Center, Huntsville, AL 35812; Enrico C. Lorenzini, Harvard-Smithsonian Center for Astrophysics, Cambridge, MA 02318

1999-221: COMPARISON BETWEEN PLASMA PLUME THEORETICAL MODELS AND EXPERIMENTAL DATA; A. G. Korsun, B. S. Borisov, E. M. Tverdokhlebova, and F. F. Gabdullin, Central Research Institute of Machine Building (TsNIIMASH), Korolev, Moscow Region, Russia

1999-222: THE REACTION YIELD OF GRAPHITE WITH HYPERTHERMAL ATOMIC OXYGEN IN A LOW EARTH ORBITAL SPACE ENVIRONMENT; Hiroshi Kinoshita and Masatake Umeno, Department of Material and Life Science, Graduate School of Engineering, Osaka University, 2-1 Yamada-oka, Suita, Osaka 565-0871, Japan; Masahito Tagawa and Nobuo Ohmae, Department of Mechanical Engineering, Faculty of Engineering, Kobe University, 1-1 Rokko-dai, Nada, Kobe 657-8501, Japan

1999-223: EXPERIMENTAL DETERMINATION OF SPUTTERING COEFFICIENTS ISP SOFTWARE: NUMERICAL CALCULATION OF MATERIAL EROSION; I. Jouin, V. Perrin, D. Borie (Alcatel Space Industries), V. Huchet (Teuchos PACA), S. Khartov, A. Nadiradze, I. Shkarban, A. Semenov, and A. Chirov. (Moscow Aviation Institute), Alcatel Space Industries – 100, Bd du Midi BP 99 -06156 Cannes – France

1999-224: GROUND EXPERIMENTS OF INTERACTION BETWEEN PLASMA FLOW AND NEGATIVELY BIASED OR CHARGED MATERIALS; Daiki Matsuyama, Hirokazu Tahara, Takashi Matsuda, Toshiaki Yasui, and Takao Yoshikawa, Division of Mechanical Science, Department of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

1999-226: PLUME MEASUREMENT OF PLASMA PROPULSION SYSTEM; Taizou Noutsuka, Yoshiyuki Takao, Tomoya Hida, Yoshiki Yano, Gen Kantou, Kazuhiko Uemura, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-Kouen Kasuga, Fukuoka 816-8580, Japan

1999-227: ICRF WAVE PROPAGATION AND ABSORPTION IN A MICROWAVE DISCHARGE ION THRUSTER; Yoshitaka Mori, Yoshiyuki Takao and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-Kouen, Fukuoka 816-8580, Japan

1999-228: INTERACTION BETWEEN PLASMA PLUME OF ELECTRIC PROPULSION AND SPACECRAFT COMMUNICATION; Noriyoshi Onodera and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino-shi, Tokyo 191-0065, Japan; Ikko Funaki and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihra-shi, Kanagawa 229-8510, Japan

1999-229: MATHEMATICAL MODELING OF INTERACTION OF THE ELECTRIC PROPULSION AND SPACECRAFT RADIOTEXNICAL SYSTEMS; I. P. Kozlov, Research Institute of Applied Mechanics and Electrodynamics (RIAME), 4 Volokolamskoye sh., Moscow, 125810

1999-230: OPTICAL MEASUREMENT OF CHARGING AND DISCHARGING PROCESSES ON INSULATOR SURFACE IN SIMULATED LOW EARTH ORBIT PLASMA ENVIRONMENT; Ko Shiraishi, Mengu Cho, and Masayuki Hikita, Department of Electrical Engineering, Kyushu Institute of Technology, Tobata-ku, Kitakyushu, Japan 804-8550

1999-232: CONTAMINATION SENSOR FOR ELECTRIC PROPULSION AND SOLID ROCKET MOTOR; Kazutaka Nishiyama, Ikkoh Funaki, and Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-233: ISAS HIGH ENTHALPY FLOW FACILITY FOR THERMAL PROTECTION MATERIAL TESTS; Tetsuya Yamada, Naohiro Suzuki, and Yoshifumi Inatani, Division for Space Propulsion Systems, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

1999-235: EXPERIMENTAL ANALYSIS OF A SOLID PROPELLANT MPD THRUSTER WITH DIFFERENT ANODE RADII; Giorgio Paccani and Luigi Petrucci, Universita degli Studi di Roma “La Sapienza”, Rome, Italy; and William D. Deininger, Ball Aerospace & Technologies Corp., Boulder, CO, USA

1999-238: PRELIMINARY DEVELOPMENT STATUS OF THE IUA’S P4S-1 ABLATIVE PULSED PLASMA THRUSTER; Hector H. Brito, Roque O. De Alessandro, and Carlos A. Dominguez, Centro de Investigaciones Aplicadas, Instituto Universitario Aeronautico, Ruta 20, Km 6.5, 5022 Cordoba, Argentina

1999-241: MICROWAVE TELEMETRY BREAKDOWN CAUSED BY ROCKET PLUME; Takashi Abe, Kazuhisa Fujita, Hiroyuki Ogawa, and Ikkoh Funaki, The Institute of Space and Astronautical Science, Kanagawa 229-8510, Japan

1999-242: A MODEL FOR THE CHARACTERIATION OF PLASMA INSIDE THE STATIONARY PLASMA THRUSTER; K Makowski, Z. Peradynski, and S. Barral, Institute of Fundamental Technological Research, Polish Academy of Sciences, Swietokrzyska 21, 00-049 Warsaw, Poland; M. Dudeck, Laboratoire d’Aerothermique du CNRS, 1C, avenue de la Recherche Scientifique, 45071 Orleans Cedex 2, France

1999-244: DESIGN AND MANUFACTURE OF THE ETS VIII COMPOSITE OVERWRAPPED XENON PRESSURE VESSEL; Walter H. Tam, Pressure Systems, Inc.; Mark D. Drey and Arthur C. Jackson, Programmed Composites, Inc.; Eiji Nishida and Yukikazu Kasai, Mitsubishi Electric Corporation; and Akio Tsujihata and Kenichi Kajiwara, National Space Development Agency of Japan

1999-245: PARAMETRIC INVESTIGATIONS OF SEGMENTED ELECTRODE HALL THRUSTER; Y. Raitses, L. A. Dorf, A. A. Litvak, and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ 08540

1999 FILE DIRECTORY (add "199" to begining of file name)

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2001 INDEX

2001-001: NASA’S NEW EMPHASIS ON IN-SPACE PROPULSION TECHNOLOGY RESEARCH; Les Johnson, Advanced Space Transportation Program/TD15, Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812, USA

2001-002: NASA’S ELECTRIC PROPULSION PROGRAM; John W. Dunning Jr., Scott Benson, Steven Oleson, National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, Ohio USA 44135

2001-003: OVERVIEW OF THE USAF ELECTRIC PROPULSION PROGRAM; Ronald A. Spores and Gregory G. Spanjers, Air Force Research Laboratory Propulsion Directorate, Edwards AFB, CA 93524; Mitat Birkan, Air Force Office of Scientific Research, Bolling AFB, Washington, DC 20332; and Major Timothy J. Lawrence, European Office of Aerospace Research and Development, London, NW1 5^TH UK

2001-004: AN OVERVIEW OF ELECTRIC AND ADVANCED PROPULSION ACTIVITIES IN JAPAN; Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., Asahigaoka 6, Hino, Tokyo 191-0065, Japan

2001-005: ELECTRIC PROPULSION ACTIVITY IN RUSSIA; Vladimir Kim and Garri Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, P.O. Box 43, Moscow 125080, Russa; Boris Arkhipov and Vyacheslav Murashko, “Fakel” Design Bureau, Kaliningrad, Russia; Oleg Gorshkov and Anatoly Koroteyev, Keldysh Research Center; Valery Garkusha, Alexander Semenkin, and Sergei Tverdokhlebov, Tsentral Institute of Machinebuilding, Moscow, Russia

2001-006: EUROPEAN ELECTRIC PROPULSION ACTIVITIES AND PROGRAMMES; G. Saccoccia, ESA Technical and Operational Support Directorate, ESTEC, Noordwijk, The Netherlands

2001-007: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN CHINA; Xiaolu Kang, Zhaoling Wang and Nanhao Wang, Shanghai Spaceflight Power Machinery Institute, Shanghai, P. R. China, 200233; Anjie Li, Center for Space Science and Applied Research of CAS (CSSAR); Guofu Wu, Lanzhou Institute of Physics (LIP); Gengwang Mao, Northwestern Polytechnical University (NPU); Haibin Tang, Beijing University of Aeronautics and Astronautics (BUAA); and Wenhuua Zhao, Tsinghua University

2001-008: AN OVERVIEW OF THE CNES ELECTRIC PROPULSION PROGRAM; Anne Cadiou, CÃ©cile Gelas, Franck Darnon, Laurent Jolivet, and Nicolas Pillet, CNES, 18 Avenue Edouard Belin, 31401 Toulouse Cedex 4

2001-010: THE DEVELOPMENT AND QUALIFICATION OF A 4.5 KW HALL THRUSTER PROPULSION SYSTEM FOR GEO SATELLITE APPLICATIONS; Jack Fisher, Alfred Wilson, David King, Steve Meyer, Carl Engelbrecht and Kristi de Grys, General Dynamics Space Propulsion Systems; 1141 Willows Road N.E., P.O. Box 97009, Redmond, WA 9807309709; Lance Werthman, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

2001-011: DEVELOPMENT AND TESTING OF A 4500 WATT FLIGHT TYPE HALL THRUSTER AND CATHODE; Kristi de Grys, Nicole Meckel, George Callis, Doug Greisen, Andrew Hoskins, David King, and Fred Wilson, General Dynamics Space Propulsion Systems, 11441 Willows Road N.E., P.O. Box 97009; Lance Werthman, and Vadim Khaymas, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

2001-012: PERFECTING OF THE TECHNOLOGICAL SOLUTIONS AT MANUFACTURING OF A ET MT 12; A.N. Tarasov, V. M. Murashko, and A. G. Niatin, OKb “Fakel”, Kaliningrad, Russian Federation

2001-013: OPERATING ENVELOPES OF THRUSTERS WITH ANODE LAYER; A. V. Semenkin, S. O. Tverdokhlebov, V. I. Garkusha, A. V. Kochergin, G. O. Chislov, B. V. Shumkin, A. V. Solodukhin, and L. E. Zakharenkov

2001-015: A CONCEPT OF DEVELOPMENT OF ELECTRIC THRUSTERS WITH THRUST VECTOR CONTROL; Valery Petrosov, Keldysh Research Center, Moscow, Russia

2001-017: CHARACTERIZATION OF THE PLASMA IN A HALL THRUSTER; E. Ahedo, P. MartÃnez Cerezo, and J. M. Gallardo, E.T.S.I. AeronÃ¡uticos, Univ. PolitÃ©cnica, 28040 Madrid, Spain; M. MartÃnez-SÃ¡nchez, Dep. Of Aeronautics & Astronautics, M.I.T., Cambridge, MA 02139

2001-018: AZIMUTHAL NON-UNIFORMITIES IN ACCELERATORS WITH CLOSED ELECTRON DRIFT; Vladimir Baranov, Yuri Nazarenko, and Valery Petrosov, Keldysh Research Center, Moscow, Russia

2001-019: DECONVOLUTION OF AXIAL VELOCITY DISTRIBUTIONS FROM HALL THRUSTER LIF SPECTRA; Timothy B. Smith, Daniel A. Herman, Alec D. Gallimore, and R. Paul Drake, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Rm. B107, 1919 Green Rd., Ann Arbor, MI 48105

2001-020: A COMPARISON OF NUDE AND COLLIMATED FARADAY PROBES FOR USE WITH HALL THRUSTERS; Richard R. Hofer, Mitchell L. R. Walker, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

2001-021: DETERMINATION OF THE IONIZATION AND ACCELERATION ZONES IN A STATIONARY PLASMA THRUSTER; N. Dorval, J. Bonnet, J. P. Marque, and E. Rosencher, ONERA/DMPH, Chemin de la HuniÃ©re, 91761 Palaiseau (France); S. Chable and F. Rogier, ONERA/DTIM, 2 avenue E. Belin, 31055, Toulouse (France); and P. Lasgorceix, LAMO, 3 avenue de la Recherche Scientifique, 45071, OrlÃ©ans Cedex 2 (France)

2001-022: A 1-D TIME-DEPENDENT MODEL OF A HALL THRUSTER WITH SIDE WALLS; Peter S. Rostler, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760

2001-023: A NUMERICAL STUDY OF THE EFFECT OF CHANNEL INSULATOR DISCONTINUITY ON HALL THRUSTER DISCHARGE; Summer Locke and Uri Shumlak, Department of Aeronautics and Astronautics, University of Washington, BOX 352250, Seattle, WA 98145-2400; J. M. Fife, Electric Propulsion Group, Air Force Research Laboratory, AFRL/PRRS, 1 Ara Road, Edwards AFB, CA 93524-7190

2001-024: A STATIONARY HYDRODYNAMIC MODEL FOR HALL THRUSTER; Vasily Lobzin, Institute of Terrestrial Magnetism, Ionosphere and Radio Wave Propagation, Russian Academy of Sciences, Troitsk, Moscow region, Russia, 142190; Nicolas Gascon, Thermosciences Division, Mechanical Engineering Department, Stanford University, Stanford, California 94305-3032; Vladimir Krasnoselskikh, Laboratoire de Physique et Chimie de l’Environnement, Centre National de la Recherche Scientifique, 3A, Avenue de la Recherche Scientifique, 45071 OrlÃ©ans CEDEX 2; Michael Dudeck, Laboratoire d’ AÃ©rothermique, Centre National de la Recherche Scientifique, 1C, Avenue de la Recherche Scientifique, 45071 OrlÃ©ans CEDEX 2

2001-025: ABOUT THE DOUBLE-HUMPED ELECTRON DISTRIBUTION FUNCTION IN HALL THRUSTERS; S. Barral, Z. Peradzynski, and K. Makowski, Institute of Fundamental Technological Research, Swietokrzyska 21, 00049 Warsaw, Polad; M. Dudeck, CNRS Laboratoire d’ Aerothermique, 1c avenue de la Recherche Scientifique, 45071 Orleans, France

2001-026: ANALYSIS OF THE STEADY-STATE AXIAL FLOW IN THE HALL THRUSTER; Avi Cohen-Zur and Alon Gany, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; Amnon Fruchtman, Holon Academic Institute of Technology, P. O. Box 305, Holon 58102, Israel; Joseph Ashkenazy, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

2001-027: NUMBERICAL STUDY OF THE CURRENT-VOLTAGE CHARACTERISTIC OF HALL THRUSTERS; S. Barral, K. Makowski, Institute of Fundamental Technological Research – PAS, Swietokrzyska 21, 00-049 Warsaw, Poland; Z. Peradzynski, Dept. of Mathematics, Informatic and Mechanics of Warsaw University, Banacha 2, 00-097 Warsaw, Poland; N. Gascon, Stanford University, Mechanical Engineering Department, Stanford – California, 94305-3032, USA; M. Dudeck, CNRS Laboratoire d’Aeothermique, 1c avenue de la Recherche Scientifique, 45071 Orleans, France

2001-028: PARAMETRIC STUDY OF A STATIONARY PLASMA THRUSTER USING A TWO-DIMENSIONAL HYBRID MODEL; G.J.M. Hagelaar, J. Bareilles, L. Garrigues, and J. P. Boeuf, CPAT, Batiment 3R2, UniversitÃ© Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse, France

2001-029: MAGNETIC SYSTEM FOR HALL THRUSTERS EVALUATION AND DESIGN; V. I. Garkusha and A. V. Semenkin, Central Research Institute of Machine Building, Korolev, Russia

2001-030: EXPERIMENTAL INVESTIGATION OF A HALL THRUSTER INTERNAL MAGNETIC FIELD TOPOGRAPHY; Peter Y. Peterson, Alec D. Gallimore, and James M. Haas, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, College of Engineering, Ann Arbor, MI 48109 USA

2001-032: PARAMETERS OF D-80 ANODE LAYER THRUSTER IN ONE- AND TWO- STAGE OPERATION MODES; A. E. Solodukhin, A. V. Semenkin, S. O. Tverdohlebov and A. V. Kochergin, Central Research Institute of Machine Building, Korolev, Moscow Reg., Russia

2001-035: PERFORMANCE OF A HIGH SPECIFIC IMPLUSE HALL THRUSTER; Bruce Pote and Rachel Tedrake, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-036: A HIGH SPECIFIC IMPLUSE TWO-STAGE HALL THRUSTER WITH PLASMA LENS FOCUSING; Richard R. Hofer, Peter Y. Peterson, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA; Robert S. Jankovsky, NASA Glenn Research Center, Cleveland, OH 44135, USA

2001-037: PIC SIMULATION OF HIGH SPECIFIC IMPLUSE HALL EFFECT THRUSTER; Vincent Blateau, Manuel Martinez-Sanchez, Oleg Batishchev, and James Szabo, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139

2001-038: PARAMETRIC INVESTIGATIONS OF MINIATURIZED CYLINDRICAL AND ANNULAR HALL THRUSTERS; A. Smirnov, Y. Raitses, and N. J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, NJ 08543

2001-039: LINEAR GEOMETRY HALL THRUSTER WITH BORON NITRIDE AND DIAMOND WALLS; Nathan B. Meezan, Nicolas Gascon, and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Stanford, CA 94305-3032

2001-041: STUDY OF LOW POWER TAL CHARACTERISTICS; L. Zakharenkov, G. Chislov, and A. Semenkin, Central Research Institute of Machine Building (TsNIIMASH), Russia 141070, Korolev City, Moscow region, Pionerskaya str., 4; T. Lawrence, European Office of Aerospace Research and Development

2001-042: THRUST PERFORMANCE AND PLASMA CHARACTERISTICS OF LOW POWER HALL THRUSTERS; Hirokazu Tahara, Daisuke Goto, Toshiaki Yasui, and Takao Yoshikawa, Division of Mechanical Science, Dept. of Systems, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2001-044: HALL THRUSTER PLUME MEASUREMENTS ON-BOARD THE RUSSIAN EXPRESS SATELLITES; David Manzella, The University of Toledo, Toledo, OH 43606; Robert Jankovsky and Frederick Elliott, NASA John H. Glenn Research Center, Cleveland, OH 44135; Ioannis Mikellides and Gary Jongeward, Science Applications International Corporation, San Diego, CA 92121; and Doug Allen, Schafer Corporation, Dayton, OH 45431

2001-045: CHARACTERIZING VACUUM FACILITY BACKPRESSURE EFFECTS ON THE PERFORMANCE OF A HALL THRUSTER; Richard R. Hofer, Peter Y. Peterson, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

2001-048: THE WEAR OF THE CHANNEL WALLS IN HALL THRUSTERS; Vladimir Baranov, Yuri Nazarenko, and Valery Petrosov, Keldysh Research Center, Moscow, Russia

2001-049: DEVELOPMENT OF A FINITE ELEMENT BASED HALL THRUSTER MODEL FOR SPUTTER YIELD PREDICTION; Subrata Roy and Birendra Pandey, Computational Plasma Dynamics Research Laboratory, Kettering University, 1700 West Third Avenue, Flint, MI 48504

2001-051: A KINETIC STUDY OF ELECTRON-WALL COLLISIONS IN A HALL THRUSTER; Nathan B. Meezan and Mark A. Cappelli, Stanford University, Department of Mechanical Engineering, Stanford, CA 94305-3032

2001-053: OPTICAL EMISSION OF A HALL THRUSTER PLUME IN SPACE CONDITION; Georgie Karabadzhak, Flur Gabdullin, Anatoli Korsun, Yuri Plastinin and Ekaterina Tverdokhlebova, Central Research Institute of Machine-Building (TSNIIMASH); Pionerskaya Street, 4, Korolev, Moscow region, Russia, 141070

2001-054: SIMULATIONS FOR A SHUTTLE-BASED HALL THRUSTER PLUME EXPERIMENT; Shannon Y. Cheng and Manuel Martinez-Sanchez, Space Propulsion Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139

2001-055: INFLUENCE OF DISCHARGE OSCILLATION ON HALL THRUSTER PERFORMANCE; Naoji Yamamoto, Takafumi Nakagawa, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo, 113-8656, Japan

2001-056: LOW FREQUENCY PLASMA WAVE DISPERSION AND PROPAGATION IN HALL THRUSTERS; Nicolas Gascon, Nathan B. Meezan, and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Stanford, CA 94305-3032

2001-057: METHODS OF CONTROLLING LOW-FREQUENCY OSCILLATION IN A HALL THRUSTER; Takeshi Furukawa, Takeshi Miyasaka and Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa-ku Nagoya 464-8603, Japan

2001-058: ANALYSIS OF COMMUNICATION SIGNAL MODULATION INDUCED BY PERIODIC HALL THRUSTER PLUME INSTABILITIES; Joseph T. Loane and J. William Meyer, Lockheed Martin Space Systems Company, Sunnyvale, CA 94089; Gary A. Hallock and James C. Wiley, The University of Texas, Austin, TX 78712

2001-059: INSIGHTS ON PHYSICS OF HALL THRUSTERS THROUGH FAST CURRENT INTERRUPTIONS AND DISCHARGE TRANSIENTS; Mathieu Prioul and AndrÃ© Bouchoule, GREMI UniversitÃ© d’OrlÃ©ans, BP 6744, 45 067 OrlÃ©ans, France; StÃ©phanie Roche, Lionel Magne, Daniel Pagnon and Michael Touzeau, LPGP, UniversitÃ© Paris XI ORSAY, 91 405 Orsay, France; Pascal Lasgorceix, Laboratoire AÃ©rothermique, CNRS, 45 067 OrlÃ©ans, France

2001-060: MEASUREMENTS OF PLASMA POTENTIAL DISTRIBUTION IN SEGMENTED ELECTRODE HALL THRUSTER; Y. Raitses, D. Staack, and N. J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, NJ 08543

2001-062: ANALYSES OF THE PLASMA FLOW AND PRESHEATH STRUCTURE IN HALL THRUSTERS; Michael Keidar and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Tel Aviv University, Tel Aviv 69978, Israel

2001-063: PRELIMINARY STUDY OF ARCJET NEUTRALIZATION OF HALL THRUSTER CLUSTERS; Quentin E. Walker and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Building 520, Stanford, CA 94309-3032; William A. Hargus, Jr., ARFL, Edwards Air Force Base, Building 8895, Edwards, CA 93524; John Schilling, W.E. Research LLC, Rosemond, CA 93560

2001-064: THE RESULTS OF TESTING AND EFFECTIVENESS OF THE KR-XE MIXTURE APPLICATION IN SPT; B. A. Arkhipov, A. I. Koryakin, V. M. Murashko, A. N. Nesterenko, and I. A. Khoromsky, EDB “Fakel”, Moskovsky pr. 181, Kaliningrad, Russia; V. Kim, V. I. Kozlov, G. A. Popov, and A. I. Skrylnikov, RIAME, Moscow Volokolamskoye sh., 4, Russia

2001-065: INVESTIGATION OF SPT PERFORMANCE AND PARTICULARITIES OF IT’S OPERATION WITH KR AND KR/XE MIXTURES; Vladimir Kim, Garry Popov, Vyacheslav Kozlov, Alexander Skrylnikov, and Dmitry Grdlichko, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI); 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2001-066: HALL THRUSTERS OPERATING IN PULSED MODE; Vlad Hruby, Bruce Pote, Manuel Gamero-CastaÃ±o, George Kolencik, Larry Byrne, Rachel Tedrake and Mary Delishatsios, Buseck Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-068: THE MAIN REGULARITY OF AN IGNITION IN A SPT; Sergiy A. Oghienko and Andriy A. Rybakov, National Aerospace University by him N. E. Joukovski “The Kharkov aviation institute”, 17, Chkalova St. Kharkov, 61070, Ukraine

2001-069: PRELIMINARY STUDY OF AN ECR DISCHARGE HALL THRUSTER; Pedro Molina-Morales, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science (ISAS), 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Toyko 113-8656, Japan

2001-070: DEVELOPMENT OF ELECTRIC PROPULSION STANDARDS – CURRENT STATUS AND FURTHER ACTIVITY; A Semenkin, Central Research Institute of Machine Building (TsNIIMASH); V. Kim, Research Institute of Applied Mechanic and Electro-dynamic (RIAME); O. Gorshkov, Keldysh Research Center; R. Jankovsky, NASA Glenn Research Center

2001-072: THERMAL CHARACTERIZATION AND MODELING OF A LOW-POWER LABORATORY MODEL TAL; John Walter and James Dickens, Department of Electrical and Computer Engineering, Texas Tech University, MS 3102, Lubbock, Texas 79409

2001-073: INVESTIGATION OF THE BORON NITRIDE BASED CERAMICS SPUTTERING YIELD UNDER IT’S BOMBARDMENT BY XE AND KR IONS; Vladmir Kim, Vyacheslav Kozlov, Alexander Semenov, and Igor Shkarban, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2001-074: OVERVIEW OF HALL CURRENT THRUSTER INTEGRATION ACTIVITIES OF LOCKHEED MARTIN SPACE SYSTEMS COMPANY; Vadim Khayms, Keith Kannenberg, Bill Meyer, and Lance Werthman, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94086

2001-075: DEMONSTRATION OF THE NSTAR ION PROPULSION SYSTEM ON THE DEEP SPACE ONE MISSION; J. E. Polk, D. Brinza R. Y. Kakuda, J. R. Brophy, I. Katz and J. R. Anderson, Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; V. K. Rawlin, M. J. Patterson, J. Sovey and J. Hamley, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44130

2001-076: LONG DURATION GROUND TESTING OF THE DEEP SPACE 1 FLIGHT SPARE ION THRUSTER – THE FIRST 15600 HOURS; John R. Anderson, Keith D. Goodfellow, and James E. Polk, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109; Vincent K. Rawlin and James S. Sovey, NASA Glenn Research Center, 21000 Brook Park Road, Cleveland, Ohio 44135

2001-081: IMPROVING THE TOTAL IMPULSE CAPABILITY OF THE NSTAR ION THRUSTER WITH THICK-ACCELERATOR-GRID ION OPTICS; George C. Soulas, NASA Glenn Research Center, M.S. 301-3, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

2001-082: RESULTS OF THE 15000 HOURS LIFETIME TEST FOR THE RITA ION PROPULSION ON ESA’S ARTEMIS SATELLITE; Rainer Killinger, Helmut Bassner, Ralf Kukies, and Hans Leiter, Astrium GmbH, Post Box 80 11 69, D-816633 MÃ¼chen, Germany

2001-083: RESULTS OF A 35-CM XENON ION THRUSTER ENDURANCE TEST; Shoji Kitamura, National Aerospace Laboratory of Japan, 7-44-1 Jindaijihigashi-Machi, Chofu, Tokyo 182-8522, Japan; Yukio Hayakawa and Katsuhiro Miyazaki, National Aerospace Laboratory of Japan, 7-44-1 Jindaijihigashi-Machi, Chofu, Tokyo, 182-8522, Japan; Ken’ichi Kajiwara, National Space Development Agency of Japan, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan; Hideki Yoshida, Yuuko Yamamoto, and Kouseki Akai, Toshiba Corporation, 4-1 Ukishima-Cho, Kawasaki-Ku, Kawasaki, Kanagawa, 210-0862, Japan

2001-084: A GRID LIFETIME MODEL FOR A 3-GRID ION ENGINE; Masakatsu Nakano, Japan Science and Technology Corporation, Kakuda Space Propulsion Laboratory, National Aerospace Laboratory, 1 Kogenesawa, Kimigaya, Kakuda-shi, Miyagi, 981-1525, Japan

2001-085: THREE-DIMENSIONAL PARTICLE SIMULATIONS OF NSTAR ION OPTICS; Joseph Wang, Dept. Aerospace & Ocean Engineering, Virginia Polytechnic Institute and State University; James Polk, John Brophy, and Ira Katz, Jet Propulsion Laboratory, California Institute of Technology

2001-086: RETENTION OF SPUTTERED MOLYBDENUM ON ION ENGINE DISCHARGE CHAMBER SURFACES; James S. Sovey, Joyce A. Dever, and John L. Power, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135

2001-088: ION PROPULSION DEVELOPMENT ACTIVITIES AT THE NASA GLENN RESEARCH CENTER; Michael J. Patterson, Matthew T. Domonkos, John E. Foster, Thomas W. Haag, Maris A. Mantenieks, Luis R. Pinero, Vincent K. Rawlin, George C. Soulas, and James S. Sovey, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135; Christian Carpenter, Scott D. Kovaleski, and Robert F. Roman, QSS Group, Inc., Cleveland, Ohio; George Williams, Ohio Aerospace Institute, Cleveland, Ohio

2001-089: NEXT-GENERATION 5/10 KW ION PROPULSION DEVELOPMENT STATUS; Michael J. Patterson, John E. Foster, Thomas Haag, Luis Pinero, Vincent K. Rawlin, George C. Soulas, and Michelle S. Doehne, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135; Robert F. Roman, QSS Group Inc., Cleveland, Ohio

2001-090: DESIGN AND PERFORMANCE OF 40 CM ION OPTICS; George C. Soulas, NASA Glenn Research Center, M.S. 301-3, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

2001-091: ELECTRON BACKSTREAMING MITIGATION VIA A MAGNETIC GRID; John E. Foster, Robert F. Roman, George C. Soulas, and Michael J. Patterson, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio, 44135

2001-092: PERFORMANCE EVALUATION OF TITANIUM ION OPTICS FOR THE NASA 30 CM ION THRUSTER; George C. Soulas, NASA Glenn Research Center, M.S. 301-3, 21000 Brookpark Road, Cleveland, OH 44135, U.S.A.

2001-094: CARBON-BASED ION OPTICS DEVELOPMENT AT NASA GRC; Thomas Haag, Michael Patterson, Vince Rawlin, and George Soulas, National Aeronautics and Space Administration, Glenn Research Center, Cleveland, OH 44135

2001-095: LIGHTWEIGHT ION ENGINE BODY; Y. Robert Yamaki and Timothy R. Knowles, Energy Science Laboratories, Inc., 6888 Nancy Ridge Drive, San Diego, CA 92121; Keith D. Goodfellow, Jet Propulsion Laboratory, California Institute of Technology, MS 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106

2001-096: STATUS OF ION ENGINE DEVELOPMENT FOR HIGH POWER, HIGH SPECIFIC IMPULSE MISSIONS; Vincent K. Rawlin and Luis R. PiÃ±ero, National Aeronautics and Space Administration, Glenn Research Center MS 301-3, 21000 Brookpark Rd., Cleveland, OH 44135; George J. Williams, Ohio Aerospace Institute, NASA Glenn Group MS 301-3, 21000 Brookpark Rd., Cleveland, OH 44135; Robert F. Roman, QSS Group, Inc., Glenn Research Center MS 16-1, 21000 Brookpark Rd., Cleveland, OH 44135

2001-097: NUMERICAL ANALYSIS OF ION BEAM EXTRACTION PHENOMENA IN AN ION THRUSTER; Yasushi Okawa, Satellite Venture Business Laboratory, Kyushu Institute of Technology, 1-1, Sensuicho, Tobata, Kitakyushu, Fukuoka 804-8550, Japan; Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Takeshi Tachibana, Department of Mechanical Engineering, Kyushu Institute of Technology

2001-098: A STUDY OF HIGH SPECIFIC IMPULSE ION THRUSTER OPTICS; Paul J. Wilbur, Joshua Miller, and Cody Farnell, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523; Vincent K. Rawlin, NASA Glenn Research Center, Cleveland, OH 44135

2001-099: NUMERICAL SIMULATION OF HIGH SPECIFIC IMPULSE ION THRUSTER OPTICS; Yoshinori Nakayama and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2001-100: NUMERICAL MODELING OFNEUTRAL AND CHARGED PARTICLES WITHIN A GRIDDED ION THRUSTER; M. Jugroot and J. K. Harvey, Department of Aeronautics, Imperial College of Science, Technology and Medicine, SW7 2BY London, United Kingdom

2001-101: PARTICLE SIMULATION FOR ION THRUSTER GRID DESIGN; Yasutaka Inanaga, Environmental Technology and System Department, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1, Tsukaguchihonmachi, Amagasaki, Hyogo 661-8861, Japan; Toshiyuki Ozaki, Space Engineering Department, Kamakura Works, Mitsubishi Electric Corporation, 325, Kamimachiya, Kamakura, Kanagawa 247-8520, Japan

2001-102: DEVELOPMENT STATUS OF 20 MN CLASS XENON ION THRUSTER FOR ETS-8; Toshiyuki Ozaki and Yoshifumi Gotoh, Space Engineering Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa 247-8520, Japan; Takashi Itoh, Engineering Test Satellite-VIII Project Team, Office of Satellite Systems, National Space Development Agency of Japan (NASDA), 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan; Ken-ichi Kajiwara, Satellite Systems Engineering Department, Office of Satellite Systems, NASDA, 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan

2001-103: 20MN-CLASS MICROWAVE DISCHARGE ION THRUSTER; Ikkoh Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; Kazutaka Nishiyama, Hitoshi Kuninaka, Kyoichiro Toki, Yukio Shhimizu, and Hanya Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2001-104: DEVELOPMENT OF THE RADIO FREQUENY ION THRUSTER RIT XT – A STATUS REPORT; Hans J. Leiter, Rainer Killinger, Helmut Bassner, Johann MÃ¼ller, and Ralf Kukies, Astrium GmbH, Post Box 80 11 69, D-816633 MÃ¼chen, Germany

2001-105: DEVELOPMENT STEPS OF THE RF-ION THRUSTERS RIT; Helmut Bassner, Rainer Killinger, Hans Leiter, and Johann MÃ¼ller, Astrium GmbH, Post Box 80 11 69, D-816633 MÃ¼chen, Germany

2001-106: A STUDY ON MICROWAVE DISCHARGE ION THRUSTER; Takashi Miyamoto, Kazuya Yamawaki, Hideto Ikeda, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Yoshiyuki Takao, Department of Computer and Control Enginerring, Oita National College of Technology, 1666 Maki, Oita 870-0152, Japan

2001-107: PERFORMANCE TEST OF VARIOUS DISCHARGE CHAMBER CONFIGURATIONS FOR ECR DISCHARGE ION THRUSTER; Haruya Toki and Hajime Fujita, Graduate School of Science and Technology Nihon University, 1-8-14 Kanda Surugadai, Chiyoda, Tokyo, 101-8308, Japan; Kazutaka Nishiyama, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Ikkoh Funaki, Institute of Engineering and Systems Tsukuba University, 1-1-1 Tennodai, Tsukuba, Ibaraki, 305-8573, Japan

2001-108: HIGH PERFORMANCE, LOW POWER ION PROPULSION SYSTEM DESIGN CONCEPT; Nicole J. Meckel, Robert J. Kay, and Carl S. Engelbrecht, General Dynamics, Space Propulsion Systems, P.O. Box 97009; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, Francois-Xavier Bagnoud Building, 1320 Beal Avenue, Ann Arbor, MI 48109-2140; James C. Dickens, Texas Tech University, Department of Electrical and Computer Engineering, Box 43102, Lubbock, TX 79409-3102; Michael J. Patterson, Power and On-Board Propulsion Technology Division, NASA Glenn Research Center, Mail Stop 301-3, Cleveland, OH 44135

2001-110: DSMC-PIC ANALYSIS OF A PLUME FROM A SMALL ION ENGINE; Michio Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; Toru Hyakutake, Department of Mechanical Engineering, Okayama University, Okayama 700-8530, Japan; Hitoshi Kuninaka and Kyoichiro Toki, Institute of Space and Astronautical Science, Sagamihara, Kanagawa 229-8510, Japan

2001-111: THE INFLUENCE OF CHARGE-EXCHANGE IONS ON THE BEAM DIVERGENCE OF AN ION THRUSTER; David H. Mundy and David G. Fearn, Space Department, QinetiQ, Farnborough, Hants, GU14 0LX, UK; Robert A. Bond, AEA Technology Space, Culham Science Centre, Abingdon, Oxon, OX14 3ED, UK

2001-112: MEASUREMENTS OF THE ELECTROMAGNETIC EMISSIONS FROM THE MUSES-C ION ENGINE SYSTEM; Kazutaka Nishiyama, Yukio Shimizu, Ikkoh Funaki, Hitoshi Kuninaka, Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, Japan 2298510

2001-113: MOLECULAR DYNAMICS SIMULATION OF LOW-ENERGY SPUTTERING OF MOLYBDENUM WITH XENON IONS; Pradosh K. Ray, Mechanical Engineering Department, Tuskegee University, Tuskegee, AL 36088

2001-114: THRUST-VECTOR TILTING CAUSED BY GRID MISALIGNMENT; M. Tartz, E. Hartmann, R. Deltschew, and H. Neumann, Institut fÃ¼r OberflÃ¤chenmodifizierung e. V. (IOM), Permoserstr. 15, D-04318 Leipzig, Germany

2001-115: ION THRUSTER THRUST VECTORING REQUIREMENTS AND TECHNIQUES; David G. Fearn, Space Department, QinetiQ, Farnborough, Hants, GU12 0LX, UK

2001-116: OPERATIONAL FEATURES OF A LINEAR SLIT COLLOID MICROTHRUSTER; Julius Perel and John F. Mahoney, Phrasor Scientific Incorporated, Duarte, CA 91010

2001-117: EFFECTS OF ION IMPLANTED C AND N ON THE SPUTTER BEHAVIORS OF TI AND MO GRID MATERIALS; Paul J. Wilbur and Joshua Miller, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523; Don L. Williamson, Department of Physics, Colorado School of Mines, Golden, CO 80401

2001-118: SPUTTER CHARACTERISTICS OF CARBON-CARBON COMPOUND MATERIAL; R. Deltschew, M. Tartz, V. Plicht, E. Hartmann, and H. Neumann, Institut fÃ¼r OberflÃ¤chenmodifizierung e. V. (IOM), Permoserstr. 15, D-04318 Leipzig, Germany; H. J. Leiter, Astrium GmbH, Space Infrastructure, PF 80 11 69, D-81663 MÃ¼chen, Germany; J. Esch, Schunk Kohlenstofftechnik GmbH, Rodheimer StraÃŸe 59, D-35452 Heuchelheim, Germany

2001-120: A STUDY OF LOW-POWER MPD ARCJETS FOR FUTURE HIGH-POWER EVOLUTION; Kyoichiro Toki and Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2001-123: DEVELOPMENT AND TESTING OF A NEW TYPE OF MPD THRUSTER; V.B. Tikhonov, N. N. Antropov, G. A. Dyakonov, and V. A. Obukhov, RIAME MAI, 125080 Moscow, PB 43, Russi;, F. Paganucci, P. Rossetti, and M. Andrenucci, CENTROSPAZIO, Via Gherardesca, 5, 56014, Pisa, Italy

2001-124: DESIGN AND OPERATION OF MW-CLASS MPD THRUSTERS PART I: NUMERICAL MODELING; Pavlos G. Mikellides, Ohio Aerospace Institute, 22800 Cedar Point Dr., Cleveland, OH 44142

2001-127: PARALLELIZATION AND VALIDATION OF MHD CODE FOR THE SIMULATION OF SELF-FIELD MPDT FLOWS; K. Sankaran, S. C. Jardin, and E. Y. Choueiri, Princeton University, Princeton, New Jersey 08544

2001-128: NUMERICAL SIMULATION OF HIGH POWER STEADY STATE MPD THRUSTERS; JÃ¶rg Heiermann and Monika Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

2001-130: EFFECT OF APPLIED MAGNETIC FIELD ON ARCJET THRUSTER; Takeshi Miyasaka, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa, Nagoya 464-8603, Japan; Hiroshi Katsurayama, Department of Aeronautics and Astronautics, University of Tokyo, Hongo, Bunkyo, Tokyo 113-8656, Japan; Toshi Fujiwara, Department of Aerospace Engineering, Nagoya University, Furo, Chikusa, Nagoya 464-8603, Japan

2001-131: EFFECT OF STRONG MAGNETIC FIELD ON TEMPERATURE DISTRIBUTION IN PLASMA JET; Kazuo Koike and Norifumi Ono, Department of Mechanical Engineering, Tohoku Gakuin University, 1-13-1, Chuo, Tagojo, Miyagi 985-8537, Japan; Takashi Uno, Sayama Precision Co., Ltd, 2-15-1, Fujimi, Sayama, Saitama 350-1393, Japan

2001-132: PERFORMANCE OF AN APPLIED FIELD MPD THRUSTER; F. Paganucci, P. Rossetti, and M. Andrenucci, Centrospazio, Via Gherardesca 5, I-56014, Pisa, Italia; V. B. Tikhonov and V. A. Obukhov, RIAME-MAI, Volokolamskoe shosse, 4, 125810, Moscow, Russia

2001-133: EXHAUST PLUME CHARACTERISTICS OF QUASI-STEADY MPD THRUSTERS; Hirokazu Tahara, Yoichi Kagaya, and Takao Yoshikawa, Division of Mechanical Science, Dept. of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2001-134: OPERATION OF AN MPD THRUSTER WITH A TYPE B CATHODE; Paola Rossetti, Fabrizio Paganucci and Mariano Andrenucci, Centrospazio, Via Gherardesca 5, I-56014, Pisa, Italia

2001-135: PLASMA DIAGNOSTICS IN AN APPLIED FIELD MPD THRUSTER; G. Serianni and N. Vianello, Consorzio RFX, Associazione Euratom-ENEA sulla Fusione, Corso Stati Uniti, 4, 35127 Padova, Italy; F. Paganucci, P. Rossetti, and M. Andrenucci, CENTROSPAZIO, Via A. Gherardesca, 5, 56014 Pisa; V. Antoni and M. Bagatin, Consorizo RFX, Associazione Euratom-ENEA sulla Fusione, INFM, UnitÃ¡ di Padova, Sez. A, Italy

2001-139: SELF-APPLIED MAGNETIC FIELD INTENSITY EFFECTS ON SOLID PROPELLANT MPD THRUSTER PERFORMANCE; Luigi Petrucci and Giorgio Paccani, UniversitÃ¡ degli Studi di Roma “La Sapienza”, Dipartimento Meccanica e Aeronautica, Via Eudossiana 18, 00184 Rome, Italy

2001-140: SELF-APPLIED MAGNETIC FIELD EFFECTS ON SOLID PROPELLANT MPD THRUSTER PERFORMANCE; Giorgio Paccani and Luigi Petrucci, UniversitÃ¡ degli Studi di Roma “La Sapienza”, Dipartimento Meccanica e Aeronautica, Via Eudossiana 18, 00184 Rome, Italy

2001-142: ATTILA-ADJUSTABLE THROTTLE INDUCTIVELY AFTERBURNING ARC JET; Stefan Laure, Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany; JÃ¶rg Heiermann, Monika Auweter-Kurtz, and Helmut Kurtz, Institut fÃ¼r Raumfahrtsysteme (IRS), UniversitÃ¤t Stuttgart, Germany

2001-145: PERFORMANCES AND DESIGN STUDIES STATUS OF THE P4S-1 THRUSTER; H. Brito, Instituto Universitario AeronÃ¡utico, Av. Fuerza AÃ©rea Argentina, km 5.5, (5016) CÃ³rdoba, Argentina; S. Elaskar, Instituto Universitario AeronÃ¡utico, Departmento de AeronÃ¡utica, Universidad Nacional de CÃ³rdoba, Av. Velez Sarfield 1600, (5000), CÃ³rdoba, Argentina; C. Brito, ENSAE, Toulouse, France, R. Ballete, Departmento de AeronÃ¡utica, Universidad Nacional de CÃ³rdoba, Av. Velez Sarfield 1600, (5000), CÃ³rdoba, Argentina

2001-146: SIMPLE AND EFFICIENT CIRCUIT FOR THE INITIATION PROCESS OF AN ABLATIVE PULSED PLASMA THRUSTER (APPT); Roberto Manno, Carlos Fiala, and Carlos Bortis, Facultad de IngenierÃa, Ruta 35 Km 601 (5800), RÃo Cuarto Argentina, Universidad Nacional de RÃo Cuarto

2001-147: EVALUATION OF ALTERNATE PROPELLANTS FOR PULSED PLASMA THRUSTERS; Eric J. Pencil and Hani Kamhawi, National Aeronautics and Space Administration, Glenn Research Center, 21000 Brookpark Road, Cleveland, OH 44135

2001-148: IMPACT OF PERFORMANCE SCALING ON MISSION ANALYSIS FOR GAS-FED PULSED PLASMA THRUSTERS; John K. Ziemer, Jet Propulsion Laboratory, M/S 125-109; California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109; Rodney A. Petr, Science Research Laboratory, Inc., Sommerville, MA 02143

2001-150: DEVELOPMENT OF A MULTIPLEXED COAXIAL PULSED PLASMA THRUSTER; Darren M. King, Wayne C. Solomon, and David L. Carroll, CU Aerospace, Urbana, IL 61802; Rodney L. Burton, Erik L. Antonsen, and Filip Rysanek, University of Illinois at Urbana-Champaign, Urbana, IL 61801; John Frus, Unison Industries, Jacksonville, FL 32256

2001-151: PERFORMANCE AND HEAT LOSS OF A COAXIAL TEFLON PULSED PLASMA THRUSTER; Filip Rysanek and Rodney Burton, University of Illinois Urbana-Champaign, 306 Talbot Lab, 104 South Wright St., Urbana, IL 61801

2001-152: PERFORMANCE IMPROVEMENT OF PULSED PLASMA THRUSTER FOR MICRO SATELLITE; Miwa Igarashi, Naoki Kumagai, Kensuke Sato, Kouji Tamura, and Hanuki Takegahara, Tokyo Metropolitan Institute of Technology, Asahigaoka 6-6, Hino, Tokyo 191-0065, Japan; Hiroyuki Okamoto, Astro Research Corporation, Kugenuma Tachibana 1-1-4, Fujisawa, Kanagawa, 251-0024, Japan; Takashi Wakizono, HI-SERVE Corporation, Totohara 780-7, Akiruno, Tokyo, 190-0152, Japan; Hidekazu Hashimoto, National Space Development Agency of Japan, Office of Research and Development, Advanced Mission Research Center, Micro Space Systems Laboratory, Sengen, 2-1-1, Tsukuba, Ibaraki 305-0047, Japan

2001-153: EVALUATION OF PULSED PLASMA THRUSTER SYSTEM FOR Âµ-LAB SAT II; Haruki Takegahara, Miwa Igarashi, Naoki Kumagai, Kensuke Sato, and Kouji Tamura, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., Asahigaoka 6-6, Hino, Tokyo 191-0065, Japan; Mitsuteru Sugiki, Astro Research Corporation, Kugenuma Tachibana 1-1-4, Fujisawa, Kanagawa, 251-0024, Japan; Hidekazu Hashimoto, National Space Development Agency of Japan, Advanced Mission Research Center, Micro Space Systems Laboratory, Sengen, 2-1-1, Tsukuba, Ibaraki 305-0047, Japan

2001-154: A HIGH-ORDER DISCONTINUOUS GALERKIN METHOD FOR MODELING MICRO-PULSED PLASMA THRUSTERS; G. Lin and G. E. Karniadakis, Division of Applied Mathematics, Brown University, Providence, RI 02912

2001-155: ANALYSES OF TEFLON SURFACE CHARRING AND NEAR FIELD PLUME OF A MICRO-PULSED PLASMA THRUSTER; Michael Keidar and Ian D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109; Frank S. Gulczinski III, Erik L. Antonsen and Gregory G. Spanjers, Air Force Research Laboratory, Propulsion Directorate, Electric Propulsion Laboratory, Edwards AFB, CA 93524

2001-156: DOUBLE DISCHARGE OPERATION FOR PULSED PLASMA THRSUTERS; Maki Okada, Yasushi Okawa, and Takeshi Tachibana, Kyushu Institute of Technology, 1-1, Sensuicho, Tobata, Kitakyushu 804-8550, Japan

2001-157: HIGH RESOLUTION LASER DIAGNOSTICS IN MILLIMETER-SCALE MICRO PULSED PLASMA THRUSTERS; Erik L. Antonsen and Rodney L. Burton, University of Illinois at Urbana-Champaign, IL 61801; Gregory G. Spanjers, AFRL Propulsion Directorate, Edwards AFB, CA 93524

2001-159: TWO-DIMENSIONAL NUMERICAL SIMULATION OF COAXIAL APPT; G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; M. N. Kazeev and V. F. Kozlov, Russian Research Centre “Kurchatov Institute,” 1, Kurchatov sq,. Moscow, 123182, Russia

2001-161: SOLUTION OF REAL MAGNETOGASDYNAMICS EQUATIONS USING A TVD SCHEME AS A TOOL FOR ELECTRIC PROPULSION; Sergio A. Elaskar, Departamento de AeronÃ¡utica, Universidad Nacional de CÃ³rdoba, Av. Velez Sarfield 1601,CÃ³rdoba (5000), Argentina; Hector H. Brito, Centro de Investigaciones Aplicadas, Instituto Universitario AeronÃ¡utico, Ruto 20, km. 5.5, CÃ³rdoba (5022), Argentina

2001-162: EXPERIMENTAL AND THEORETICAL INVESTIGATION OF A COAXIAL INVERSE-PINCH PULSED PLASMA THRUSTER II; Hani Kamhawi, The Ohio State University, Columbus, OH 43220; Pavlos G. Mikelides, Ohio Aerospace Institute, Brook Park, OH 44142; Peter J. Turchi, Los Alamos National Laboratory

2001-163: EXPERIMENTAL STUDY OF PLASMA PARAMETERS IN HIGH-EFFICIENCY PULSED PLASMA THRUSTERS; Garri Popov, Nikolay Antropov, Grigory Dyakonov, Michail Orlov, Valery Tyutin, and Vladimir Yakovlev, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2001-165: THE AFRL TECHSAT 21 PROPULSION SUBSYSTEM DEVELOPMENT PROGRAM; Daron R. Bromaghim and Greg G. Spanjers, Air Force Research Laboratory, AFRL/PRSS, 1 Ara Road, Edwards AFB, CA 93524-7013; Lee K. Johnson, The Jet Propulsion Laboratory, M/S 125-721, 4800 Oak Grove Drive, Pasadena, CA 91106; Ricardo Gorecki, F. Dong Tan, and Robert Vondra, TRW, One Space Park, Redondo Beach, CA, 90278; Bruce Pote, Busek Co., Inc., 11 Tech Circle, Natick, MA, 01760; Joe Barbarits, Moog, Inc., Space Products Division, East Aurora, NY 14052

2001-166: AFRL MICROPPT DEVELOPMENT FOR THE TECHSAT 21 FLIGHT; Gregory G. Spanjers, Daron R. Bromaghim, Capt. James Lake, and Michael Dulligan, AFRL Propulsion Directorate, Edwards AFB, CA 93524; David White, John H. Schiling, and Stewart Bushman, W.E. Research, Rosamond, CA

2001-167: PLASMA PROPULSION ON STENTOR SATELLITE: IN FLIGHT ACCEPTANCE OPERATIONS AND EXPERIMENTAL PROGRAM; Franck Darnon, Luc Petitjean, Jean-Pierre Diris, Jacques Hoarau, and Louis Torres Centre National d’Etudes Spatiales, 18 av. E. Belin, 31401 Toulouse, France; Thierry Grassin, Alcatel Space, 100 Bd du Midi, 06159 Cannes, France

2001-169: PROPULSION INSTRUMENTS FOR SMALL HALL THRUSTER INTEGRATION; Lee. K. Johnson and David G. Conroy, The Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109-8099; Greg G. Spanjers and Daron R. Bromaghim, Air Force Research Laboratory, AFRL/PRSS, 1 Ara Road, Edwards AFB, CA 93524-7013

2001-170: CONCEPTUAL DESIGN OF A SYNERGISTIC PROPULSION SYSTEM FOR THE INTERNATIONAL SPACE STATION (ISS); Jochen Wilms, Arndt HinÃ¼ber, Godehard Nentwig, and Monkia Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme (Space Systems Institute), Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2001-172: SYSTEMS-LEVEL TRADE STUDIES OF A DUAL-MODE SPT FOR GEOSYNCHRONOUS COMMUNICATIONS SATELLITES; J. Steven Snyder, Tom Randolph, David Oh, Birgit Sauer, and Guenter Fischer, Space Systems/Loral, 3825 Fabian Way, Palo Alto, CA

2001-173: ANALYTIC OPTIMIZATION OF MIXED CHEMICAL-ELECTRIC ORBIT RAISING MISSIONS; David Y. Oh, Glenn Santiago, Space Systems/Loral, 3825 Fabian Way M/S G-80, Palo Alto, CA

2001-174: TECHNOLOGICAL READINESS OF MICROWAVE ION ENGINE SYSTEM FOR MUSES-C MISSION; Kyoichiro Toki, Hitoshi Kuninaka, Kazutaka Nishiyama, and Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Ikkoh Funaki, University of Tsukuba, 1-1-1, Tennodai, Tsukuba, Ibraki 305-8577, Japan

2001-175: EVALUATING ADVANCED PROPULSION SYSTEMS FOR THE TITAN EXPLORER MISSION; Muriel Noca and Robert Frisbee, Jet Propulsion Laboratory, California Institute of Technology, MS 301-180, MS 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106; Les Johnson and Larry Kos, Mail Code TD15, Bldg. 4203, Mail Code TD30, Bldg. 4203, Marshall Space Flight Center, Huntsville, AL 35812; Leon Gefert and Len Dudzinski, NASA Glenn Research Center, MS 86-15, 21000 Brookpark Rd., Cleveland, Ohio 44135

2001-176: ION PROPULSION TECHNOLOGY FOR FAST MISSIONS TO PLUTO; Dave Rodgers and John Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

2001-177: A POSSIBLE ASTEROID RENDEZVOUS MISSION LAUNCHED AS AN ARIANE 5 AUXILIARY PAYLOAD; David G. Fearn, Space Department, QinetiQ, Farnborough, Hants, GU14 0LX, UK; Nigel S. Wells, Space Department QinetiQ, Farnborough, Hants, GU14 0LX, UK

2001-179: OUTER PLANET EXPLORATION WITH ADVANCED RADIOISOTOPE ELECTRIC PROPULSION; Steve Oleson, Leon Gefert, Michael Patterson, Jeffrey Schreiber, and Scott Benson, National Aeronautics and Space Administration, Glenn Research Center, MS 500-203, 21000 Brookpark Rd., Cleveland, OH 44135; Jim McAdams and Paul Ostdiek, The Johns Hopkins University, Applied Physics Laboratory, 11100 Johns Hopkins Road, Laurel, MD 20723-6099

2001-181: OPTIMIZATION OF ELECTRIC THRUSTERS FOR PRIMARY PROPULSION BASED ON THE ROCKET EQUATION; Monkia Auweter-Kurtz and Helmut Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

2001-182: ABLATIVE PULSED PLASMA THRUSTER SYSTEM OPTIMIZATION FOR MICROSATELLITES; Paolo Gessini, Astronautics Research Group, School of Engineering Sciences, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, United Kingdom; Giorgio Paccani, Dipartimento di Meccanica e Aeronautica, UniversitÃ¡ degli Studi di Roma “La Sapienza”, Via Eudossiana 18, 00184 Rome, Italy

2001-187: ELECTRIC PROPULSION FOR A REUSABLE SPACE CARGO; Ivo Vieira, GoLP – Grupo de Lasers e Plasmas, Centro de Fisica de Plasmas, Complexo Interdisciplinar, Piso 2, Instituto Superior TÃ©nico, Av. Rovisco Pais, 1049-001, Lisboa - Portugal

2001-191: EVAPORATION – TYPE RESISTOR THRUSTER WITH THERMAL CATALYTIC DECOMPOSITION OF HYDRAZINE; V.N. Vinogradov, B. E. Didenko, V. M. Murashko, and A. G. Njatin, EDB FAKEL, Russian Federation, Kaliningrad, 236000, Moskovsky prospect, 181

2001-192: MULTI-HOUR TEST OF TUNSTEN ANODES FOR A LOW POWER DC ARCJET; Kiyoshi Kinefuchi, Ikkoh Funaki and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagaw, 229-8510, Japan; Yasuyuki Suwama, NEC Aerospace Systems, LTD., 1-10 Nisshin, Fuchu, Tokyo, 183-8501, Japan; Kenichi Okamoto, Allied Material Corporation, 2 Iwasekoshi-machi, Toyama-shi, Toyama, 931-8371, Japan

2001-193: NUMERICAL STUDIES ON EFFECT OF NOZZLE GEOMETRY AND OF FLOW CONTINUITY ON THRUST PERFORMANCE; S. Hatta and S. Aso, Space Transportation Systemd Engineering Laboratory, Department of Aeronautics and Astronautics, Kyushu University, 6-10-1 Hakozaki, Higashi-ku, Fukuoka-shi, 812-8581, Japan

2001-194: NON-EQUILIBRIUM NUMERICAL STUDY OF A TWO-STAGE MICROWAVE ELECTROTHERMAL THRUSTER; V. P. Chiravalle, R. B. Miles and E. Y. Choueiri, Princeton University, Princeton, NJ 08544

2001-195: DIAGNOSTICS OF ATOMIC OXYGEN IN ARC-HEATER PLUMES; Makoto Matsui, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Tokyo, 7-3-1 Hongo, Bunkyo, Tokyo 113-8656, Japan; Masahito Mizuno, National Aerospace Laboratory of Japan (NAL), 7-44-1 Jindaiji Higashi-machi, Chofu, Tokyo, 182-8522, Japan

2001-196: CHARACTERISTICS OF TIN COATINGS BY GAS TUNNEL TYPE PLASMA REACTIVE SPRAYING; Akira Kobayashi, Joining and Welding Research Institute, Osaka University, 11-1 Mihogaoka, Ibaraki, Osaka 567-0047, Japan

2001-200: COMPUTER MODELING OF THE LABORATORY TESTING OF MINI-MAGNETOSPHERIC PLASMA PROPULSION (M2P2); R. M. Winglee and P. Euripides, Department of Earth and Space Sciences, Univeristy of Washington, Seattle, WA 98145-1650; J. Slough and T. Ziemba, Department of Aeronautics and Astronautics, University of Washington, Seattle, WA 98195-2400

2001-201: PARAMETERIZATION OF THE LABORATORY PERFORMANCE OF THE MINI-MAGNETOSPHERIC PLASMA PROPULSION (M2P2) PROTOTYPE; T. M. Ziemba and J. Slough, Department of Aeronautics and Astronautics, University of Washington, Box 352400, Seattle, WA 98195-2400; R. M. Winglee and P. Euripides, Department of Earth and Space Science, University of Washington, Box 351650, Seattle, WA 98195-2400

2001-202: HIGH BETA PLASMA FOR INFLATION OF A DIPOLAR MAGNETIC FIELD AS A MAGNETIC SAIL; John Slough, Redmond Plasma Physics Laboratory, University of Washington, 14700 NE 95^th Street, Redmond, WA 98052

2001-205: PRESSURE WAVES IN A FAR-FIELD REPETITIVE PULSE LASER THRUSTER; Koichi Mori, Hiroshi Katsurayama, Kimiya Komuraski, and Yoshihiro Arakawa, University of Tokyo, Hongo 7-3-1, Bunkyo, Tokyo 113-8656, Japan

2001-207: THRUST MEASUREMENT OF A CW LASER THRUSTER IN VACUUM; Kazuhiro Toyoda, Kyushu Institute of Technology, Komurasaki Kimiya and Yoshihiro Arakawa, University of Tokyo

2001-208: NUMERICAL STUDY OF PLASMA PRODUCTION IN THE VASIMR THRUSTER; Oleg Batishchev and Kim Molvig, Massachusetts Institute of Technology, Nuclear Engineering Department, MIT NW 16-258, 167 Albany St., Cambridge, MA 02139, USA

2001-209: ION ACCELERATION BY BEATING ELECTROSTATIC WAVES: CRITERIA FOR REGULAR AND STOCHASTIC ACCELERATION; R. Spektor and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2001-210: THE POTENTIAL FOR COMPACT HELICON WAVE SOURCES FOR ELECTRIC PROPULSION; Jim Gilland, Ohio Aerospace Institute, NASA Glenn Research Center, Cleveland, OH 44142

2001-211: A THEORETICAL ANALYSIS OF VACUUM ARC THRUSTER PERFORMANCE; James E. Polk, Mike Sekerak, and John K. Ziemer, Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109, Jochen Schein, Niansheng Qi and Robert Binder, Alameda Applied Sciences Corp, 2235 Polvorosa Ave. San Leandro, CA 94577; AndrÃ© Anders, Lawrence Berkeley National Laboratory, 1 Cyclotron Road, Berkeley, CA 94720

2001-214: OPPOSED-CAVITY SOLAR THERMAL THRUSTER MADE OF SINGLE CRYSTAL TUNGSTEN; Hironori Sahara, Japan Science and Technology Corporation (JST), 7-44-1, Jindaiji-Higashi-Machi, Chofu, Tokyo, 182-8522, Japan; Morio Shimizu, National Aerospace Laboratory of Japan (NAL), Japan; Tadayuki Fujii, National Institute of Materials Science (NIMS), Japan, Ken-ichi Okamoto, Shigehiko Takaoka, Allied Material Corporation, Japan; Yoshihiro Nakamura, Hosei University, Japan

2001-220: A DIODE-LASER-DRIVEN MICROTHRUSTER; Claude R. Phipps, Photonic Associates, 200A Ojo de la Vaca Road, Santa Fe, NM 87508; James R. Luke and G. Glen McDuff, UNM/New Mexico Engineering Research Institute, 901 University Blvd. SE, Albuquerque, NM 87106-4339

2001-221: COMPACT PLASMA ACCELERATOR FOR MICRO-PROPULSION APPLICATIONS; John e. Foster, NASA Glenn Research Center, Cleveland, OH 44135, USA

2001-223: DIODE LASER DRIVEN MICROTHRUSTER PROTOTYPE; James R. Luke, UNM/New Mexico Engineering Research Institute, 901 University Blvd. SE, Albuquerque, NM 87109-4339; Claude R. Phipps, Photonic Associates, 200A Ojo de la Vaca Road, Sante Fe, NM 87505; G. Glen McDuff, UNM/New Mexico Engineering Research Institute, 901 University Blvd. SE, Albuquerque, NM 87106-4339

2001-224: DEVELOPMENT OF MICROWAVE ENGINE; Shin Satori, Hokkaido Institute of Technology, Hiroyuki Okamoto, Ted Mitsuteru Sugiki, and Yasumasa Ito, Astro Research Corporation; Yoshinori Aoki, Atsushi Nagata, and Takayoshi Kizaki, Advanced Technology Institute, 7-15-4-1, Maeda, Teine, Sapporo, Hokkaido 006-8585, Japan

2001-226: HOLLOW CATHODE MICRO-THRUSTER PERFORMANCE; Michael J. Patterson and John E. Foster, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, OH 44135

2001-228: LOW MASS VACUUM ARC THRUSTER SYSTEM FOR STATION KEEPING MISSION; Jochen Schein, Niansheng Qi, Robert Binder, and Mahadevan Krishnan, Alameda Applied Sciences Corp, 2235 Polvorosa Ave, San Leandro, CA 94577; John K. Ziemer and James E. Polk, NASA Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91109; AndrÃ© Anders, Lawrence Berkeley National Laboratory, 1 Cyclotron Road, Berkeley, CA 94720

2001-231: STUDY OF VERY LOW-POWER DC PLASMA-JET MICROTHRUSTERS; Hideyuki Horisawa, Department of Aerospace Engineering, Tokai University, 1117 Kitakaname, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, and Nara Textile Inc., 4-19-4 Nakahara, Isogo, Yokohama, 235-0036, Japan

2001-232: TEMPERATURE AND POWER PREDICTIONS FOR FLIGHT-TESTING THE FREE MOLECULE MICRO-RESISTOJET; Joyce Wong and Helen Reed, Arizona State University, Mechanical & Aerospace Engineering, Campus Box 6106; Andrew Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards AFB, CA 93524

2001-233: THE HOLLOW CATHODE AS A MIRCO-ION THRUSTER; Paolo Gessini and Stephen B. Gabriel, Astronautics Research Group, School of Engineering Sciences, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, United Kingdom; David G. Fearn, Space Department, Y72 Building, QinetiQ, Farnborough, Hants, GU14 0LX, United Kingdom

2001-234: CONCEPTUAL DESIGN OF AN ION MICROTHRUSTER; K. G. Hutchison and S. B. Gabriel, School of Engineering Sciences, University of Southampton, Southampton, Hants, SO17 3QX, UK

2001-235: A TORSIONAL BALANCE THAT RESOLVES SUB-MICRO-NEWTON FORCES; Manuel Gamero-CastaÃ±o and Vlad Hruby, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023; Manuel Martinez-SÃ¡nchez, Massachusetts Institute of Technology, 77 Massachusetts Ave., 37-401, Cambridge, MA 02139

2001-236: ACCURATE MEASUREMENT OF NANO-NEWTON THRUST FOR MICROPROPULSION SYSTEM CHARACTERIZATION; Andrew J. Jamison and E. P. Muntz, Department of Aerospace and Mechanical Engineering, University of Southern California, Los Angeles, CA 90089-1191; Andrew D. Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards AFB, CA 93524

2001-238: PERFORMANCE MEASUREMENTS USING A SUB-MICRONEWTON RESOLUTION THRUST STAND; John K. Ziemer, Jet Propulsion Laboratory, M/S 125-109, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109

2001-240: PROPULSIVE SMALL EXPANDABLE DEPLOYER SYSTEM (PROSEDS): PREPARING FOR FLIGHT; Brian Gilchrist, Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109-2143; Judy Balance, Leslie Curtis, Les Johnson, Jason Vaughn, and Ken Welzyn, Marshall Space Flight Center, National Aeronautics and Space Administration, Huntsville, AL 35812

2001-242: EVALUATION OF PLASMA CONTACTOR GROUND EXPERIMENTS FOR ELECTRODYNAMIC TETHER; Masaya Kozakai and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan

2001-243: KINETIC MODELING OF THE ELECTRON CURRENT COLLECTION TO A MOVING BARE ELECTRODYNAMIC TETHER; Eric ChoiniÃ©re and Brian E. Gilchrist, Radiation Laboratory, EECS Department, University of Michigan, 1301 Beal Avenue, Ann Arbor, MI 48109-2122

2001-244: PERFORMANCE OF ELECTRODYNAMIC TETHER DE-ORBIT SYSTEM ON ELLIPTICAL ORBIT; Yoshiki Yamagiwa, Ryosuke Tuyuki, Shinichi Takenaka and Eiji Hiragi, Faculty of Engineering, Shizuoka University, 3-5-1, Johoku, Hamamatsu, Shizuoka 432-8561, Japan

2001-245: PIC COMPUTATION OF ELECTRON CURRENT COLLECTION TO A MOVING BARE TETHER IN THE MESOTHERMAL CONDITION; Tatsuo Onishi and Manuel MartÃnez-SÃ¡nchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, USA; David L. Cooke, Air Force Research Laboratory, Space Vehicle Directorate, Hanscom AFB, MA, USA; Juan R. SanmartÃn, Universidad PolitÃ©cnica de Madrid, Spain

2001-251: A HALL-EFFECT THRUSTER PLUME AND SPACECRAFT INTERACTIONS MODELING PACKAGE; I. G. Mikellides, G. A. Jongeward, G. A., B. M. Gardner, I. Katz, M. J. Mandell and V. A. Davis, Science Applications International Corporation, 9455 Towne Center Drive, MS W2076, San Diego, CA 92121

2001-252: CORRELATION OF HOLLOW CATHODE ASSEMBLY AND PLASMA CONTACTOR DATA FROM GROUND TESTING AND IN-SPACE OPERATION ON THE INTERNATIONL SPACE STATION; Scott D. Kovaleski, QSS Group, Inc., NASA Glenn Research Center Group, 21000 Brookpark Rd, MS 301-3, Cleveland, OH 44135; Michael J. Patterson and George C. Soulas, NASA Glenn Research Center, 21000 Brookpark Rd., MS 301-3, Cleveland, OH 44135

2001-254: EXPANSION OF SECONDARY PLASMA GENERATED IN AN EP PLUME. THEORY AND EXPERIMENT; B. S. Borisov, A. G. Korsun, F. F. Gabdullin, N. V. Kozyrev, A. V. Semenkin, and E. M. Tverdokhlebova, Central Research Institute of Machine Building (TSNIIMASH), 141070 Korolev, Moscow region, Russia

2001-257: METHODS FOR INVESTIGATING THE INFLUENCE OF SELF-INDUCED ELECTROMAGNETIC EMISSION OF ELECTRIC PROPULSIONS UPON THE SENSITIVITY CHARACTERISTICS OF ONBOARD RADIO SYSTEMS OF SPACECRAFTS; A. P. Plokhikh, N. A. Vazhenin, and G. V. Soganova, Research Institute of Applied Mechanics and Electrodynamics (RIAME), P.O. Box 43, Moscow 125080, Russia

2001-258: MITIGATION PROCESS OF SPACECRAFT NEGATIVE CHARGING BY PLASMA FLOW; Hirokazu Tahara, Daiki Matsuyama, Toshiaki Yasui and Takao Yoshikawa, Division of Mechanical Science, Dept. of Systems and Human Science, Graduate School of Engineering Science, Osaka University, 1-3 Machikaneyama Toyonaka, Osaka 560-8531, Japan

2001-260: PLASMA PLUME FAR FIELD ANALYSIS; J. Ashkenazy, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel; A. Fruchtman, Holon Academic Institute of Technology, Holon 58102, Israel

2001-261: SOLUTION OF REAL MAGNETOGASDYNAMICS EQUATIONS USING A TVD SCHEME AS A TOOL FOR ELECTRIC PROPULSION; Sergio A. Elaskar, Departamento de AeronÃ¡utica, Universidad Nacional de CÃ³rdoba Av. Velez Sarfield 1601, CÃ³rdoba (5000), Argentina; HÃ©ctor H. Brito, Centro de Investigaciones Aplicadas, Instituto Universitario AeronÃ¡utico, Ruta 20 km, 5.5, CÃ³rdoba (5022), Argentina

2001-262: PPS EFFEXTS ON SATELLITES ANALYSES AND TOOLS IN ALCATEL SPACE INDUSTRIES; V. Perrin, D. Pogarieloff, P. MÃ©tois, and S. Brosse, Alcatel Space Industries, 100 Bd du Midi 06156 Cannes la Bocca Cedex, France

2001-264: PIC SIMULATIONS OF SPACECRAFT CHARGING AND ITS NEUTRALIZATION PROCESS BY PLASMA EMISSION; Hideyuki Usui, Hiroshi Matsumoto, Makoto Yasugi, and Yoshiharu Omura, Radio Science Center for Space and Atmosphere, Kyoto University, Gokasho, Uji, Kyoto 611-0011, Japan

2001-270: RECENT DEVELOPMENT ACTIVITIES IN HOLLOW CATHODE TECHNOLOGY; Michael J. Patterson and Matthew T. Domonkos, National Aeronautics and Space Administration, Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, Ohio 44135; Christian Carpenter and Scott d. Kovaleski, QSS Group, Inc., Cleveland, Ohio

2001-271: A REVIEW OF TESTING OF HOLLOW CATHODES FOR THE INTERNATIONAL SPACE STATION PLASMA CONTACTOR; S. D. Kovaleski, QSS Group, Inc., NASA Glenn Research Center Group, 21000 Brookpark Rd., Cleveland, OH 44135; M. J. Patterson, G. C. Soulas, and T. R. Sarver-Verhey, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135

2001-272: THE RESULTS OF RESEARCHING OF LOW-CURRENT SELFHEATED HOLLOW CATHODES ON ELECTRIC CURRENT RANGE FROM 0,3 UP TO 0,5 A; Dr. Loyan A., Koshelev N., STC SPE “KhAI”, 17, Chkalova st., 310070, Kharkov, Ukraine

2001-273: HIGH-CURRENT SELF-HEATED HOLLOW CATHODES WITH OPERATION CURRENT MORE THAN 25 A. STATE AND DEVELOPMENT; Dr. Loyan A., Dr. Oransriy A., and Ichenko E., STC SPE “KhAI”, 17, Chkalova st. 310070, Kharkov, Ukraine

2001-274: HIGH-CURRENT HOLLOW CATHODE DEVELOPMENT; Christian B. Carpenter, QSS Group, Inc., MS 16-1, 21000 Brookpark Rd., Cleveland, OH 44135; Michael J. Patterson, NASA Glenn Research Center, MS 301-3, 21000 Brookpark Rd., Cleveland, OH 44135

2001-276: LIFE MODEL OF HOLLOW CATHODES USING A BARIUM CALCIUM ALUMINATE IMPREGNATED TUNGSTEN EMITTER; S. D. Kovaleski, QSS Group, Inc., NASA Glenn Research Center Group, 21000 Brookpark Rd., Cleveland, OH 44135

2001-277: ON THE HOLLOW CATHODE FOR AN OXYGEN DISCHARGE; Yoshihiro Nakamura and Teruaki Sue, Department of Mechanical Engineering, Hosei University, 3-7-2, Kajino-cho, Koganei, Tokyo 184-8584, Japan

2001-278: EXPERIMENTAL PERFORMANCE EVALUATIONS OF MO AND ZRC-COATED MO FIELD EMISSION ARRAY CAHTODES IN OXYGEN ENVIRONMENTS; Colleen Marrese-Reading and Jay Polk, Jet Propulsion Laboratory (JPL), California Institute of Technology, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106; Kevin L. Jensen, Naval Research Laboratory, Code 6841, ESTD, Washington, DC 20375-5347

2001-279: DEVELOPMENT OF FIELD EMITTER ARRAY TECHNOLOGY FOR ED TETHER PROPULSION; Dave Morris and Brian Gilchrist, Space Physics Research Laboratory, University of Michigan, Ann Arbor, MI 48109; Alec Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109

2001-280: PRELIMINARY RESULTS OF FIELD EMISSION CATHODE TESTS; James S. Sovey, NASA Glenn Research Center; Scott D. Kovaleski, QSS Group at NASA Glenn Research Center, MS 301-3, 21000 Brookpark Road, Cleveland, OH 44135

2001-281: MICRO NEWTON COLLOID THRUSTER SYSTEM DEVELOPMENT; Vlad Hruby, Manuel Gamero-CastaÃ±o, Paul Falkos, and Suren Shenoy, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-282: CHARACTERIZATION OF A COLLOID THRUSTER PERFORMING IN THE MICRO-NEWTON THRUST RANGE; Manuel Gamero-CastaÃ±o and Vladimir Hruby, Busek Co. Inc., 11 Tech Circle, Natick, Massachusetts 01760

2001-283: CHARACTERIZATION OF ELECTROSPRAYS AND ITS RELEVANCE TO COLLOID THRUSTERS; Manuel Gamero-CastaÃ±o and Vladimir Hruby, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2001-284: PERFORMANCE STUDIES OF A COLLOID THRUSTER SYSTEM; Freddy M. Pranajaya and Mark A. Cappelli, Thermosciences Division, Mechanical Engineering Department, Stanford University, Building 520, Stanford, CA 94309-3032

2001-286: THE EFFECT OF USING FINITE-WIDTH ELECTROSTATIC GATES IN TIME-OF-FLIGHT MEASUREMENTS FOR COLLOID THRUSTERS; Paulo Lozano and Manuel Martinez-SÃ¡nchez, Massachusetts Institute of Technology, Room 37-438, 70 Vassar St., Cambridge, MA 02139

2001-288: FEEP-5 THRUST VALIDATION IN THE 10-100ÂµN RANGE WITH A SIMPLE NULLED-PENDULUM THRUST STAND: INTEGRATION PROCEDURES; D. Nicolini, E. Chesta, J. Gonzalez del Amo, and G. Saccoccia, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands; E. B. Hughes and S. Oldfield, National Physical Laboratory, Dimensional Metrology Section, Queens Road, Teddington, TW11 0LW Middlesex, United Kingdom

2001-289: INDIUM FEEP ENDURANCE TEST: PRELIMINARY RESULTS; Angelo Genovese, Martin Tajmar, and Wolfgang Steiger, ARC Seibersdorf research GmbH, A-2444 Seibersdorf, Austria; Friedrich RÃ¼denauer, International Atomic Energy Agency, A-2444 Seibersdorf, Austria

2001-290: IN-FEEP THRUSTER ION BEAM NEUTRALIZATION WITH THERMIONIC AND FIELD EMISSION CATHODES; Colleen Marrese-Reading, Jay Polk, Juergen Mueller, and Al Owens, Jet Propulsion Laboratory (JPL), California Institute of Technology, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91106; Martin Tajmar, ARC Seibersdorf Research GmbH, A-2444 Seibersdorf, Austria; Capp Spindt, SRI International, Bldg. 320T, 333 Ravenswood Ave., Menlo Park, CA 94025; Richard Fink, Field Emission Picture Element Technology (FEPET) Inc., 3006 Longhorn Blvd. Suite 107, Austin, TX 78758-7631

2001-291: PLUME CHARACTERISTICS OF THE INDIUM NEEDLE EMITTER (InFEEP) THRUSTER; D. Nicolini, E. Chesta, and J. Gonzalez del amo, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2001-295: FEEP THRUSTER SURVIVABILITY IN THE LEO ATOMIC OXYGEN ENVIRONMENT; Fabioo Ceccanti, Salva Marcuccio, and Mariano Andrenucci, Centrospazio – Alta S.r.l., Via Gherardesca 5, 56014 Ospedaletto, Pisa, Italy

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2003 INDEX

2003-003: OPTIMIZATION OF GEOGYNCHRONOUS SATELLITE SYSTEM USING ELECTRIC PROPULSION BASED ON GENETIC ALGORITHM; Han Xianwei, He Hongqing, Tang Jinlan Mao, Genwang, and Yang Juan, College of Astronautics, Northwestern Polytechnical University, Xi’an, P. R. Chine, 710072

2003-005: COMBINING ELECTRIC AND SAIL PROPULSION FOR INTERPLANETARY SAMPLE RETURN; Robert J. Noble, Stanford Linear Accelerator Center, Stanford University, 2575 Sand Hill Road, Menlo Park, California 94025 USA

2003-007: ABOUT MODEL OF JET PROPULSION; Kolgotin O. V., Engineer, Postgraduate Student Moscow aviation institute, Russia, Pensa, ul.Stavskogo 12-125 440008

2003-008: SPACE TRANSPORTER; Kolgotin O., The Moscow aviation institute (Technical University)

2003-011: NUMERICAL INVESTIGATION OF A HALL THRUSTER PLASMA INCLUDING SPUTTER YIELD, Subrata Roy and B. P. Pandey, Computational Plasma Dynamics Laboratory, Kettering University, 1700 West Third Avenue, Flint, MI 48504

2003-014: MULTI-FLUID SHEATH MODEL FOR ELECTRIC PROPULSION DEVICES; Subrata Roy and B. P. Pandey, Computational Plasma Dynamics Laboratory, Kettering University, 1700 West Third Avenue, Flint, MI 48504

2003-015: OPTIMIZATION ON MAGNETIC FIELD AND ACCELERATION CHANNEL FOR LOW POWER HALL THRUSTERS; Hirokazu Tahara, Takashi Fujioka, Takahisa Kitano, Atsushi Shirasaki, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan; Kenji Fuchigami and Fumihiro Ueno, Fujio Iinoya, and,

2003-016: SIMPLE ONE-DIMENSIONAL CALCULATIONS OF HALL THRUSTER FLOWFIELDS; Hirokazu Tahara, Takashi Fujioka, Atsushi Shirasaki and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan; Kenji Fuchigami and Fumihiro Ueno, Technical Research Laboratory, Ishikawajima-Harima Heavy Industries Co., Ltd., 1, Shinnakahara Ishogo, Yokohoma, Kanagawa 235-8501, Japan; Fujio Iinoya, Technologies Development Department, IHI Aerospace Co., Ltd., 1, Shinnakahara, Ishogo, Yokohama, Kanagawa 235-8501, Japan

2003-017: PLASMA CHARACTERISTICS OF QUASI-STEADY MPD ARCJETS FOR MATERIAL PROCESSING; Hirokazu Tahara, Tetsuji Shibata, Kazunori Mitsuo, Atsushi Shirasaki, Yoichi Kagaya, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-019: TRACEABLE, HIGH-ACCURACY THRUST MEASUREMENT FOR ELECTRIC PROPULSION; E. B. Hughes and S. Oldfield, National Physical Laboratory, Queens Road, Teddington, Middlesex, TW11 0LW, UK

2003-021: THERMAL MODELING AND MEASUREMENTS OF AN ENGINEERING MODEL HALL THRUSTER; A. Warshavsky, Manor Division, Rafael, Haifa 31021, Israel; I. Zur, Mechanical CAD Division, Rafael, Haifa 31021, Israel; J. Ashkenazy and G. Appelbaum, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

2003-022: COMPARISON OF ORBIT TRANSFER VEHICLE CONCEPTS UTILIZING MID-TERM POWER AND PROPULSION OPTIONS; Frank S. Gulczinski III, AFRL Propulsion Directorate (AFRL/PRSS), 1 Ara Road, Edwards AFB, CA 93524-7013; John H. Schilling, W. E. Research, 4360 San Juan Ct., Rosamond, CA 93560

2003-024: THE GEAR OF A WORKING GAS FLOW IN THE SPT DISCHARGE CHAMBER; Sergey A. Oghienko and Anatoliy I. Oranskiy, Scientific and Technological Center of Space Power and Engines at Kharkov Aviation Institute, 17, Chkalova St., Kharkov, 61070, Ukraine

2003-027: NUMERICAL SIMULATION OF THE HOLLOW CATHODE PLASMA USING A PIC-DCMC CODE; Francis T. Crawford and Stephen B. Gabriel, School of Engineering Sciences, University of Southampton, UK

2003-028: MOMENTUM AND HEAT FLUX MEASUREMENTS IN THE EXHAUST OF VASIMR USING HELIUM PROPELLANT; D. Gregory Chavers, Research Scientist, Propulsion Research Center, MSFC/NASA, Huntsville, AL; Franklin R. Chang-DÃaz, NASA Astronaut, ASPL Director, JSC/NASA, Houston, TX; Claude Irvine, Research Scientist, Propulsion Research Center, MSFC/NASA, Huntsville, AL; Jared P. Squire, Research Scientist, Advanced Space Propulsion Laboratory, Muniz Engineering, Houston, TX

2003-030: INTERACTIONS WITHIN A CLUSTER OF LOW POWER HALL THRUSTERS; W. A. Hargus, Jr., AFRL/PRSS, 1 Ara Road, Edwards AFB, CA, USA

2003-031: EFFECT OF APPLIED MAGNETIC NOZZLE IN A QUASI-STEADY MPD THRUSTER; Yoichi Kagaya, Hirokazu Tahara, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-032: DEVELOPMENT AND TESTING FOR A HIGH-POWER HALL THRUSTER; Olivier Duchemin and Pierre Dumazert, SNECMA Moteurs, Space Propulsion Division, Spacecraft Propulsion and Equipment, Villaroche Nord, 77550 Moissy-Cramayel, France; S. D. Clark and D. H. Mundy, Space Propulsion, QinetiQ, Farnborough, Hampshire, GU14 0LX, The United Kingdom

2003-033: NUMERICAL SIMULATION OF THE ARTUER-2 ARCJET; J. Heiermann and M. Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany

2003-034: ANALYSIS OF HALL-EFFECT THRUSTERS AND ION ENGINES FOR EARTH-TO-MOON TRANSFER; A. Bober and M. Guelman, Asher Space Research Institute, Technion-Israel Institute of Technology, 32000 Haifa, Israel

2003-035: ENERGY ANALYSIS OF A HALL THRUSTER CLUSTER; Brian E. Beal and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, The University of Michigan, Ann Arbor, MI 48109

2003-036: END TO END OPTIMIZATION OF THREE DIMENSIONAL CHEMICAL-ELECTRIC ORBIT RAISING MISSIONS; David Y. Oh and Scott Kimbrel, Space Systems/Loral, 3825 Fabian Way M/S G-80, Palo Alto, CA 94303-4604; Manuel Martinez-Sanchez, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139

2003-037: RECENT RESULTS FROM INTERNAL AND VERY-NEAR-FIELD PLASMA DIAGNOSTICS OF A HIGH SPECIFIC IMPULSE HALL THRUSTER; Richard R. Hofer, QSS Group, Inc., Cleveland, OH 44135, USA; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109, USA

2003-038: SENSITIVITY OF THE BEHAVIOR OF BACKFLOW CEX IONS TO ION ENGINE PLUME CHARACTERISTICS; M. Matsushiro and M. Nishida, Department of Aeronautics and Astronautics, Kyushu University, Fukuoka 812-8581, Japan; H. Kuninaka and K. Toki, Institute of Space and Astronautical Science, Sagamihara, Kanagawa 229-8510, Japan

2003-039: PROPELLANT ENERGY FLUX MEASUREMENTS IN PULSED PLASMA THRUSTER; Y. A. Alexeev, N. N. Kazeev, and V. F. Kozlov, Russian Research Centre “Kurchatov Institute”, 1, Kurchatov sq., Moscow, 123182, Russia

2003-040: PULSED PLASMA THRUSTER PROPULSION TECHNOLOGY FOR SMALL SATELLITE; Garry A. Popov and Nikolay N. Antropov, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Vladimir P. Khodnenko and Yakov V. Dubrovinskyi, All-Russian Research Institute of Electromechanics, 101000, P.O. Box 496, Moscow, Russia

2003-041: FUNCTIONALLY GRADED THERMAL BARRIER COMPOSITE COATINGS FORMED BY GAS TUNNEL TYPE PLASMA SPRAYING; Akira Kobayashi, JWRI, Osaka University, 11-1 Mihogaoka, Ibaraki, Osaka 567-0047, Japan

2003-043: PULSED PLASMA THRUSTERS FOR SPACE PROPULSION AND INDUSTRIAL PROCESSING; Henri P. Wagner and Monika Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart

2003-048: STENTOR PLASMA PROPULSION SYSTEM EXPERIENCE; Pascal Garnero and Thierry Grassin, ALCATEL SPACE, 100 Bd du Midi, 06159 Cannes, France; F rank Darnon and Luc Petitjean, CNES, Centre Spatial de Toulouse, 18 av. E. Belin, 31401 Toulouse, France

2003-050: TRAJECTORY SIMULATION FOR THRUST-VECTORED ELECTRIC PROPULSION MISSIONS; N. Leveque, C. Welch, A. Ellery, and A. Curley, Kingston University, Astronautics and Space Systems Group, School of Engineering, Friars Avenue, London SW 15 3DW, UK

2003-051: OPERATIONAL CHARACTERISTICS OF CYLINDRICAL HALL THRUSTERS; Atsushi Shirasaki, Hirokazu Tahara, and Takao Yoshikawa, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-052: ANGULAR DISTRIBUTION OF CERAMIC ISOLATOR SPUTTERED MATERIAL IN THE SPT JET; S. A. Khartov, A. B. Nadiradze, and Yu V. Zikeeva, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia; V. K. Egorov, IPMT RAS, Chernogolovka, Moscow Region, Russia

2003-053: INTERACTION BETWEEN HIGH VOLTAGE SOLAR ARRAY AND ION THRUSTER PLASMA; Mengu Cho, Akiyo Saionji, and Kazuhiro Toyoda, Kyushu Institute of Technology; Yukishige Nozaki, NEC Toshiba Space Systems, Ltd., Tetsuo Sato, National Space Development Agency of Japan

2003-056: NOZZLE SHAPE EFFECTS ON VELOCITY DISTRIBUTION IN AN MPD ARCJET; Kiyoshi Kinefuchi and Kyoichiro Toki, Institute of Space and Astronautical Science, Kanagawa, Japan; Ikkoh Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Ibaraki, Japan

2003-057: MICROWAVE HALL THRUSTER DEVELOPMENT; Pedro Molina-Morales, Hitoshi Kuninaka, and Kyoichiro Toki, Institute of Space and Astronautical Science (ISAS), 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2003-058: INVESTIGATION OF DIFFERENT SCHEMES OF GAS DISTRIBUTION IN SPT CHANNEL; Sergey A. Khartov and Alexander B. Perfiliev, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2003-059: SPT CERAMIC ISOLATOR SURFACED LAYER COMPOSITION CHANGE WITH LIFETIME; Sergey Khartov and Andrey Nadiradze, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia; Olivier Duchemin and Snecma Moteurs, Villaroche Nord Plant, Arodrome de Melun-Villaroche 77550, Moissy-Cramayel-France

2003-060: THE RELIABILITY OF THE ELECTRIC PROPULSION PARAMETERS MEASUREMENT INCREASING; S. A. Khartov, L. A. Latyshev, and D. U. Silantiev, Moscow Aviation Institute (technical university) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2003-061: DEVELOPMENT AND REFINEMENT OF HIGHLY EFFICIENT 150 J APPT; N. Antropov, G. Diakonov, M. Orlov, G. Popov, V. Tyutin, and V. Yakovlev, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, post box 43, Moscow, 125080, Russia

2003-062: 30MN-CLASS MICROWAVE DISCHARGE ION THRUSTER; Kazutaka Nishiyama, Hitoshi Kuninaka, Yukio Shimizu, and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-063: ANALYSIS OF THE PLUME DIVERSION IN THE HALL THRUSTER IN THE NEAR AND FAR FIELDS; Avi Cohen-Zur and Alon Gany, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; Amnon Fruchtman, Holon Academic Institute of Technology, P. O. Box 305, Holon 58102, Israel

2003-064: A SIMILARITY PARAMETER FOR CAPILLARY FLOWS OF RELEVANCE TO MICROPROPULSION; Kurt A. Polzin and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2003-065: EFFECTS OF ION COLLISIONS ON ION ACCELERATION BY BEATING ELECTROSTATIC WAVES; R. Spektor and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2003-067: HIGH POWER PROCESSING UNIT FOR STATIONARY PLASMA THRUSTER; E. Bourguignon and T. Scalais, Alcatel ETCA s.a., BP 4008, B-6000, Charleroi (Belgium)

2003-069: DISCHARGE PLASMA PARAMETERS OF A 30-cm ION THRUSTER MEASURED WITHOUT BEAM EXTRACTION USING A HIGH-SPEED PROBE POSITIONING SYSTEM; Daniel A. Herman, Daniel S. McFarlane, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48105, USA

2003-070: NUMERICAL SIMULATION OF TWO-DIMENSIONAL, NON-STEADY IDEAL MAGNETOGASDYNAMICS EQUATIONS; Livio S. Maglione, Facultad de IngenierÃa, Universidad Nacional de RÃo Cuarto; Sergio A. Elaskar, Department de AeronÃ¡utica, Universidad Nacional de CÃ³rdoba, Av. Velez Sarfield 1601, CÃ³rdoba (5000), Argentina, Centro de Investigaciones Aplicadas, Instituto Universitario AeronÃ¡utico, Ruta 20, km. 5.5, CÃ³rdoba (5022), Argentina; HÃ©ctor H. Brito, Centro de Investigaciones Aplicadas, Instituto Universitario AeronÃ¡utico, Ruta 20, km. 5.5, CÃ³rdoba (5022), Argentina

2003-071: COMPUTATIONAL MODEL OF AN SPT-100 THRUSTER; Justin W. Koo and Iain D. Boyd, Nonequilibrium Gas and Plasmadynamics Group, Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109

2003-072: CHARACTERISTICS OF ENERGETIC IONS EMITTED FROM HOLLOW CATHODES; Casey C. Farnell, John D. Williams, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-073: NUMERICAL SIMULATION OF ION THRUSTER OPTICS; Cody C. Farnell, John D. Williams, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-075: DISCHARGE CHARACTERISITICS OF A LASER-ASSISTED PLASMA THRUSTER; Hideyuki Horisawa, Masatoshi Kawakami, Wun-Wei Lin, and Akira Igari, Department of Aeronautics and Astronautics, Tokai University, 1117 Kitakaname, Hiratsuka, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, 113-8856, Japan

2003-077: HOT FLOW PRESSURE MAP OF A VACUUM FACILITY AS A FUNCTION OF FLOW RATE TO STUDY FACILITY EFFECTS; Mitchell L. R. Walker and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, College of Engineering, Ann Arbor, MI 48109, USA

2003-078: DISCHARGE CHARACTERISTICS OF A VERY LOW-POWER ARCJET; Hideyuki Horisawa and Hotaka Ashiya, Department of Aeronautics and Astronautics, Tokai University, 1117 Kitakaname, Hiratsuka, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, 113-8856, Japan

2003-079: HIGH ACCURACY MULTI-COLOR PYROMETRY FOR HIGH TEMPERATURE SURFACES; L. D. Cassady and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey, 08544

2003-082: CHARACTERIZATION OF A HIGH SPECIFIC IMPULSE HALL THRUSTER USING ELECTROSTATIC PROBES; Noah Z. Warner and Manuel Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, 77 Massachusetts Ave., Cambridge, MA 02139, USA; James J. Szabo, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760, USA

2003-083: ION THRUSTER THRUST VECTORING BY GRID TRANSLATION; Yasushi Okawa, Japan Society for the Promotion of Science, YukÃo Hayakawa, Katsuhiro Miyazaki, and Shoji Kitamura, National Aerospace Laboratory of Japan

2003-084: ULTRA-LIGHT CONCENTRATORS FOR SOLAR THERMAL PROPULSION; Hironori Sahara, Japan Society for the Promotion of Science (JSPS), 7-44-1, Jindaiji-Higashi-Machi, Chofu, Tokyo 182-8522, Japan; Shinsuke Ezaki, Yasuhiro Matsui, and Yoshihiro Nakamura, Hosei University; Morio Shimizu, National Aerospace Laboratory of Japan (NAL)

2003-085: SOLAR THERMAL PROPULSION FOR MICROSATELLITES END-OF-LIFE DE-ORBITING; Hironori Sahara, Japan Society for the Promotion of Science (JSPS), NAL, 7-44-1, Jindaiji-Higashi-Machi, Chofu, Tokyo, 182-8522, Japan; Morio Shimizu, National Aerospace Laboratory of Japan (NAL); 7-44-1, Jindaiji-higashimachi, Chofu, Tokyo, 182-8584, Japan; Keitaro Osa, Kai Watanabe, and Yoshihiro Nakamura, Hosei University, 3-7-2, Kajino-Cho, Koganei, Tokyo, 184-8584, Japan

2003-086: CONDITION OF STABLE OPERATION IN A HALL THRUSTER; Naoji Yamamoto, Kimiya Komurasaki, and Yoshihiro Arakawa, University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo, 113-8656, Japan

2003-087: LIQUID PROPELLANT PULSED PLASMA THRUSTER; H. Koizumi, A. Kakami, Y. Furuta, K. Komurasaki, and Y . Arakawa, The University of Tokyo, Department of Aeronautics and Astronautics, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2003-088: EXPERIMENTAL INVESTIGATION OF THE THRUST PERFORMANCE OF ATTILA; Stefan Laure, Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany; JÃ¶rg Heiermann, Monika Auweter-Kurtz and Helmut Kurtz, Institut fÃ¼r Raumfahrtsysteme (IRS), UniversitÃ¤t Stuttgart, Germany

2003-089: STUDY OF A PLASMA SAIL FOR FUTURE DEEP SPACE MISSIONS; I. Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; H. Yamakawa, K. Fujita, H. Ogawa, S. Nonaka, S. Sawai, and H. Kuninaka, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; H. Otsu, Faculty of Engineering, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan

2003-092: FEASIBILITY STUDY OF A LOW-POWER APPLIED-FIELD MPD ARCJET; Tetsuaki Nakano and Atsushi Ishiyama, Waseda University, 3-4-1 Ohkubo, Shinjuku, Tokyo, Japan; Yukio Shimizu and Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-093: SINGLE IMPULSE MEASUREMENT OF A COAXIAL PULSED PLASMA THRUSTER; Masahiko Kameoka and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., 6-6, Asahigaoka, Hino, Tokyo 191-0065, Japan; Yukio Shimizu and Kyoichiro Toki, Institute of Space and Astronautical Science, Japan, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-095: AN ANALYTICAL STUDY OF THE THRUST IN MPD THRUSTERS; Luigi Petrucci, Space Propulsion Laboratory, University of Rome “La Sapienza”, Via Eudossiana 18, 00184 Rome, Italy

2003-096: ARTEMIS ORBIT RAISING IN-FLIGHT EXPERIENCE WITH ION PROPULSION; Rainer Killinger and Ralk Kukies, Astrium GmbH, 74215 Lampoldshausen, Germany; Michael Surauer, Astrium GmbH, 81663 MÃ¼nchen, Germany; Howard Gray and Ray Dunster, Astrium Ltd., Portsmouth, United Kingdom; Giorgio Saccoccia, European Space Agency – ESTEC, Noordwijk, The Netherlands; Angelo Tomasetto, Alenia Spazio, Roma, Italy

2003-097: EVALUATIOIN OF NEW CARBON-CARBON COMPOSITE MATERIAL FOR A 20 CM ION ENGINE; Y. Shimizu, H. Kuninaka, K. Nishiyama, and K. Toki, The Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-098: FLIGHT READINESS OF THE MICROWAVE ION ENGINE SYSTEM FOR MUSES-C MISSION; Kyoichiro Toki, Hitoshi Kuninaka, Kazutaka Nishiyama, and Yukio Shimizu, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2003-100: ELECTRON INSTABILITIES IN HALL THRUSTERS: MODELING AND APPLICATION TO ELECTRIC FIELD DIAGNOSTICS; A. Kapulkin, A. Kogan, D. Alkalay, and M. Guelman, Asher Space Research Institute, Technion, I.I.T., Haifa, 32000, Israel; J. Ashkenazy and G. Appelbaum, Propulsion Physics Laboratory, Soreq, NRC, Yavne 81800, Israel

2003-103: STUDY OF THE HALL THRUSTER DISCHARGE WITH AN INTERMEDIATE ELECTRODE; B. Navazo and E. Ahedo, Univ. PolitÃ©cnica de Madrid, Spain

2003-104: SCALING DOWN HALL THRUSTERS; E. Ahedo and J. M. Gallardo, E.T.S.I. AeronÃ¡uticos, Universidad PolitÃ©cnica de Madrid, Spain

2003-107: PLASMA PARAMETER DISTRIBUTION DETERMINATION IN SPT-70 PLUME; Vladimir Kim, Vyacheslav Kozlov, Garry Popov, and Alexander Skyrlnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), 5, Leningradskoye shosse, p.b. 43, Moscow, 125080, Russia

2003-110: NUMERICAL ANALYSIS OF NEXT ION THRUSTER OPTICS; Jerold W. Emhoff, Graduate Student Research Assistant; Iain D. Boyd, Professor; Steven P. Shepard, Undergraduate Student, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109

2003-112: INVESTIGATION OF A PPT UTILIZING WATER AS A COMPONENT PROPELLANT; Carsten A. Scharlemann and Thomas M. York, The Ohio State University, Aero/Astro Laboratory, 2300 West Case, Columbus, OH 43235; Peter J. Turchi, Los Alamos National Laboratory, Mail Stop D410. Los Alamos, NM 87545

2003-114: OPTIONS AND RISK FOR QUALIFICATION OF ELECTRIC PROPULSION SYSTEMS; Michelle Bailey, NASA/MSFC, Mail Code ED20, Marshall Space Flight Center, AL 35812, USA; Charles Daniel, 3418 Wildwood Drive, Huntsville, AL 35801, USA

2003-115: DEVELOPMENT AND PERFORMANCE OF THE ADVANCED RADIO FREQUENCY ION THRUSTER RIT-XT; Hans J. Leiter, Rainer Killinger, Helmut Bassner, Johann MÃ¼ller, Ralf Kukies, and Thomas FrÃ¶hlich, Astrium GmbH, Space Infrastructure, Post Box 11 19, D-74215 MÃ¶ckmÃ¼hl, Germany

2003-116: PLASMA MODELING OF A HOLLOW ANODE FOR AN ANODE LAYER TYPE HALL THRUSTER; Ken Kumakura and Kimiya Komurasaki, Department of Advanced Energy, The University of Toyko; Shinsuke Yasui and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, The University of Tokyo, Hongo 7-3-1, Bunkyo, Tokyo 113-8656, Japan

2003-118: PROPELLANTS BEYOND XENON FOR RADIO FREQUENCY ION THRUSTER OPERATION; Hans J. Leiter, Astrium GmbH, IP 47, 81663 Munich, Germany

2003-120: PROBE MEASUREMENTS IN DISCHARGE CHAMBER OF LOW-POWER ION THRUSTER; M. V. Zikeyev and A. A. Shagayda, Keldysh Research Center, 125438, Russia, Moscow, Onezhskaya, 8/10

2003-121: OPERATION PRECULIARITIES OF HALL THRUSTER WITH POWER 1.5-2.0 KW AT HIGH DISCHARGE VOLTAGES; M. B. Belikov, N. V. Blinov, O. A. Gorshkov, R. N. Rizakhanov, and A. A. Shagayda, Keldysh Research Center, 125438, Moscow, Onezhskaya 8

2003-122: TWO KILOWATT BIPROPELLANT ARCJET DEVELOPMENTS; Kurt Hohman, Thomas Brogan, and Vladimir Hruby, Busek Company, Inc, 11 Tech Circle, Natick, MA 01760, USA; Kurt Annen and Robert Brown, Aerodyne Research Inc., 45 Manning Road, Billerica, MA 01821

2003-123: EXPENDING PLASMA JET FROM THE NOZZLE OF THE RF-PLASMA THRUSTER; Leonid A. Bazyma, National Aerospace University, “Kharkov Aviation Institute” 17 Chkalov Street, Kharkov, 61070, Ukraine; Vasyl M. Rashkovan, Instituto Politecnico Nacional de Mexico, ESIME-Culhuacan, Av. Santa Ana 1000

2003-124: INDUCTIVE PULSED THRUSTER WITH SUPERCONDUCTING ACCELRATING ELEMENTS; Vasyl Rashkovan, Iryna Ponomaryova and Omar J. Ramirez, Instituto PolitÃ©cnico Nacional de MÃ©xico, ESIME-CULHUACAN, Av. Santa Ana, 1000, C.P.04430, MÃ©xico; Andrey Dashkov, National Aerospace University of Ukraine (KhAI), 17 Chkalov Street, Kharkov, 61070, Ukraine

2003-125: DEVELOPING SPACE STATION-BASED DEMONSTRATION FOR THE VASIMR PLASMA ROCKET; Andrew Petro, Franklin Change DÃaz, Jared P. Squire, and Andrew Ilin, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, USA

2003-126: FEASIBILITY STUDY OF AN ACTIVE PLASMA EXPERIMENTAL PLATFORM IN JAPANESE EXPERIMENTAL MODULE ONBOARD THE ISS; Ikkoh Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; Hideyuki Usui and Hayato Tashima, Radio Science Center for Space and Atmosphere, Kyoto University, Uji, Kyoto, 611-0011, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Masaki Okada, National Institute of Polar Research, 1-9-10 Kaga, Itabashi, Tokyo, 173-8512, Japan; and Yoshinori Nakayama, National Defense Academy, Yokoshuka, Kanagawa, 239-8686, Japan

2003-128: EXPERIMENTAL PERFORMANCE LIMITS ON HIGH SPECIFIC IMPULSE ION OPTICS; John D. Williams, D. Mark Laufer, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-129: ELECTROMAGNETIC EMISSIONS TO 60 GHZ FROM A BPT-4000 EDM HALL THRUSTER; Edward j. Beiting and James E. Pollard, The Aerospace Corporation, Los Angeles, California; Vadim Khayms and Lance Werthman, Lockheed Martin Space Systems Company, Sunnyvale, Caifornia

2003-130: XENON SPUTTER YIELD MEASUREMENTS FOR ION THRUSTER MATERIALS; John D. Williams, Michael M. Gardner, Mark L. Johnson, and Paul J. Wilbur, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2003-131: ALCATEL SPACE PLASMA PROPULSION SUBSYSTEM QUALIFICATION STATUS; Pascal Garnero and Olivier Dulau, ALCATEL SPACE, 100, Bd. Du Midi, BP 99, 06156 CANNES LA BOCCA Cedex, France

2003-132: FLIGHT TESTING OF VOLUME-IONIZATION ION THRUSTERS ON METEOR SATELLITE; Vladimir P. Khodnenko, NPP Russian Scientific and Research Institute of Electromechanics, Moscow 101000, P.O. Box 496, Russia

2003-133: EROISION ACTION OF THE SPT JET ONTON SOLAR BATTERIES OF METEOR-PRIDODA SPACECRAFT; Vladimir P. Khodnenko, NPP Russian Scientific and Research Institute of Electromechanics, Moscow 101000, P.O. Box 496, Moscow, Russia

2003-134: HYBRID-PIC SIMULATION OF HALL THRUSTERPLUME ON AN UNSTRUCTURED GRID WITH DSMC COLLISIOINS; Murat Celik, Mark Santi, Manuel Martinez-Sanchez, and Jamie Peraire, Massachusetts Institute of Technology, United States of America

2003-135: PULSED INDUCTIVE THRUSTER (PIT); MODELING AND VALIDATION USING THE MACH2 CODE; Pavlos G. Mikellides, Arizona State University, Tempe, AZ 85287-6106

2003-136: 3-D COMPUTATION OF SURFACE SPUTTERING AND REDEPOSITION DUE TO HALL THRUSTER PLUMES; J. M. Fife, M. R. Gibbons, and W. A. Hargus, U.S. Air Force Research laboratory, Edwards AFB, CA; D. B. VanGilder and D. E. Kirley, ERC, Inc., Edwards AFB, CA; L. K. Johnson, Jet Propulsion Laboratory, Pasadena, CA

2003-137: RADIOISOTOPE ELECTRIC PROPULSION FOR NEW FRONTIERS CLASS MISSIONS; Steven Oleson, Scott Benson, Michael Patterson, Jeffrey Schreiber, National Aeronautics and Space Administration, Glenn Research Center, MS 500-103, 21000 Brookpark Rd, Cleveland, Ohio 4413; Douglas Fiehler, QSS Group, Inc., Cleveland, Ohio

2003-138: DEVELOPMENT OF A MICRO-FABRICATED COLLOID THRUSTER ARRAY; Luis Fernando VelÃ¡squez GarcÃa, PhD Candidate, Aeronautics and Astronautics, MIT; Manuel MartÃnez-SÃ¡nchez, Professor, Aeronautics and Astronautics, MIT; Akintunde I. Akinwande, Professor, Electrical Engineering and Computer Science, MIT

2003-139: PRELIMINARY RESULTS OF PLASMA FLOW MEASUREMENTS IN A 2 KW SEGMENTED HALL THRUSTER; Y. Raitses, D. Staack, A. Dunaevsky, L. Dorf, and N. J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ 08543

2003-140: INSTRUMENT DESIGN AND ANALYSIS FOR DIAGNOSIS OF A HALL THRUSTER PLUME FOR THE ETEEV SHUTTLE EXPERIMENT; Yassir Azziz and Manaul Martinez-Sanchez, Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 77 Massachusetts Avenue, Cambridge, MA 02139

2003-142: THE INFLUENCE OF CURRENT DENSITY AND MAGNETIC FIELD TOPOGRAPHY IN OPTIMIZING THE PERFORMANCE, DIVERGAENCE, AND PLASMA OSCILLATIONS OF HIGH SPECIFIC IMPULSE HALL THRUSTERS; Richard R. Hofer, QSS Group, Inc., Cleveland, OH 44135, USA; Robert S. Jankovsky, NASA Glenn Research Center, Cleveland, OH 44135, USA

2003-146: HIGH POWER MPD THRUSTER DEVELOPMENT AT THE NASA GLENN RESEARCH CENTER; Michael R. LaPointe, Ohio Aerospace Institute, 22800 Cedar Point Road, Cleveland, OH 44142

2003-150: HELICON WAVE PHYSICS IMPACTS ON ELECTRODELESS THRUSTER DESIGN; James Gilland, OAI, 22800 Cedar Point Rd., Brookpark, OH 44142

2003-154: THRUST MEASUREMENTS OF A MESO-SCALE HOLLOW CATHODE DISCHARGE; Andrew J. Jamison, Joseph Landon, Joshua A. Cripps, University of Southern California, Department of Aerospace and Mechanical Engineering, Los Angeles, CA 90089-1191; Andrew D. Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards AFB, CA 93524; Joseph Wang, Virginia Polytechnic Institute & State University, Dept. Aerospace and Ocean Engineering, Blacksburg, VA 24061-0203

2003-156: ENHANCED IONIZATION IN THE CYLINDRICAL HALL THRUSTER; A. Smirnov, Y. Raitses, and N. J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, New Jersey 08543

2003-157: DIAGNOSTIC SETUP FOR CHARACTERIZATION OF NEAR-ANODE PROCESSES IN HALL THRUSTERS; L. Dorf and Y. Raitses, Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ, 08543

2003-158: NASA’S ELECTRIC PROPULSION PROGRAM; John W. Dunning Jr., Scott Benson, and Steven Oleson, National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field, Cleveland, Ohio, USA 44135

2003-159: NUMERICAL FEASIBILITY DESIGN CODE OF ION THRUSTER; Yoshinori Nakayama, Department of Aerospace Engineering, National Defense Academy, 1-10-20, Hashirimizu, Yokosuka, 239-8686, Japan

2003-160: STUDY ON PLUME CHARACTERISTICS OF PULSED PLASMA THRUSTER; Kentaro Kawahara, Naoki Kumagai, Kensuke Sato, Kohji Tamura, Takahiro Koide, Kenji Harima, Tadanori Fukushima, and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Department of Aerospace Engineering, Asahigaoka 6-6, Hino, Tokyo, 191-0065, Japan

2003-161: THREE-DIMENSIONAL IN-FEEP PLASMADIAGNOSTICS, M. Tajmar, K. Marhold, and S. Kropatschek, Space Propulsion, ARC Seibersdorf Reseach A-2444 Seibersdorf, Austria

2003-162: KINETIC MODEL OF THE ELECTRON AND ION TRANSPORT IN HALL THRUSTERS; I. Levchenko, National Aerospace University, Kharkov, Ukraine; M. Keidar, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109

2003-163: ENGINE DEVELOPMENT STATUS FOR NEXT: NASA’S EVOLUTIONARY XENON THRUSTER; Michael J. Patterson, John E. Foster, Thomas Haag, Vincent K. Rawlin, and George Soulas, NASA Glenn Research Center, 21000 Brookpark Rd. Cleveland, Ohio 44135; Robert F. Roman, QSS Group, Inc.

2003-164: YIELD OF SECONDARY ELECTRON EMISSION FROM CERAMIC MATERIALS OF HALL THRUSTER WITH SEGMENTED ELCTRODES; A. Dunaevsky, Y. Raitses, and N. J. Fisch, Plasma Physics Laboratory, Princeton University, P.O. Box 451, Princeton, NJ 09543, US

2003-165: RESEARCH AND DEVELOPMENT OF 150-MN XENON ION THRUSTER; Shoji Kitamura, Yukio Hayakawa, Katsuhiro Miyazaki, and Hideki Yoshida, National Aerospace Laboratory of Japan, Chofu, Tokyo 182-8522, Japan; Kenichi Kajiwara, National Space Development Agency of Japan, Tsukuba, Ibaraki 305-8505, Japan; Kouseki Akai, NEC Toshiba Space Systems, Yokohoma, Kanagawa 224-8555, Japan

2003-166: THE AZIMUTHAL BEAM-PLASMA INSTABILITIES IN STATIONARY PLASMA THRUSTERS; K. Makowski and S. Barral, Institute of Fundamental Technological Research – IPPT-PAN, Swietokrzyska 11/21, 00-049 Warsaw, Poland; Z. Peradzynski, Institute of Fundamental Technological Research – IPPT-PAN, Swietokrzyska 11/21, 00-049 Warsaw, Poland, Institute of Applied Mathematics & Mechanics, Warsaw University, Banacha 2, 02-697 Warsaw, Poland; M. Dudeck, Laboratoire d’ AÃ©rothermique du CNRS, 1C av. de la Recherches Scientifiques, 45000 OrlÃ©ans, France

2003-167: SOLUTIONS WITH SHOCKS FOR FLUID MODEL OF STATIONARY PLASMA THRUSTER; Zbigniew Peradzynski, Serge Barral, and Karol Makowski, Institute of Fundamental Technological Research – PAS, Swietokrzyska 21, 00-049 Warsaw, Poland, Institute of Applied Mathematics and Mechanics, Warsaw University, Banacha 2, 02-097 Warsaw, Poland; Michael Dudeck, CNRS Laboratoire d’ AÃ©rothermique, 45071 OrlÃ©ans, France

2003-168: PRELIMINARY INVESTIGATION OF HELICON PLASMA SOURCE FOR ELECTRIC PROPULSION APPLICATIONS; Kyoichiro Toki, Institute of Space and Astronautical Science, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Shunjiro Shinohara, Interdisciplinary Graduate School of Engineering Sciences, Kyushu University, 6-1 Kasuga-Koen, Kausga, Fukuoka 816-8580, japan; Takao Tanikawa, Research Institute of Science and Technology, Tokai University, 2-28-4 Tomigaya, Shibuya-ku, Tokyo 151-0064, Japan; Ikkho Funaki, Institute of Engineering Mechanics and Systems, University of Tsukuba, 1-1-1, Ten-nodai, Tsukuba, Ibraki 305-8577, Japan; Konstantin P. Shamrai, Scientific Center Institute for Nuclear Research, National Academy of Sciences, 47 Prospeckt Nauki, Kiev 28, 03680 MSP, Ukraine

2003-169: AN OVERVIEW OF THE CNES ELECTRIC PROPULSION PROGRAM; Anne Cadiou, Franck Darnon, and Laurent Jolivet, CNES, 18 Avenue Edouard Belin, 31401 Toulouse Cedex 4

2003-170: ELECTRIC PROPULSION ON @BUS PLATFORM; Michel Lyszyk, @Bus Alcatel-Astrium JPT, Alcatel Space 100 Boulevard du Midi 06156, Cannes la Bocca Cedex, France; Vincent Jacod, @Bus Alcatel-Astrium JPT, Astrium Space 31 Rue des Cosmonautes 31402 Toulouse Cedex 4, France

2003-171: A COMPARISON OF SPUTTERING MODELS FOR PLASMA-SURFACE INTERACTIONS; D. B. VanGilder and D. E. Kirtley, ERC, Inc., Edwards AFB, CA; J. M. Fife and M. R. Gibbons, U. S. Air Force Research Laboratory, Edwards AFB, CA

2003-172: IMPROVED XENON LOADING EQUIPMENT WITH LOADING CAPACITY UP TO 1200 KG FOR ALPHABUS; Patrick Bravais, AIR LIQUIDE DTA; Roland Salome and CÃ©cile Gelas, CNES Toulouse

2003-174: EFFECT OF PLASMA-WALL RECOMBINATION AND TURBULENT RESISTIVITY ON THE CONDUCTIVITY IN HALL THRUSTERS; A. A. Ivanov, RRC Kurhatov Institute, Kurchatov Square 1, 123182 Moscow, Russia; A. A. Ivanov Jr. and M. Bacal, Laboratoire de Physique et Technologie des Plasmas, Ecole Polytechnique, UMR 7648 du CNRS, 91128 Palaiseau, France

2003-176: STUDY OF EXTRACTION GRID EROSION IN A LONG-TIME ION THRUSTER OPERATIONAL TEST; M. Tartz, E. Harmann, and H. Neumann, Institut fÃ¼r OberflÃ¤chenmodifizierung e. V., Permoserstr. 15, D-04318 Leipzig, Germany; R. Deltschew, Solarion GmbH Leipzig

2003-180: A COLLOID ENGINE ACCELERATOR CONCEPT UPDATE; D. Kirtley, ERC, Inc., Edwards AFB, CA; J. M. Fife, U. S. Air Force Research Laboratory, Edwards AFB, CA

2003-181: MW-CLASS INDUCTIVE MPD THRUSTER USING NON-UNIFORM GAS-PLASMA FLOW; V. S. Slavin and A. A. Gavrilov, Krasnoyarsk State Technical University, 26 Kirensky Str, Krasnoyarsk, 660074, Russia

2003-183: PARAMETRIC STUDY OF HALL THRUSTER OPERATION BASED ON A 2D HYBRID MODEL: INFLUENCE OF THE MAGNETIC FIELD ON THE THRUSTER PERFORMANCE AND LIFETIME; L. Garrigues, C. Boniface, J. Bareilles, G. J. M. Hagelaar, and J. P. Boeuf, Centre de Physique des Plasmas et Applications, UniversitÃ© Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse cedex, France

2003-184: CRITICAL ASSESSMENT OF A 2D MODEL OF HALL THRUSTERS-COMPARISONS WITH EXPERIMENTS; J. Bareilles, G. J. M. Hagelaar, L. Garrigues, C. Boniface, and J. P. Boeuf, Centre de Physique des Plasmas et Applications, UniversitÃ© Paul Sabatier 118 Route de Narbonne, 31062 Toulouse cedex, France; N. Gascon, Laboratoire d’ AÃ©rothermique, 1C Avenue de la Recherche Scientifique, 45071 OrlÃ©ans cedex 2, France

2003-185: MODELING OF ION CYCLOTRON WAVES ABSORPTION IN VASIMR; Andrew V. Ilin, MuÃ±iz Engineering, Inc., Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, 77059, USA; Franklin R. Chang DÃaz, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, USA; Boris N. Breizman, University of Texas at Austin, Austin, Texas, USA; Mark D. Carter, Oak Ridge National Laboratory, Oak Ridge, Tennessee, USA

2003-186: ACCELERATOR SYSTEMS FOR LONG-LIFE ION THRUSTER OPERATION AT SPECIFIC IMPULSES GREATER THAN 4000 S; John Brophy, Ira Katz, and James Polk, Jet Propulsion Laboratory, California Institute of Technology, MS 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-187: MODELING A MESO-SCALE HOLLOW CATHODE THRUSTER; Joseph J. Wang, Virginia Polytechnic Institute & State University, Dept. Aerospace and Ocean Engineering, Blacksburg, VA 24061-0203; Andrew D. Ketsdever, Air Force Research Laboratory, Propulsion Directorate, Edwards, AFB, CA 93524; and Andrew J. Jamison, University of Southern California, Department of Aerospace and Mechanical Engineering, Los Angeles, CA 90089-1191

2003-188: CHARGED PARTICLES TRANSPORT IN THE HALL EFFECT THRUSTER; Oleg Batishchev and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, MIT NW 16-232, 167 Albany St. Cambridge, MA 02139, USA

2003-191: VASIMR THRUSTER OPERATION WITH HYDROGEN AND HELIUM GAS PROPELLANTS; Oleg Batishchev and Kim Molvig, Massachusetts Institute of Technology, MIT NW 16-232, 167 Albany St. Cambridge, MA 02139, USA

2003-192: THE DEVELOPMENT OF ION PROPULSION IN THE UK: A HISTORICAL PERSPECTIVE; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK

2003-193: THE POTENTIAL APPLICATION OF SMALL ELECTRICALLY-PROPELLED SPACECRAFT TO LOW-COST INTERPLANETARY MISSIONA; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK; Stephen D. Clark, Space Department, Y72 Building, QinetiQ, Farnborough, Hants GU14 OLX, UK

2003-198: STUDY OF ENERGY CONVERSION PROCESS IN CW LASER PROPULSION; Satoshi Hosoda, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2003-202: RESEARCH AND DEVELOPMENT STATUS OF LOW POWER PULSED PLASMA THRUSTER SYSTEM FOR Âµ-LAB SAT II; Naoki Kumagai, Kensuke Sato, Kohji Tamura, Kentaro Kawahara, Takahiro Koide, and Haruki Takegahara, Tokyo Metropolitan Institute of Technology, Dept. of Aerospace Eng., Asahigaoka 6-6, Hino, Tokyo 191-0065, Japan; Mitsuteru Sugiki, Astro Research Corporation, Kugenuma Tachibana, 1-1-4, Fujisawa, Kanagawa, 251-0024, Japan; Takashi Wakizono, HI-SERVE Corporation, Totohara 780-7, Akiruno, Tokyo, 190-0152, Japan; Hidekazu Hashimoto, National Space Development Agency of Japan, Advanced Mission Research Center, Micro Space Systems Laboratory, Sengen, 2-1-1, Tsukuba, Ibaraki 305-0047, Japan

2003-204: STUDY OF DISCHARGE CHANNEL EROSION IN MULTI MODE ANODE LAYER THRUSTER; A. E. Solodukhin and A. V. Semenkin, Central Research Institute of Machine Building (TSNIIMASH(, Pionerskaya 4, Korolev, Moscow region, Russia 141070

2003-205: SMART-1 PRIMARY ELECTRIC PROPULSION SUB-SYSTEM THE FLIGHT MODEL; Christophe R. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux, Site de Villaroche Nord, Direction Propulsion et Equipements Satellites, AÃ©rodrome de Melun Villaroche; Denis Estublier, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2003-206: COMPARISON OF MATHEMATICAL MODEL OF A PLASMA PLUME WITH OUTCOMES OF SPACE EXPERIMENTS; A. G. Korsun, F. F. Gabdullin, E. M. Tverdokhlebova, and V. I. Garkusha, Central Research Institute of Machine Building (TSNIIMASH), 141070 Korolev, Moscow region, Russia; V. P. Khodnenko, NPP All-Russian Research Institute of Electromechanics, 101000, P. O. Box 496, Moscow, Russia

2003-207: EXPERIMENTAL AND NUMERICAL COMPARISON OF HIGH POWER STEADY STATE MPD-THRUSTERS WITH RADIATION-AND-WATER-COOLED ANODES; Michael W. Winter, JÃ¶rg Heiermann, and Monika Auweter-Kurtz; Institut fÃ¼r Raumfahrtsysteme (IRS), UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2003-210: A SUMMARY THE QINETIQ HOLLOW CATHODE PROGRAMME IN SUPPORT OF THE ARTEMIS MISSION; N. C. Wallace and H. B. Simpson, Electric Propulsion, Space Department, QinetiQ, Farnborough, Hampshire, United Kingdom, GU14 0LX

2003-211: INVESTIGATION OF THE SPT OPERATION UNDER HIGH DISCHARGE VOLTAGES; Andre Bouchoule, Alexey Lazurenko and Vanessa Vial, GREMI Laboratory, Orleans University, 45067, OrlÃ©ans cedex 2, France; Vladimir Kim, Vyacheslav Kozlov, and Alexander Skrylnikov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute, 5 Leningradskoye shosse, p/b 43, Moscow, 125080, Russia

2003-212: FIRST TEST RESULTS OF THE HEMP THRUSTER CONCEPT; GÃ¼nter Kornfeld, Norbert Koch, and GrÃ©gory Coustou, Thales Electron Devices GmbH, SÃ¶flinger StraÃŸe 100, D-89077 Ulm, Germany

2003-213: A DESCRIPTION OF THE NEW 3.8M DIAMETER HIGH POWER ELECTRIC PROPULSION TEST FACILITY AT QINETIQ FARNBOROUGH, UK, H. B. Simpson, N. C. Wallace, S. D. Clark, and D. H. Mundy, QinetiQ, Farnborough, Hampshire, GU14 0LX, The United Kingdom

2003-214: A SUMMARY OF THE QINETIQ HOLLOW CATHODE DEVELOPMENT PROGRAMME IN SUPPORT OF EUROPEAN HIGH POWER HALL EFFECT AND GRIDDED THRUSTERS; H. B. Simpson, N. C. Wallace, D. G. Fearn, and M. K. Kelly, QinetiQ, Farnborough, Hampshire, GU14 0LX, The United Kingdom

2003-216: A STUDY INTO THE TECHNIQUES FOR MINIATURISED ELECTRIC PROPULSION SYSTEMS, AND MISSION CATEGORIES, FOR SMALL SPACECRAFT; Stephen D. Clark, Space Department, Y72 Building, QinetiQ, Farnborough, Hants, GU14 0LX, UK; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, UK; Frederic Marchandise, Rocket Engine Division, Satellites Propulsion & Equipment, Aerodrome de Melun, Villaroche, 77550 Moissy-Cramayel, France

2003-218: CHARACTERIZATION OF MICROINST ABILITIES IN HALL THRUSTER PLASMA: EXPERIMENTAL AND PIC CODE SIMULATION RESULTS, PHYSICAL INTERPRETATION AND IMPACT ON TRANSVERSE ELECTRON TRANSPORT; A. Lazurenko, V. Vial, and A. Bouchoule, GREMI, UniversitÃ© d’OrlÃ©ans, BP 6744, 45067 OrlÃ©ans, France; M. Prioul, SNECMA, Villaroche Nord, B.P. nÂ°93, F-77552 Moissy-Cramayel CÃ©dex; J. C. Adam, A. Heron, and G. Laval, CPHT, Ecole Polytechnique, route de Saclay, 91128 Palaiseau, France

2003-219: OPTICAL PROBE MEASUREMENTS ON THE INTERNAL PLASMA OF A T6 TYPE HOLLOW CATHODE; S. J. Pottinger and S. B. Gabriel, Astronautics Research Group, University of Southampton SO17 1BJ, United Kingdom

2003-220: PHYSICAL INSIGHTS ON SPT THRUSTERS THROUGH ULTA-FAST, EXTERNALLY DRIVEN CURRENT INTERRUPTIONS; Vanessa Vial, Alexey Lazurenko, and AndrÃ© Bouchoule, GREMI Laboratory, OrlÃ©ans university, 45067 OrlÃ©ans Cedex 2; Mathieu Prioul, SNECMA, Direction Propulsion et Equipements Satellites, 77-550, Moissy Cramayel

2003-221: XENON GAS INJECTION IN SPT THRUSTERS; Vanessa Vial, Alexey Lazurenko, Claude Laure, and AndrÃ© Bouchoule, GREMI, OrlÃ©ans University, 45067 OrlÃ©ans Cedex 2, France; Daniel Pagnon, LPGP, Orsay University, 91405 Orsay Cedex, France

2003-222: AUTOMATIC INTERPLANETARY MISSIONS. OPTIMISATION OF A MISSION WITH LOW THRUST STRATEGY; Nicolas Pillet, Sophie Geffroy, and RÃ©gis Bertrand, CNES Toulouse, Space Technic’s Directory, Denis Moura, CNES Toulouse, Orbital System Directory; Christophe Talbot, CNES Evry, Launcher Directory; Mikhail Stepanov, ENSMA, Ecole Nationale SupÃ©rieure de MÃ©chanique et d’AÃ©rotechnique

2003-225: PROPULSION INSTRUMENT ELECTRONICS AND SENSOR PACKAGE; Paul B. Adkison, Sverdrup Inc., Edwards AFB, CA 93524; Michael J. Dulligan, ERC, Inc., Edwards AFB, CA 93524; Greg Spanjers and Daron Bromaghim, USAF, Edwards AFB, CA 93524; Rick Harrison and Dale McGehee, Naval Post Graduate School, Monterey, CA 93940; Dave White, W.E. Research, Rosamond, CA 93560; David Conroy and Lee Johnson, Jet Propulsion Laboratory, Pasadena, CA 91109

2003-226: MICRO NEWTON COLLOID THRUSTER SYSTEM DEVELOPMENT FOR ST7; Manuel Gamero-CastaÃ±o, Vlad Hruby, Douglas Spence, Charles Gasdaska, and Bill Connolly, Busek Co. Inc., 11 Tech Circle, Natick, MA 01760-1023

2003-227: LOW POWER HALL THRUSTER DEVELOPMENT FOR TECHSAT 21; B. Pote, V. Hruby, M. Gamero-CastaÃ±o, G. Kolencik, L. Byrne, R. Tedrake, and W. Connolly, Buseck Co. Inc., 11 Tech Circle, Natick, MA 01760-1023; D. Bromaghim and G. Spanjers, Air Force Research Laboratory, Propulsion Directorate, 1 Ara Road, Edwards AFB, CA 93524-7013

2003-228: DESIGN AND PRELIMINARY CHARACTERIZATION OF A 5 KW HALL THRUSTER PROTOTYPE; L. Biagioni, M. Saverdi, M. Berti, and M. Andrenucci, Centrospazio-CPR, Pisa (Italy); U. Cesari, Alta S.p.A., Via A. della Gherardesca 5, I-56121, Pisa (Italy)

2003-229: THE NEW EP TEST FACILITIES AT CENTROSPAZIO AND ALTA; M. Andrenucci, M. Berti, Centrospazio-CPR, Pisa (Italy); L. Biagioni, U. Cesari, R. Falorni, L. Milaneschi, and M. Saverdi, Alta S.p.a., 56121 Ospedaletto, Pisa (Italy)

2003-230: BASIC ISSUES IN ELECTRIC PROPULSION TESTING AND THE NEED FOR INTERNATIONAL STANDARDS; L. Biagioni, Alta S.p.A. Pisa (Italy); V. Kim, Moscow Aviation Institute, RIAME, Moscow (Russia); D. Nicolini, European Space Agency, ESTEC, TOS-MPE, Noordwijk (The Netherlands); A. V. Semenkin, Central Institute of Machine Building (TsNIIMash), Korolev (Russia; N. C. Wallace, Qinetiq Ltd., Space Dept., Farnborough (United Kingdom)

2003-231: ONE AND TWO DIMENSIONAL MODELING OF THE BHT-1000; James J. Szabo, Peter S. Rostler, Seth A. McElhinney, and Noah Z. Warner; Busek Co. Inc., 11 Tech Circle, Natick, MA 01760, The United States of America

2003-234: EXPERIMENTAL PERFORMANCE OF 1 MN-CLASS FEEP THRUSTERS; Salvo Marcuccio, Marco Saviozzi, Leonardo Priami, and Mariano Andrenucci, Alta S.r.l., Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-236: ELECTRIC PROPULSION IN ITALY: STATUS AND PERSPECTIVES; Mariano Andrenucci, Alta S.p.A. / Centrospazio, Via A. Gherardesca 5, 56121 Ospedaletto, Pisa, Italy; Giovanni Matticari, LABEN – Proel Tecnologie Division, Viale Machiavelli 31, 50125 Firenze, Italy

2003-237: PERFORMANCE CHARACTERIZATION OF THE VAPORIZING LIQUID MICRO THRUSTER (VLM); Juergen Mueller, John Ziemer, Amanda Green, and David Bame, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2003-240: PRELIMINARY RESULTS FROM A PERMANENT MAGNET HALL THRUSTER EVALUATION; JosÃ© Leonardo Ferreira and Ivan Soares Ferreira, Plasma Laboratory of Institute of Physics at University of Brasilia (UnB), ICC- Centro, Campus UniversitÃ¡rio Darcy Ribeiro – Asa Norte, 70910-900 BrasÃlia – DF, Brasil

2003-241: THE DESIGN OF MICRONEWTON FEEP THRUSTERS FOR DISTURBANCE REDUCTION SYSTEMS; Salvo Marcuccio, Alta / Centrospazio, Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-242: ELECTRIC PROPULSION SYSTEM FOR A MANEUVERABLE ORBITAL VEHICLE; Fabio Ceccanti and Salva Marcuccio, Alta S.p.A / Centrospazio, Via A. Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-243: MODEL OF HOLLOW CATHODE OPERATION AND LIFE LIMITING MECHANISMA; Ira Katz, John R. Anderson, James E. Polk, and Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA 91109, USA

2003-244: END-OF-MISSION CHARACTERIZATION OF THE ION THRUSTER ON DS1; John Brophy, Dave Brinza, James Polk, and Mike Henry, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California

2003-245: 3-DIMENSIONAL ION OPTICS SIMULATIONS USING AN IFE-PIC CODE; J. Wang, R. Kafafy, and T. Lin, Virginia Polytechnic Institute & State University, Blacksburg, VA 24061-0203

2003-246: APPLICATIONS OF MICROTHRUST SYSTEMS FOR MICROSPACECRAFT, DRAG-FREE, AND PRECISION CONSTELLATION STATIONKEEPING MISSIONS; John K. Ziemer, Juergen Mueller, Colleen M. Marrese, James E. Polk, and Robert F. Shotwell, Jet Propulsion Laboratory, M/S 125-109, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-247: A NEW ULTA-HIGH VACUUM FACILITY FOR PLUME CHARACTERIZATION AND NEUTRALIZATION STUDIES OF FEEP AND COLLOID THRUSTERS; John K. Ziemer, Colleen M. Marrese, Juergen Mueller and James E. Polk, Jet Propulsion Laboratory, M/S 125-109, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-250: CONDENSABLE PROPELLANTS AS AN OPTION FOR MULTI KILOWATT SPACE PROPULSION; S. O. Tverdokhlebov, A. V. Semenkin, B. S. Borisov, and F. F. Gabdullin, Central Research Insitute of Machine Building (TsNIIMASH), Russia; C. M. Marrese and J. E. Polk, Jet Propulsion Laboratory, USA

2003-251: DEVELOPMENT OF MICROWAVE ENGINE; S-W. Kim, Y. Aoki, A. Nagata, and T. Kizaki, Advanced Technology Institute, Sapporo, Hokkaido 006-0814, Japan; S. Satori, Hokkaido Institute of Technology, Sapporo, Hokkaido 006-8585, Japan; Y. Itoh, H. Okamoto, and T. M. Sugiki, Astro Research Corporation, Fujisawa, Kanagawa 251-0024, Japan

2003-253: HOLLOW CATHODE THRUST MEASUREMENTS USING A TARGET: INITIAL RESULTS AND SOME ISSUES; Paolo Gessini and Stephen B. Gabriel, Astronautics Research Group, School of Engineering Sciences, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, United Kingdom; David G. Fearn, EP Solutions, Fleet, Hants, GU14 0LX, United Kingdom

2003-257: EROSION OF MATERIALS USED ON A SATELLITE EXTERNAL SKIN BY ELECTRIC PROPULSION; T. Tondu and V. Viel-Inguimbert, ONERA/DESP 2, Avenue Edouard Belin, 31 055 Toulouse CÃ©dex, France; F. Darnon, CNES 18, Avenue Edouard Belin 31 401 Toulouse CÃ©dex, France

2003-258: SECONDARY ELECTRON EMISSION OF CERAMICS USED IN THE CHANNEL OF SPT; V. Viel-Inguimbert, ONERA/DESP 2, Avenue Edouard Belin, 31 055 Toulouse CÃ©dex France

2003-259: FUNDAMENTAL SCALING LAWS FOR ELECTRIC PROPULSION CONCEPTS; PART 1: HALL EFFECT THRUSTERS; Mariano Andrenucci, Leonardo Biagioni, Salvo Marcuccio, and Fabrizio Paganucci, Alta S.p.A/Centrospazio, Via A. Gherardesca 5, 56121 Ospedaletto, Pisa, Italy

2003-262: DEVELOPMENT OF A CLUSTER OF LOW POWER HALL THRUSTERS; Lawrence Byrne, Bruce Pote, George Kolencik, Rachel Tedrake, and Vlad Hruby, Busek Co. Inc. 11 Tech Circle, Natick, MA 01760-1023

2003-263: AN IMPROVED SMALL CLOSED DRIFT THRUSTER WITH BOTH CONDUCTING AND DIELECT RIC CHANNELS; A. I. Burgrova, A. D. Desiatskov, and V. K. Kharchevnikov, Moscow Institute of Radioelectronics, Moscow, Russia; H. R. Kaufman, Kaufman & Robinson Inc., Fort Collins, CO, U.S.A.; A. I. Morozov, Kurchatov_s Russian Research Center, Moscow, Russia; V. V. Zhurin, Front Range Fakel Inc., Fort Collins, CO, U.S.A.

2003-265: MODELING DEVELOPMENTS ON COLLOID THRUSTERS; Jorge A. Carretero, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139; Francisco J. Higuera, E.T.S. Ingenieros Aeronautics, Madrid Spain; Manuel Martinez-Sanchez, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139

2003-266: OVERVIEW OF ASTRIUM EROSION / CONTAMINATION MODELLING TOOL AND VALIDATION ON ONERA EXPERIMENTAL RESULTS; S. Provost, C. Theroude, and P. ChÃ©oux-Damas, ASTRIUM SAS, 31 avenue des Cosmonautes, 31402 Toulouse Cedex 4 (France)

2003-267: OVERVIEW OF ASTRIUM MODELLING TOOL FOR PLASMIC THRUSTER FLOW FIELD SIMULATION; C. Theroude, S. Provost, and P. ChÃ©oux-Damas, Astrium SASM 31 avenue des Cosmonautes, 31402 Toulouse Cedex 4 (France)

2003-270: PPS -1350-G QUALIFICATION STATUS MARCH 2003; Pierre Dumazert, Sophie EagardÃ©re-Verdier, FrÃ©dÃ©ric Marchandise, and Christophe R. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux; Pascal Garnero and Francois Balme, Alcatel Space Industries

2003-272: MAGNETIC NOZZLE PLASMA EXHAUST SIMULATION FOR THE VASIMR ADVANCED PROPULSION CONCEPT; A. G. Tarditi and J. V. Shebalin, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, TX (USA)

2003-273: CONTROL OF THE ACCELERATION REGION IN HALL THRUSTERS; David Staack, Yevgeny Raitses and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ 08543

2003-276: VACUUM ARC THRUSTER FOR CUBESAT PROPULSION; Jochen Schein, Andrew Gerhan, and Mahadevan Krishnan, Alameda Applied Sciences Corporation, San Leandro, CA, USA; Filip Rysanek, University of Illinois Urbana-Champaign, IL, USA

2003-277: MEDIUM AND HIGH CURRENT CATHODES FOR ELECTRIC PROPULSION: REVIEW OF RECENT DEVELOPMENTS AT LABEN/PROEL; J. Bussotti, M. Capacci, G. Matticari, G. E. Noci, A. Severi, and P, Siciliano, LABEN Proel Tecnologie Division, Viale Machiavelli, 31-50125 Firenze (Italy); R. Grill, PLANSEE AG A-6600, Reutte, Tyrol – Austria; D. Estublier, ESA/ESTEC Keplerlaan 1, 2200 AG Noordwijk – The Netherlands

2003-278: A COMPUTATIONAL STUDY OF SINGLE AND DOUBLE STAGE HALL THRUSTERS; Kay Sullivan, Manuel MartÃnez-SÃ¡nchez, Oleg Batishchev, and James Szabo, Massachusetts Institute of Technology, 77 Massachusetts Avenue, Cambridge, MA 02139

2003-279: FEEP SYSTEM FOR THE MICROSCOPE MISSION; Salvo Marcuccio and Lorenzo Serafini, Alta S.p.A. / Centrospazio, Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy; David Nicolini, ESA-ESTEC, Noordwijk, The Netherlands; Laurent Jolivet and Olivier Vandermarcq, CNES, Toulouse, France; Pierre Touboul, ONERA, Chatillon, France

2003-284: MAGNETIC CIRCUITS FOR HALL THRUSTERS; USE OF PERMANENT MAGNETS; P. Renaudin, V. Cagan, and M. Guyot, Laboratoire de MagnÃ©tisme et d’Opitque de Versailes, 45 avenue des Etats-Unis, 78035 Versailles, France; A. Cadiou, CNES, 18 avenue Edouard Belin, 31401 Toulouse cedex 4, France; P. Lasgorceix and M. Dudeck; Laboratoire d’ AÃ©othermique, 1C avenue de la Recherche Scientifique, 45071 OrlÃ©ans cedex, France; V. Vial, Groupe de Recherche sur l’EnergÃ©tique des Milieux IonisÃ©s, 12 rue de Blois, 45067 OrlÃ©ans cedex 2, France; P. Dumazert, SNECMA, AÃ©rodrome de Melun-Villaroche, 77550 Moissy-Cramayel, France

2003-285: CORONAL TYPE AND COLLISIONAL-RADIATIVE MODELLING OF RARE GASES PLASMA; K. Katsonis, A. Siskos, and M. Touzeau, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, UniversitÃ© Paris-sud 91405 Orsay, France

2003-286: EXPERIMENTAL RESEARCH PROGRESS TOWARD THE VASIMR ENGINE; Jared P. Squire and Verlin T. Jacobson, MuÃ±iz Engineering, Inc., Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, 77059, USA; Franklin R. Chang DÃaz, Advanced Space Propulsion Laboratory, NASA Johnson Space Center, Houston, Texas, USA; Tim W. Glover, Rice University, Advanced Space Propulsion Laboratory, Houston, Texas, USA; F. Wally, and Richard H. Goulding, Oak Ridge National Laboratory, Oak Ridge, Tennessee, USA; Roger Bentson, University of Texas at Austin, Austin, Texas, USA; Edgar A. Bering III, University of Houston, Houston, Texas, USA; Kristy A. Stokke, Massachusetts Institute of Technology, Cambridge, Massachusetts, USA

2003-287: FLOW CHARACTERISTICS OF SUPERSONIC LASER-SPIKE ENGINE; In-Seuck Jeung and Sung-Don Kim, Seoul National University, Seoul 151-744, Korea; Jeong-Yeol Choi, Pusan National University, Pusan 609-735, Korea

2003-288: DEVELOPMENT STATUS OF NEXT: NASA’S EVOLUTIONARY XENON THRUSTER; Scott W. Benson and Michael J. Patterson, NASA Glenn Research Center

2003-289: RADIOFREQUENCY WITH MAGNETIC FIELD ION THRUSTER (RMT): REVIEW OF THE ENGINEERING PHASE ACCOMPLISHED UNDER ASI CONTRACT; M. Capacci, G. Matticari, G. E. Noci, and A. Severi, LABEN Proel Tecnologie Division, Viale Machiavelli, 31-50125, Firenze (Italy); A. Ricciardi and F. Svelto, Italian Space Agency (ASI), Viale Liegi 26-00198 Roma (Italy)

2003-290: RESEARCH ON TWO-STAGE ENGINE SPT-MAG; A. I. Morozov, Kurchatov’s Russia Research Center, Moscow, Russia 123098; A. I. Bugrova, A. D. Desiatskov, and V. K. Kharchevnikov, Moscow Institute of Radioelectronics, Moscow Russia 129110; M. Prioul, SNECMA MOTEURS, Site de Villaroche Nord, BP NÂ°93, 77552 Moissy-Cramayel Cedex, France; L. Jolivet, CNES, 18 avenue Edouard Belin, 31401 Toulouse Cedex 4, France

2003-291: FIELD EMISSION ELECTRIC PROPULSION PLUME EFFECTS ON MICROSCOPE SATELLITE; L. Jolivet and B. Debray, CNES, 18-avenue Edouard Belin, 31401 Toulouse Cedex 4 (France)

2003-292: TIME-RESOLVED SURFACE TEMPERATURE MEASURMENT FOR PULSED ABLATIVE THRUSTERS; Erik L. Antonsen and Rodney L. Burton, University of Illinois at Urbana-Champaign, IL 61801; Gregory G. Spanjers and Ronald A. Spores, AFRL Propulsion Directorate, Edwards AFB CA 93524

2003-293: PHENOMENOLOGICAL MODEL OF CURRENT SHEET CANTING IN PULSED ELECTROMAGNETIC ACCELERATORS; T. E. Markusic, Propulsion Research Center, NASA Marshall Space Flight Center, Huntsville, AL 35812; E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2003-294: THEME: ELECTRICAL PROPULSION ON SPACE VEHICLES: ELECTRICAL MOOVING

2003-295: THE DEVELOPMENT AND QUALIFICATION OF A 4.5 KW HALL THRUSTER PROPULSION SYSTEM FOR GEO SATELLITE APPLICATIONS-STATUS UPDATE; J. Fisher, A. Wilson, D. King, S. Meyer, and K. de Grys, Aerojet, P. O. Box 97009, Redmond, VA 98073-9709; L. Werthman, Lockheed Martin Space Systems Company, 1111 Lockheed Martin Way, Sunnyvale, CA 94089

2003-296: CONVERGENCE AND DEFLECTION OF A HALL THRUSTER PLUME; I. Viera, L. GargatÃ© and J. T. Mendonca, GoLP – Centro de Fisica de Plasmas, Instituto Superior TÃ©cnico, Av. Rovisco Pais, 1049-001, Lisboa-Portugal

2003-297: LOW POWER HALL THRUSTER FOR THE ESEO SATELLITE; L. GargatÃ© and I. Vieira, Instituto Superior TÃ©cnico, 1049-001 Lisbon, Protugal; N. Adams, University of Strathclyde – Glasgow, United Kingdom

2003-298: RESONANT OPERATION OF A MICRO-NEWTON THRUST STAND; Capt. James P. Lake, Lt. Greg Cavallaro and Greg Spanjers, AFRL Propulsion Directorate, Edwards AFB, CA 93524; Paul B. Adkison, Sverdrup Inc., Edwards AFB, CA 93524; Michael J. Dulligan, ERC, Inc., Edwards AFB, CA 93524

2003-299: PLASMA FLUCTUATIONS IN A MPD THRUSTER WITH AND WITHOUT THE APPLICATION OF AN EXTERNAL MAGNETIC FIELD; M. Zuin, V. Antoni, G. Regnoli, N. Vianello and M. Bagatin, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, Corso Stati Uniti, 4, I-35127 Padova (Italy), INFM, UnitÃ¡ di Padova, sez. A, (Italy); F. Paganucci, P. Rossetti, and M. Andrenucci, Centrospazio, Via A. Gherardesca 5, 56014 Pisa (Italy); R. Cavazzana, G. Serianni, and M. Spolaore, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, Corso Stati Uniti, 4, I-35127 Padova (Italy)

2003-301: DIAGNOSTICS OF AN APPLIED FIELD MPD THRUSTER; M. Andrenucci, F. Paganucci, and P. Rossetti, Department of Aerospace Engineering, Univ. of Pisa / Centrospazio, Via A. Gherardesca 5, 56014 Pisa; V. Antoni, M. Bagatin, R. Cavazzana, G. Serianni, and M. Zuin, RFX Consortium, Association Euratom-ENEA on Fusion, Corso Stati Uniti 4, 35127 Padova; M. R. Carraro, A. Cristofolini, and R. Ghidini, Department of Electrical Engineering, University of Bologna, Viale Risorgimento 2, 40136 Bologna

2003-302: PERFORMANCE OF AN APPLIED FIELD MPD THRUSTER WITH A PRE-IONIZATION CHAMBER; Fabrizio Paganucci, Paola Rossetti, and Mariano Andrenucci, CENTROSPAZIO, Via Gherardesca, 5, 56121, Pisa, Italy; Victor B. Tikhonov and Vladimir A. Obukhov, RIAME MAI, 125080 Moscow, PB 43, Russia

2003-303: SMART-1 EPS END-TO-END TEST: FINAL RESULTS & LESSONS LEARNT; Denis Estublier, ESA/ESTEC, Keplerlaan 1, Postbus 299, 2200 AG Noordwijk ZH, The Netherlands; Christophe Koppel, SNECMA Mouteurs, Division Moteurs-Spatiaux, DPES, Propulsion et Equipements Satellites, AÃ©rodrome de Melun-Villaroche

2003-304: EXPERIMENTAL STUDIES RELATED TO FIELD EMISSION THRUSTER OPERATION: EMISSION IMPACT ON SOLAR CELL PERFORMANCES AND NEUTRALIZATION ELECTRON BACKSTREMING PHENOMENA; E. Chesta, D. Nicolini, D. Robertson, and G. Saccoccia, European Space Agency, Electric and Advanced Propulsion Section, ESTEC, TOS-MPE, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2003-305: XENON RESISTOJETS AS SECONDARY PROPULSION ON EP SPACECRAFTS AND PERFORMANCE RESULTS OF RESISTOJETS USING XENON; D. Nicolini, D. Robertson, E. Chesta, and G. Saccoccia, European Space Agency, ESTEC, Noordwijk, The Netherlands; D. Gibbon and A. Baker, Surrey Satellite Technology Ltd., University of Surrey, Guildford, England

2003-306: COUPLED ELECTRODYNAMIC TETHER/ELECTROSTATIC PROPULSION SYSTEM; D. Nicolini, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2003-307: CHARACTERIZATION OF CURRENT SHEET EVOLUTION IN A PULSED ELECTROMAGNETIC ACCELERATOR; J. W. Berkery and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey 08540

2003-308: ADVANCES IN THE PULSED INDUCTIVE THRUSTER DRIVE SYSTEM; M. Franklin Rose, Radiance Technologies, Inc., 500 Wynn Dr. Suite 504, Huntsville, AL 35816; Henry W. Brandhorst Jr., Space Research Institute, 231 Leach Center, Auburn University, AL 36849-5320

2003-311: STUDY OF MULTI THRUSTER ASSEMBLY OPERATION; L. E. Zakharenkov, A. V. Semenkin, A. V. Rusakov, N. A. Urchenko, S. O. Tverdokhlebov, and V. I. Garkusha, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070; U. V. Lebedev and S. N. Podkolsin, Institute of Space Research, Moscow, Russia; J. M. Five, U.S. Air Force Laboratory Edwards, AFB, CA

2003-312: ANALYSIS OF PROSEDS BARE-TETHER PERFORMANCE; J. R. SanmartÃn, Universidad PolitÃ©cnica de Madrid, Spain; E. C. Lorenzini and M. L. Cosmo, Harvard-Smithsonian Center for Astrophysics, Cambridge, MA, USA; R. D. Estes, OnScreen Science, Inc. Cambridge, MA, USA

2003-313: NEXT GENERATION ION ENGINES: MISSION PERFORMANCES; Muriel Noca, Jet Propulsion Laboratory, California Institute of Technology, MS 301-180, 4800 Oak Grove Drive, Pasadena, CA 91109

2003-316: ELECTRON CURRENTS IN HALL THRUSTER; Igor Levchenko, National Aerospace University, Kharkov, Ukraine; Michael Keidar, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109

2003-319: ELECTRIC PROPULSION SYSTEMS WITH FAST NON-INCANDESCENT START; Mykola V. Bilan, Volodymyr I. Bilokon, Mykola M. Koshelev, Andriy V. Loyan, Sergiy Yu. Nesterenko, Anatoliy I. Oranskiy, and Mykola P. Stepanushkin, Scientific & Technological Center of Space Power & Engines at National Aerospace University, “Kharkov Aviation Institute”, 17, Chkalov St., Kharkov, 61070, Ukraine

2003-320: THE INFLUENCE OF STATIONARY PLASMA THRUSTER FACTORS ON FUNCTIONAL PARAMETERS OF NEUTRALIZER CATHODE; Mykola V. Bilan, Volodymyr I. Bilokon, Sergey V. Veryutin, Volodymyr D. Olendarev, and Anatoliy I. Oranskiy, Scientific & Technological Center of Space Power & Engines at National Aerospace University “Kharkov Aviation Institute”, 17, Chkalov St. Kharkov, 61070, Ukraine

2003-321: TWO DIMENSION EFFECTS IN ION FLOW INSIDE INTER-ELECTRODE GAP OF PLASMA-ION THRUSTER ION OPTICAL SYSTEM; Sergey Yu. Nesterenko and Anatoily I. Oranskiy, Scientific & Technological Center of Space Power & Engines at National Aerospace University “Kharkov Aviation Institute”, 17, Chkalov St. Kharkov, 61070, Ukraine

2003-327: FURTHER INVESTIGATIONS OF AN OPEN DRIFT HALL THRUSTER WITH BORON NITRIDE AND DIAMOND WALL; N. Gascon, C. Thomas, W. Hermann, and M. A. Cappelli, Stanford University, Mechanical Engineering Department, Thermosciences Division, Stanford, CA 94305-3032

2003-328: WALL EFFECTS ON THE EXCITATION AND PROPAGATION OF INSTABILITIES IN HALL THRUSTERS; N. Gascon and M. A. Cappelli, Stanford University, Mechanical Engineering Department, Thermosciences Division, Stanford, CA 94305-3032

2003-329: A NEW LARGE VACUUM TEST FACILITY FOR HIGH POWER ELECTRIC PROPULSION TESTING; Fabrizo Scortecci, AEROSPAZIO Tecnologie s.r.l., I-53040 Rapolano Terme, Siena, Italy

2003-330: IN-SPACE PROPULSION PROGRAM OVERVIEW AND STATUS; Paul F. Wercinski, ISP Program Executive, Solar System Exploration Division, NASA Headquarters, Office of Space Science, Washington, D.C. 20546; Les Johnson, In Space Transportation Investment Area Manager, Advanced Space Transportation Program/TD15, NASA Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812; Randy M. Baggett, Project Manager, Next Generation Ion, Advanced Space Transportation Program/TD15, NASA Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812

2003-331: RECENT RESULTS FROM A MODEL OF THE HALL THRUSTER DISCHARGE; E. Ahedo, J. M. Gallardo, F. I. Parra, and C. PÃ©rez Trigo, E.T.S.I. AeronÃ¡uticos, Universidad PolitÃ©cnica de Madrid, Spain

2003-332: THE HELICON DOUBLE LAYER THRUSTER; Rod Boswell and Christine Charles, Space Plasma and Plasma Processing, PRL/RSPhySE, Australian National University, Canberra ACT 0200

2003-333: INTERACTION OF A HOLLOW CATHODE STREAM WITH A HALL THRUSTER; L. AlbarÃ©de, V. Largo, P. Lasgorceix, and M. Dudeck, Laboratoire d’ AÃ©rothermique, 1C avenue de la Recherche Scientifique, 45071 OrlÃ©ans cedex, France; A. I. Bugrova, Moscow State Institute of Radio-Engineering Electronics and Automation, MIREA, Laboratory of Plasmotics, 78, 117454, Moscow, Russia; K. Malik, Imperial College, London, Great-Britain

2003-334: MODELING AND OPTICAL DIAGNOSTICS OF AN AR PLASMA UNDER PLASMA THRUSTER CONDITIONS; K. Katsonis, S. Bliman, and A. Siskos, Laboratoire de Physique des Gaz et des Plasmas (LPGP), UMR 8578, UniversitÃ© Paris-sud 91405, Orsay cedex, France; S. Pellerin, Ch. De Izarra, and J. Chapele, Laboratoire d’Analyse Spectroscopique et d’EnergÃ©tique des Plasmas (LASEP), UniversitÃ© d’OrlÃ©ans-Site de Bourges, rue Gaston Berger, BP 4043, 18028 Bourges cedex, France; K. Dzierzega, M. Smoluchowski Institute of Physics, Jagiellonian University, ul. Reymonta 4 30-059 KrakÃ³w, Poland; M. Tanguy, Laboratoire de Physique et Technologie des Plasmas (LPTP), Ecole Polytechnique 91128 Palaiseau, France

2003-335: AN ALTERNATIVE THEORY OF TRANSIT-TIME OSCILLATIONS IN HALL THRUSTERS; Serge Barral, Zbigniew Peradzynski, and Karol Makowski, Institute of Fundamental Technological Research – PAS; Swietokrzyska 21, 00049 Warsaw, Poland; Michael Dudeck, CNRS Laboratoire d’ AÃ©othermique, 45071 OrlÃ©ans, France

2003-336: TAL RELATIVE EROSION RATE REAL-TIME MEASUREMENTS THROUGH ANALYSIS OF ITS EMISSION SPECTRA; O. S. Tverdokhlebov, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia 141070; G. F. Karabadzhak, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia 141070

2003-339: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN JAPAN; Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2003-340: STATE OF THE ART AND PROSPECTS OF ELECTRIC PROPULSION IN RUSSIA; Vyacheslav Murashko, Alexander Koryakin, and Arkadij Nyatin, Design Bureau Fakel, 181 Moskovsky prospect, Kaliningrad, 236000, Russia; Vladimir Kim and Garry Popov, Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (RIAME MAI), Moscow, Russia; Anatoly Romashko, Yuri Yermoshkin, and Victor Petrusevich, Reshetnev Scientific and Production Association of Applied Mechanics (NPO PM), Zheleznogorsk, Krasnoyarsk Region, Russia; Oleg Gorshkov and Anatoly Koroteyev, Keldysh Research Center (KeRC), Moscow, Russia; Valrey Garkusha and Alexander Semenkin, Sergei Tverdokhlebov Central Institute of Machine-building (TsNIIMASH), Korolev of Moscow Region, Russia

2003-341: INTRODUCTION TO THE EUROPEAN ACTIVITIES IN ELECTRIC PROPULSION; G. Saccoccia, Head of Propulsion and Aerothermodynamics Division, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2003-366: INTEGRAL AND SPECTRAL CHARACTERISTICS OF ATON STATIONARY PLASMA THRUSTER OPERATING ON KRYPTON AND XENON; A. I. Bugrova, A. S. Lipatov, A. M. Bishaev, V. K. Kharchevnikov, and M. V. Kozintseva, Moscow Institute of Radio Engineering, Electronics and Automation (Technical University), Laboratory of Plasmaoptics, prosp. Vernadskogo, 78, Moscow, Russia, 119454; A. I. Morozov, Russian Scientific Center “Kurchatov Institute”, Kurchatov sq., 1, Moscow, Russia 123182

2003-367: HYBRID PARTICLE-FLUID MODEL OF A HALL THRUSTER PLUME; Francesco Taccogna, Savino Longo, and Mario Capitelli, IMIP-CNR sect. Bari, Italy, Department of Chemistry, University of Bari, Italy

2003-368: A PARALLEL PIC CODE FOR A HALL THRUSTER SIMULATION; I. Vieira, L. GargatÃ©, R. Fonseca, L. Silva, and J. T. Mendoca, GoLP – Centro de Fisica de Plasmas, Instituto Superior TÃ©cnico, Av. Rovisco Pais, 1049-001, Lisboa-Portugal

2003 FILE DIRECTORY

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2005 INDEX

2005-001: ELECTRIC PROPULSION THRUSTER POINTING MECHANISM (TPM) FOR EUROSTAR 3000: DESIGN & DEVELOPMENT TEST RESULTS; Manfred Falkner, Theodor Nitschko, Josef Zemann, Gerhard Mitterbauer, and Gerhard Traxler, Austrian Aerospace GmbH (AAE), Vienna, A-1120, Austria; Alain Demaire, EADS-Astrium, 31402 Toulouse, France

2005-002: EFFECT OF MAGNETIC FIELD PROFILE ON THE ANODE FALL IN A HALL THRUSTER; Leonid A. Dorf, Yevgeny F. Raitses, and Nathaniel J. Fisch, Princeton Plasma Laboratory (PPPL), Princeton, NJ 08543, USA

2005-003: SPACECRAFT/THRUSTERS INTERACTION ANALYSIS FOR SMART-1; J. Gonzalez del Amo and D. Estublier, ESA Technical and Operational Support Directorate ESTEC, Noordwijk, The Netherlands; C. Koppel, Snecma; M. Capacci, M. Tajmar, and A. Passaro, Alenia-Laben, ARC, Alta Spa

2005-004: INVESTIGATION OF THE LOCAL PLASMA PARAMETER DISTRIBUTIONS IN THE SPT ACCELERATING CHANNEL UNDER INCREASED DISCHARGE VOLTAGES; Vladimir Kim, Vycheslav I. Kozlov, Alexander I. Skrylnikov, Lev N. Umnitsin, and Victoria V. Svotina, Research Institute of Applied Mechanics and Electrodynamics (RIAME), 4 Volokolamskye shosse, Moscow, 125871, Russia; Andre Bouchoule, Orleans University, France; Mathieu Prioul, Snecma Moteurs, France

2005-005: RESEARCH AND DEVELOPMENT STATUS OF JAXA NEXT-GENERATION ION ENGINE; Shoji Kitamura, Yukio Hayakawa, Hideki Yoshida and Yasushi Okawa, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; Ken-ichi Kajiwara, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2005-006: IMPLEMENTATION OF EXTERNALLY-APPLIED MAGNETIC FIELDS TO A NON-IDEAL MHD SOLVER FOR MPD THRUSTER SIMULATION; P.C. Norgaard and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University, Princeton, NJ, 08544, USA; S. C. Jardin, Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ 08643, USA

2005-007: RESONANT CAVITY HOLLOW CATHODE PROGRESS; Kevin D. Diamant, The Aerospace Corporation, Los Angeles, CA 90009

2005-008: COMPARISON OF EXPERIMENTAL AND COMPUTATIONAL SIMULATIONS RESULTS OF A PULSED PLASMA ACCELERATOR; T. Moeller, D. Keefer, R. Rhodes, and D. Rooney, University of Tennessee Space Institute, Tullahoma, TN 37388, USA; D. Li and C. Merkle, Purdue University, West Lafayette, IN 47907, USA

2005-009: THE CHARGED PARTICLE BEAM SYSTEM OF AN ELECTROSTATIC ION THRUSTER AS AN ANTENNA BEACON ABOARD A SATELLITE; K. Malik, Imperial College, London, SW7 2BZ, UK; J. Gonzalez del Amo, European Space Agency, ESTEC, TOS-MPE, Noordwijk aan Zee (NL)

2005-010: ASTEROID RENDEZVOUS OF HAYABUSA EXPLORER USING MICROWAVE DISCHARGE ION ENGINES; Hitoshi Kuninaka, Kazutaka Nishiyama, Ikko Funakai, Tetsuya, Yukio Shimizu and Jun’ichiro Kawaguchi, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229, Japan

2005-011: PERFORMANCE OF A LOW-POWER CYLINDRICAL HALL THRUSTER; Kurt A. Polzin, Thomas E. Markusic, Boris J. Stanojev and Amado Dehoyos, Propulsion Research Center, NASA – Marshall Space Flight Center, Huntsville, Alabama 35812; Yevgeny Raitses, Artem Smirnov, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory (PPPL), P. O. Box 451, Princeton, New Jersey 08543

2005-012: NUMERICAL MODEL OF PLASMA SHEATHS IN HALL THRUSTER; F. Taccogna, Max-Planck Instittue fÃ¼r Plasmaphysik, EURATOM Association, Wendelsteinstr. 1, Greifswald, D-17491, Germany; S. Longo and M. Capitelli, Dip. Di Chimica, UniversitÃ¡ degli Studi di Bari, Via Orabona 4, Bari, I-70126, Italy

2005-013: A HYDRODYNAMIC-BASED EROSION MODEL FOR HALL THRUSTERS; John T. Yim, Michael Keidar, and Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109, USA

2005-014: ANALYSIS OF PLUME BACKFLOW FROM A LITHIUM MAGNETOPLASMADYNAMIC THRUSTER; Ian D. Boyd, Kevin Scavezze, and Chunpei Cai, University of Michigan, Ann Arbor, Michigan, 48109, USA; James E. Polk, NASA Jet Propulsion Laboratory, Pasadena, California, 91109, USA; Edgar Y. Choueiri, Princeton University, Princeton, New Jersey, 08544, USA

2005-015: EFFECTS OF CHANNEL WALL MATERIAL ON PERFORMANCE AND PLASMA CHARACTERISTICS OF HALL THRUSTERS; Hirokazu Tahara, Katsumi Imanaka, and Seiro Yuge, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-016: DEVELOPMENT OF THE TOP HAT ELECTRIC PROPULSION PLUME ANALYZER (TOPAZ): MASS ANALYZER DESIGN AND PRELIMINARY CALIBRATION DATA; Allen L. Victor , Thomas Zurbuchen, and Alec D. Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2005-017: PERFORMANCE CHARACTERISTICS OF LASER ABLATIVE THRUSTERS FOR SMALL SATELLITES; Hirokazu Tahara, Elichiro Koizumi, and Shin-ichiro Kitagawa, Graduate School of Engineering Science, Osaka Universi04, Toyonaka, Osaka 560-8531

2005-018: SILICON NITRIDE SPRAYING USING QUASI-STEADY MPD ARCJETS; Hirokazu Tahara and Toshiaki Edamitsu, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-019: LEVEL SET SIMULATIONS OF CHARGED DROPLETS USING A BOUNDARY ELEMENT METHOD; Anton VanderWyst, University of Michigan, Ann Arbor, MI 8109-210, USA; Andrew Christlieb, University of Michigan, Ann Arbor, MI 8109-103, USA; Mark Sussman, Florida State University, Tallahassee, FL 32306-510, USA; Ian D. Boyd, University of Michigan, Ann Arbor, MI 8109-210, USA

2005-020: PERFORMANCE ENHANCEMENT OF A 1-KW ANODE-LAYER HALL THRUSTER; Seiro Yuge and Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka, 560-8531, Japan

2005-021: THEORETICAL ANALYSIS OF ANOMALOUS CONDUCTIVITY IN HALL EECT THRUSTERS; A. Ducrocq, J. C. Adamy, A. Heronzand, and G. Lavalx, Centre de Physique Theorique, Ecole Polytechnique, CNRS UMR, 7644 Palaiseau, 91128, France

2005-022: POTENTIAL STRUCTURE AND PROPELLANT FLOW RATE THEORY FOR ION THRUSTER DISCHARGE CATHODE EROSION; Joshua L. Rovey and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI, 48109, USA; Daniel A. Herman, QSS Group, Inc., Cleveland, OH 44135, USA

2005-023: NEW GENERATION PROPELLANT FLOW CONTROL COMPONENTS FOR ELECTRIC PROPULSIOIN SYSTEMS: STATUS OF ACHIEVEMENTS AT ALCATEL ALENIA SPACE ITALIA/LABEN-PROEL; G. Matticari, G. E. Noci, and P. Siciliano, Alcatel Alenia Space Italia, BU Pro. El, via A. Enstain 35, 50013, Campi Bisenzio, Firenze; G. Martini and A. Rivetti, Istituto Metrologia Guido Colonnetti (IMGC) CNR Torino; N. Kutufa, AOES – BV Leiden – ESA/ESTEC, TOS-MPE, Keplerlaan I, Noordwijk (NL)

2005-024: INTERNAL PLASMA STRUCTURE MEASUREMENTS OF A HALL THRUSTER USING XENON AND KRYPTON PROPELLANT; Jesse A. Linnell and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI 48109, USA

2005-026: DESTRUCTIVE PHYSICAL ANALYSIS OF HOLLOW CATHODES FROM THE DEEP SPACE 1 FLIGHT SPARE ION ENGINE 30,000 HR LIFE TEST; Anita Sengupta, Jet Propulsion Laboratory, Pasadena, CA 91109, US

2005-028: NON-LOCAL ELECTRIC FIELD EFFECTS IN MAGNETIZED PLASMAS; Cliff A. Thomas, Nicolas Gascon, Michelle Allis, Emmanuelle Sommier, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305-3032

2005-029: DEMONSTRATION OF ION HEATING AND ACCELERATION IN A FAST-FLOWING PLASMA FOR THE VASIMR THRUSTER; A. Ando, M. Inutake, K. Hattori, H. Tobari, M. Hatanaka, and M. Shibata, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2005-031: FORTY YEARS OF GIESSEN EP-ACTIVITIES AND THE RECENT RIT-MICROTHRUSTER DEVELOPMENT; H. W. Loeb, K. – H. Schartner, B. K. Meyer, D. Feili, St. Weis, and D. Kirmse, 1^st Institute of Physics, Giessen University, Giessen D 35392, Germany

2005-033: EXPERIMENTAL INVESTIGATION OF MAGNETIC FIELD TOPOLOGY INFLUENCE ON STRUCTURE OF ACCELERATING LAYER AND PERFORMANCE OF HALL THRUSTER; Nikolay V. Blinov, Oleg A. Gorshkov, and Andrey A. Shagayda, Keldysh Research Center, Moscow, Russia

2005-035: FULLY KINETIC MODELING OF LOW-POWER HALL THRUSTERS; Sergey V. Irishkov, Oleg A. Gorshkov, and Andrey A. Shagayda, Keldysh Research Center, Moscow, Russia

2005-036: EFFECT OF ANTENNA CONFIGURATION ON THRUST PERFORMANCE IN A MINIATURE MICROWAVE DISCHARGE ION ENGINE; Naoji Yamamoto, Hiroshi Kataharada Takayuki Chikaoka, Hirokazu Masui, and Hideki Nakashima, Graduate School of Engineering Sciences, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Yoshiyuki Takao, Oita National College of Technology, Maki, Oita, 870-0152, Japan

2005-037: ESTIMATION OF EROSION RATE BY ABSORPTION SPECTROSCOPY IN A HALL THRUSTER; Naoji Yamamoto, Graduate School of Engineering Sciences, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Shirgeru Yokota, Makoto Matsui, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, City, Bunkyo-ku, Tokyo, 113-8656, Japan

2005-038: NON-DIMENSIONAL PERFORMANCE TRENDS OF A PULSED PLASMA ACCELERATOR; John W. Berkery and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2005-040: SIMULATION OF HIGH-SPECIFIC-IMPULSE AND DOUBLE-STAGE HALL THRUSTERS; D. Escobar, A. Ant, and E. Ahedo, Universidad Politdcnica de Madrid, Spain

2005-041: ON CONDITIONS AT THE SHEATH BOUNDARIES OF A QUASINEUTRAL CODE FOR HALL THRUSTERS; D. Escobar and E. Ahedo, E.T.S.L Aeronduticos, Universidad Politdcnica de Madrid, Madrid 28050, Spain

2005-043: MODELING OF A MICRO-MACHINED PULSED PLASMA THRUSTER; Michael Keidar and Iain D. Boyd, University of Michigan, Ann Arbor, MI; Daniel Simon and Bohdan Cybyk, The Johns Hopkins University Applied Physics Laboratory, Laurel, MD

2005-044: PROGRESS IN HYDRODYNAMIC MODELING OF HALL THRUSTERS; Michael Keidar and Iain D. Boyd, University of Michigan, Ann Arbor, MI

2005-045: MODELING A TWO-STAGE HIGH-POWER BISMUTH ANODE LAYER THRUSTER AND ITS PLUME; Michael Keidar, Yongiun Choi, and Iain D. Boyd, University of Michigan, Ann Arbor, MI

2005-046: CHARACTERIZATION OF HALL EFFECT THRUSTER PLASMA OSCILLATIONS BASED ON THE HILBERT-HUANG TRANSFORM; Gerard Bonhomme and Cedric Enjolras, LPMI, UMR 7040 CNRS-UniversitÃ© Henri PoincarÃ©, BP 239, F-55506 Vandoeuvre-IÃ©s-Nancy Cedex, France; Jacek Kurzyna, Institute of Fundamental Technological Research, Polish Academy of Sciences, Swietokrzyska 21, 00049 Warsaw, Poland; StÃ©hane Mazouffre, Luc AlbarÃ©de, and Michael Dudeck II, Laboratoire d’ AÃ©rothermique, CNRS, 1C Avenue de la Recherche Scientifique, 45071 OrlÃ©ans Cedex 2, France

2005-047: HOLLOW CATHODE WITHOUT LOW-WORK-FUNCTION INSERT; H. R. Kaufman and J. R. Kahn, Kaugman & Robinson, Inc., Fort Collins, Colorado 80524, USA

2005-048: THREE-DIMENSIONAL PARTICLE SIUMLATION OF PLUME FLOWS FROM HALL THRUSTERS; Chunpei Cai, Iain D. Boydy and Quanhua Sunz, University of Michigan, Ann Arbor, Michigan, 48109, U.S.A.

2005-049: ADVANCED ELECTRIC PROPULSION CONCEPTS BASED ON MAGNETIC FLUX COMPRESSION AND EXPANSION; P. J. Turchi, Los Alamos National Laboratory, Los Alamos, NM 87545, USA

2005-051: PLUME MEASUREMENTS AND MINIATURIZATION OF THE HALL THRUSTERS WITH CIRCULAR CROSS-SECTIONAL DISCHARGE CHAMBERS; Atsushi Shirasaki and Hirokazu Tahara, Department of Mechanical Science and Bioengineering, Graduate School of Engineering Science, Osaka University, 1-3, Machikaneyama, Toyonaka, Osaka 560-8531, Japan

2005-052: THE DEPENDENCE OF THE ELECTRON TEMPERATURE ON THE DISCHARGE VOLTAGE FOR DIFFERENT HALL THRUSTER CONFIGURATIONS; Yevgeny Raitses, Artem Smirnov, David Staack, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ, 08543

2005-053: CONTROLLING ION ACCELERATION REGION IN HALL THRUSTERS; Yevgeny Raitses, David Staack, Leonid Dorf, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ, 08543; Michael Keidar, University of Michigan, Ann Arbor, MI 48109

2005-054: SWIRL ACCELERATION IN A QUASI-STEADY MPD THRUSTER BY APPLIED MAGNETIC NOZZLE; Yoichi Kagaya and Hirokazu Tahara, Osaka University, Toyonaka, Osaka, 560-8531, Japan

2005-055: RESEARCH AND DEVELOPMENT STATUS OF MICROWAVE DISCHARGE ION THRUSTER Âµ20, Kazutaka Nishiyama, Yukio Shimizu, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency / Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 229-8510, Japan; Takashi Miyamoto, Kyushu University, Koganei, Tokyo, 184-8584, Japan; Tatsuya Nakai, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan

2005-056: DEVELOPMENT OF A MICROWAVE-EXCITED MICROPLASMA THRUSTER; Yoshinori Takao, Kouichi Ono Kazuo Takahashi, and Koji Eriguchi, Department of Aeronautics and Astronautics, Kyoto University, Kyoto, 606-8501, Japan

2005-057: EFFECT OF CHARGE EXCHANGE ON 2D HALL THRUSTER SIMULATION; Michelle K. Allis, Nicolas Gascon, and Mark A. Cappelli, Stanford University, Stanford, CA 94305; Eduardo Fernandez, Eckerd College, St. Petersburg, FL, 33711

2005-058: STATIONARY REFERENCE BI DISCHARGE CELL FOR OPTICAL DIAGNOSTICS OF A BISMUTH HALL THRUSTER; David B. Scharfe and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA

2005-059: DEVELOPMENT OF AN APPLIED FIELD MAGNETOPLASMADYNAMIC THRUSTER DESIGN SUPPORTED BY NUMERICAL SIMULATIONS AT IRS; Daniel Haag, Monika Auweter-Kurz, Markus Fertig and Helmut Kurtz, UniversitÃ¤t Stuttgart, Institut FÃ¼r Raumfahrtsysteme (IRS), Pfaffenwaldring 31, 70550 Stuttgart, Germany

2005-060: TESTING OF A DIGITAL COLLOID THRUSTER FOR PRECISE THRUST THROTTLING; Mark D. Paine, Queen Mary, University of London, London, E1 4NS, United Kingdom

2005-061: PLASMA PARAMETERS INVESTIGATION IN THE NEAR CATHODE ZONE OF THE SPT DISCHARGE; A. A. Pereslavtsev and S. A. Khartov, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, 4, Volokolamskoe sh., Moscow, 125971, Russia

2005-062: SPT’S HIGH LIFETIME-SOME PROBLEMS OF SOLUTION; S. A. Khartov, A. B. Nadiradze, I. I. Shkarban, and Y. V. Zikeeva, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, 4, Volokolamskoe sh., Moscow, 125971, Russia

2005-063: AN INFRARED THERMOGRAPHY STUDY ON THE THERMAL LOAD EXPERIENCED BY A HIGH POWER HALL THRUSTER; S. Mazouffre, J. PÃ©rez Luna, D. Gawron, and M. Dudeck, Laboratoire d’AÃ©rothermique, CNRS, 1C Avenue de la Recherche Scientifique, OrlÃ©ans, 45071, France

2005-064: DEVELOPMENT STATUS OF 200MN CLASS XENON HALL THRUSTER OF MELCO; Toshiyuki Ozaki, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan; Yasutaka Inanaga, Mitsubishi Electric Corporation, Amagasaki, Hyogo, 661-8661, Japan; Takafumi Nakagawa and Hiroyuki Osuga, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan

2005-065: DIRECT MEASUREMENT OF LORENTZ FORCES IN AN APPLIED-FIELD MPD THRUSTER; H. Tobari, A. Ando, M. Inutake and K. Hattori, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8759, Japan

2005-066: THE XENON REGULATOR AND FEED SYSTEM FOR ELECTRIC PROPULSION SYSTEMS; Ray Thompson and Howard Gray, EADS Astrium Ltd, Portsmouth, PO3 5PU, UK

2005-067: HEAT FLUX MEASUREMENTS IN THE HALL THRUSTER PLUME; G. Makrinich and A. Fruchtman, Holon Academic Institute of Technology, Holon 58102, Israel; S. Shitrit, G. Appelbaum and J. Ashkenazy, Soreq NRC, Yavne 81800, Israel

2005-068: THE EFFECT OF THE MAGNETIC FIELD PROFILE OIN THE PLUME AND ON THE PLASMA FLOW IN THE HALL THRUSTER; A. Fruchtman, Holon Academic Institute of Technology, 52 Golomb St., Holon 58102, Israel

2005-069: PERFORMANCE IMPROVEMENT OF A LIQUID PROPELLANT PULSED PLASMA THRUSTER; Hiroyuki Koizumi, Yoko Kawazoe, Kimiya Komurasaki, and Yoshihiro Arakawa, University to Tokyo, Tokyo, 113-8656, Japan

2005-071: DEVELOPMENT OF HYBRID PIC/DSMC CODE; Monika Auweter-Kurtz, Markus Fertig, Dejan Petkow and Torsten Stindl, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, D-70550 Stuttgart, Germany; Martin Quandt and Claus-Dieter Munz, Institut fÃ¼r Aerodynamik und Gasdynamik, UniversitÃ¤t Stuttgart, D-70550 Stuttgart, Germany; Panos Adamidis, Michael Resch and Sabine Roller, HÃ¶chstleistungsrechenzentrum Stuttgart, D-70550 Stuttgart, Germany; Danilo D’Andrea and Rudolf Schneider, Institut fÃ¼r Hochleistungsimpuls and Mikrowellentechnik, Forschungszentrum Karlsruhe, D-76133 Karlsruche, Germany

2005-073: THE DISTINCTION BETWEEN THE EP PLUME EXPANSION IN SPACE AND IN VACUUM CHAMBER; Anatoly G. Korsun, Ekaterina M. Tverdokhlebova, Flur R. Gabdullin, Central Research Institute of Machine Building (TsNIIMASH), Pionerskaya str., 4, Korolev, Moscow region, 141070, Russia

2005-074: NUMERICAL PROCEDURE PERMITTING CALCULATION OF HOW A VACUUM CHAMBER INFLUENCES ELECTRIC PROPULSION THRUSTER JET EXPANSION; Toropov G. P., Student, Moscow Aviation Institute (State Technical University) MAI Engineering Plasma Computational Laboratory (EPCLab) 24b, Zalineynaya str., Vologda, 160010, Russia

2005-075: 1 KW AMMONIA ARCJET SYSTEM DEVELOPMENT FOR A SCIENCE MISSION TO THE MOON; Dagmar Bock, Monika Auweter-Kurtz, and Helmut L. Kurtz, UniversitÃ¤t Stuttgart, Institut fÃ¼r Raumfahrtsysteme. Pfaffenwaldring 31, D-0569 Stuttgart, Germany

2005-077: A 3D MODEL CALCULATING SPUTTERING AND DEPOSITING PROCESSES UNDER ELECTRIC PROPULSION THRUSTER TESTING IN A VACUUM CHAMBER; G. P. Toropov, Student, Moscow Aviation Institute (State Technical University) MAI Engineering Plasma Computational Laboratory (EPCLab), 24b, Zalineynaya str., Vologda, 160010, Russia; A. B. Nadiradze and S. A. Khartov, Moscow Aviation Institute (State Technical University) MAI Electric Propulsioin and Space Power Plants Department 4, Volokolamskoe sh., Moscow, 125971, Russia

2005-078: KINETIC SIMULATION OF EFFECTS OF SECONDARY ELECTRON EMISSION ON ELECTRON TEMPERATURE IN HALL THRUSTERS; D. Sydorenko and A. Smolyakov, University of Saskatchewan, Saskatoon, SK, S7H3E6, Canada; I. Kaganovich and Y. Raitses, Princeton University, Princeton, NJ, 08543, USA

2005-079: PLASMA DIAGNOSTICS ON XENON FOR APPLICATION TO ION THRUSTERS; Michael W. Winter, Monika Auweter-Kurtz, Thomas Pfrommer and Nataliya Semenova, UniversitÃ¤t Stuttgart, Institut fÃ¼r Raumfahrtsysteme (IRS), Pfaffenwaldring 31, 70550 Stuttgart, Germany

2005-080: HALL THRUSTER MODIFICATIONS FOR REDUCED POWER OPERATION; J. Ashkenazy, S. Shitrit, and G. Appelbaum, Propulsion Physics Laboratory, Soreq NRC, Yavne 81800, Israel

2005-081: THE EFFECT OF MOLAR CONDUCTIVITY UPON CURRENT AND THRUST IN A COLLOID ELECTROSPRAY THRUSTER SYSTEM; Katharine L. Smith, Matthew S. Alexander, and John P. W. Stark, Queen Mary University of London, London, E1 4NS, UK

2005-082: INMARSAT 4F1 PLASMA PROPULSION SYSTEM INITIAL FLIGHT OPERATIONS; Howard Gray, EADS Astrium Ltd, Portsmouth, PO3 5PU, UK; Severin Provost, EADS Astrium SAS, 31402 Toulouse Cedex 4, France; Michael Glogowski, Inmarsat Global Ltd, London, EC1Y 1AX, UK; Alain Demaire, EADS Astrium SAS, 31402 Toulouse Cedex 4, France

2005-083: IMPROVEMENT OF AN MPD THRUSTER PERFORMANCE WITH A LAVAL-TYPE MAGNETIC NOZZLE; M. Inutake, A. Ando, K. Hattori, H. Tobari, K. Harata and T. Komagome, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2005-084: THE ONSET OF VOLTAGE HASH AND ITS RELATIONSHIP TO ANODE SPOTS IN MAGNETOPLASMADYNAMIC THRUSTERS; Luke Uribarri and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, New Jersey, 08544

2005-085: NUMERICAL SIMULATION OF FARADAY PROBE MEASUREMENTS IN A MULTI-COMPONENT NON-EQUILIBRIUM PLASMA; Jeremiah J. Boemer and Iain D. Boyd, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI, 48109

2005-086: DEVELOPMENT OF A CAPACITIVELY COUPLED INSERT-FREE RF-NEUTRALIZER; St. Weis, K. H. Schartner, H. LÃ¶b, and D. Feili, University of GieÃŸen, 1. Physikalisches Institut, Heinrich-Buff-Ring 16, 35392 GieÃŸen

2005-087: VOLTAGE EFFECTS ON THE VOLUMETRIC FLOW RATE AND THRUST PRODUCED IN ELECTROSPRAY PROPULSION SYSTEMS; Matthew S. Alexander, Katharine L. Smith, and John P. W. Stark, Queen Mary, University of London, London, E1 4NS, UK

2005-088: LOWER-HYBRID INSTABILITY IN HALL THRUSTER; Alexander Kapulkin and Moshe Guelman, Asher Space Research Institute Technion, I.I.T., Haifa, 32000, Israel

2005-089: NUMERICAL INVESTIGATION OF IONIZATION AND ACCELERATION PROCESSED IN A SELF-FIELD MPD THRUSTER; K. Kubota, Tokyo Institute of Technology, Yokohama, Kanagawa, 226-8503, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Okuno, Tokyo Institute of Technology, Yokohama, Kanagawa 226-8503, Japan

2005-092: SPACE CHARGE NEUTRALIZATION USING NEGATIVE IONS AND DUST PARTICLES IN THE ION AND HALL THRUSTERS; Artem Smimov, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, New Jersey 08543

2005-093: ION ACCELERATION BY SINGLE PASS ION CYCLOTRON HEATING IN THE VASIMR ENGINE; Edgar A. Bering, III and Michael Brukardt, University of Houston, Houston, TX, 77204-5005, USA; Franklin R. Chang-Diaz, Jared P. Squire, Timothy W. Glover, Verlin Jacobson, Alfonso Tarditi, and Gred McKaskill, AdAstra Rocket Company, Houston, TX, 77058, USA; Roger D. Bengtson, University of Texas at Austin, Austin, TX 78712

2005-094: EXPERIMENTAL AND THEORETICAL STUDIES OF THE LITHIUM-FED MULTICHANNEL AND SINGLE-CHANNEL HOLLOW CATHODE; Leonard D. Cassady and Edgar Y. Choueiriy, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey, 08544

2005-095: ION THRUSTER OPTICAL PERFORMANCE ENHANCEMENT VIA ION-EMISSIVE-SURFACE SHAPING; Paul J. Wilbur, Cody Farnell, and John D. Williams, Colorado State University, Fort Collins, Colorado, 80523, USA

2005-096: MODELING OF COLLISIONLESS AND KINETIC EFFECTS IN THRUSTER PLASMAS; Igor D. Kaganovich, Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2005-098: ELECTRON CROSS-FIELD TRANSPORT IN A 100 W CYLINDRICAL HALL THRUSTER; Artem Smimov, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, P. O. Box 451, Princeton, New Jersey 08543

2005-099: THE EFFECT OF MAGNETIC FIELD ON THE PERFORMANCE OF LOW-POWER CYLINDRICAL HALL THRUSTERS; Artem Smimov, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, P.O. Box 451, Princeton, New Jersey, 08543

2005-100: THE COAXIAL HIGH ENERGY THRUSTER; Flavio Poehlmann, Nicolas Gascon, Cliff Thomas, Mark Cappelli, Stanford University, Stanford, CA 94305, USA

2005-101: MECHANICAL ASSEMBLY OF ELECTROSPRAY THRUSTER GRID; B. Gassend, L. F. Velasques-Garc, A. I. Akinwandez, and M. Martnez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA

2005-104: AN EXPERIMENTAL STUDY OF CARBON NANOTUBE FIELD EMISSION CATHODES FOR ELECTRODYNAMIC TETHERS; Yasushi Okawa, Shoji Kitamura, and Satomi Kawamoto, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; Yasushi Iseki, Kiyoshi Hashimoto, and Etsuo Noda, Toshiba Corporation, Fuchu, Tokyo, 183-8511, Japan

2005-105: PERFORMANCE MEASUREMENT AND FLOWFIELD CALCULATION OF AN ELECTROTHERMAL PULSED PLASMA THRUSTER WITH A PROPELLANT FEEDING MECHANISM; Toshiaki Edamitsu and Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-106: RESEARCH AND DEVELOPMENT OF A PULSED PLASMA THRUSTER IN OSAKA UNIVERSITY; Toshiaki Edamitsu, Hirofumi Asakura, Akinori Matsumoto, and Hirokazu Tahara, Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan

2005-107: EXPERIMENTAL SIMULATION OF A PLASMA FLOW AROUND MAGNETIC SAIL; H. Kojima, University of Tsukuba, Tsukuba, Ibaraki, 2305-8577, Japan; I. Funaki, Y. Shimizu, H. Yamakawa, S. Shinohara, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan

2005-108: VHITAL-160 THERMAL MODEL BUILDING AND 3D THERMAL MODELING CARRYING-OUT; Svetlana A. Tverdokhlebova, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070; Oleg S. Tverdokhlebov, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070

2005-111: APPT PROPULSION SYSTEM FOR SMALL SATELLITES; Nikolay N. Antropov and Garry A. Popv, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Vladimir P. Khodnenko, All-Russian Research Institute of Electromechanics, 101000, P.O. Box 496, Moscow, Russia; Yuri I. Pugachev and Nikolay P. Shelkov, Russian Research Institute of Electromechanics, 143500, ul. Panfilova, Istra-2 Moscow region, Russia

2005-114: DEVELOPMENT STATUS OF POWER PROCESSING UNIT FOR 200MN-CLASS HALL THRUSTER; Hiroyuki Osuga, Kentarou Suzuk, Toshiyuki Ozaki, and Takafumi Nakagawa, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Ikuro Suga, Tomoyuki Kawakam, and Takuya Sakai, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-ho nmachi, Amagasaki, Hyogo, 661-8661, Japan; Yoshiyuki Akuzawa, Fumitoshi Soga, and Teppei Furuich, Engineering Department, Kamakura Engineering Office, Mitsubishi Electric Engineering Company Limited, 730 Kamimachiya, Kamakura, Kanagawa, 247-0065, Japan

2005-115: FEASIBLITY STUDY OF MAGNETOPLASMA SAIL; Ikkoh Funaki, Hiroshi Yamakawa, Hiroyuki Ogawa, Hiroyuki Nishida, and Iku Shinohara, Institute of Space and Astronautical Science, JAXA, Sagamihara, Kanagawa, 229-8510, Japan; Kazuhisa Fujita, Institute of Space Technology and Aeronautics, JAXA, Chofu, Tokyo, 182-8522, Japan; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan; Hirotaka Otsu, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan

2005-117: ON THE ANOMALOUS DIFFUSION MECHANISM IN HALL-EFFECT THRUSTERS; J. M. Gallardo and E. Ahedo, Universidad Politdcnica de Madrid, Spain

2005-118: EFFECTS OF PARTIAL THERMALIZATION AND SECONDARY EMISSION ON THE ELECTRON DISTRIBUTION FUNCTION IN HALL THRUSTERS; E. Ahedo and V. de Pablo, Universidad PolitÃ©cnica de Madrid, Madrid 28040, Spain; M. MartÃnez-SÃ¡nchez, Massachusetts Institute of Technology, Cambridge, MA 02139, USA

2005-119: THE SMART-1 HALL EFFECT THRUSTER AROUND THE MOON: IN FLIGHT EXPERIENCE; Christophe R. Koppel, Snecma, Safran Group, Division Moteurs Spatiaux, 77552 Moissy-Cramayel, France; Denis Estublier, ESA Technical and Operational Support Directorate ESTEC, Noordwijk, The Netherlands

2005-020: NUMERICAL INVESTIGATION OF LOW-FREQUENCY LONGITUDINAL OSCILLATIONS IN HALL THRUSTERS; S. Barral, Institute of Fundamental Technological Research, PAS, 0009, Warsaw, Poland; V. Lapuerta, A. Sancho and E. Ahedo, Universidad PolitÃ©cnica de Madrid, 2800 Madrid, Spain

2005-022: ON THE POSSIBILITIES OF RF ION THRUSTERS OPTIMIZATION; A. F. Alexandrov, E. A. Kralkina, V. B. Pavlov, and A. A. Rukhadze, Physical Department of Moscow State University, Vorobjevy gory, Moscow, Russia 119992; A. I. Bugrova, G. E. Bugrov, and K. V. Vavilin, Moscow Institute of Radiotechniks, Electronics and Automatics, (Technical University), Vemadskogo pr., 78, Moscow, Russia 117454

2005-023: MICRO-ARCJET: MICROFABRICATION WITH UV LASERS AND THRUST CHARACTERISTICS; Hideyuki Horisawa and Tsuyoshi Noda, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Kosuke Onodera, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2005-124: SPACE POTENTIAL FLUCTUATION IN AN ANODE-LAYER HALL THRUSTER; Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Department of Aeronautics and Astronautics, Hongo 7-3-1, Bunkyo, Tokyo 113-8656, Japan

2005-125: MEASUREMENT OF PLASMA BEAM ENERGY EFECTED FROM MICROWAVE DISCHARGE HALL THRUSTER; Hirohisa Kuwano, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science (ISAS), Japan, Aerospace Exploration Agency (JAXA), 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Hideki Nakashima, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan

2005-126: MICRO-THRUST BALANCE TESTING AND CHARACTERIZATION; Simone Rocca, University of Padova, Padova, 35131, Italy; Davide Nicolini, European Space Agency, Noordwijk, 2201 AZ, The Netherlands

2005-128: MODELING OF THE PULSED INDUCTIVE THRUSTER, (PIT) OPERATING WITH AMMONIA PROPELLANT; Pavlos G. Mikellides and Darcy L. Allison, Arizona State University, Tempe, AZ 85287, USA; Nalin Ratnayake, Arizona State University, Tempe, AZ 85287, USA; Deborah Booze, Arizona State University, Tempe, AZ 85287, USA

2005-129: PROBE DIAGNOSTICS IN A BISMUTH HALL THRUSTER; Alex Kieckhafer, Dean Massey, and Lyon B. King, Michigan Technological University, 815 R. L. Smith Bldg., Houghton, MI 49931

2005-130: ELECTRIC PROPULSION IN GERMANY: CURRENT PROGRAM AND PROSPECTIVES; Hans Meusemann, German Aerospace Center (DLR), 53227 Bonn, Germany; Michael Winter, Institute of Space Systems at Stuttgart University, 50550 Stuttgart, Germany; Contributions of members of the “German Working Group on Electric Propulsion (EP WG)”; Horst W. Loeb, Karl-Heinz Schartner, Monika Auweter-Kurtz, Rainer Killinger, Guenter Kornfeld, Harry Adirim, Michael Tartz, Holger Kersten, Ulrich Schwab, Michael Boss, and Hartmut Henkel

2005-132: THE “NEW GRID SYSTEMS FOR ION ENGINES” TECHNOLOGY PROJECT – RESULTS AND CONCLUSION; Hans J. Leiter and Rainer Kiillinger, EADS Space Transporation GmbH, MÃ¶ckmÃ¼hl, D-74215, Germany; Elisa Bonelli, Simone Scaranzin and Fabrizio Scortecci, Aerospazio S.r.l. Zona Industriale “SENTINO”, 53040 Rapolano Terme, Siena, Italy; Marco Capacci and Maurizio Materassi, ALENIA LABEN Proel Via A. Einstein 35, 50013 Campi Bisenzio (Firenze), Italy; Leonardo Biagioni, ALTA Via A. Gherardesca 5, Ospedaletto, Pisa, Italy; Niccola Kutufa, AOES-BV Leiden and European Space Research and Technology Centre, ESTEC/ESA, P.O. 299, 2200 Noordwijk, The Netherlands; Horst Neumann and Michael Tartz, IOM Leipzig, PermoserstaÃŸe 15, 04318 Leipzig, Germany; Davar Feili, University of Giessen, Heinrich Buff Ring 16, 35539 Giessen, Germany

2005-136: CHARACTERISTICS OF PPS-1350 TYPE THRUSTERS UNDER INCREASED DISCHARGE VOLTAGES AND COMPARISON WITH HYBRID CODES SIMULATION RESULTS; L. AlbarÃ©de and A. Bouchoule, Laboratoire GREMI, universitÃ© d’OrlÃ©ans France; A. Lazurenko, Laboratoire d’AÃ©rothermique CNRS 45071 OrlÃ©ans France; V. Kim, V. Kozlov, and A. Skrylnikov, RIAME Moscow Russia

2005-137: NUMERICAL STUDY OF A DOUBLE STAGE HALL EFFECT THRUSTER; C. Boniface, G.J.M. Hagelaar, L. Garrigues and J. P. Boeuf, CPAT, UMR 5002, UniversitÃ© Pau Sbatier, 118 Route de Narbonne, 31062 Toulouse Cedex 4, France; M. Prioul Snecma Moteurs DPES Site de Villaroche Nord BP93F 77552, Moissy-Cramayel, France

2005-138: PARTICLE SIMULATION OF HALL THRUSTER PLUMES IN THE 12V VACUUM CHAMBER; Iain D. Boyd, Quanhua Sun, and Cai Chunpei, University of Michigan, Ann Arbor, MI, 48109, USA; Kenneth E. Tatum, Aerospace Testing Alliance, Arnold Air Force Base, TN, 37389, USA

2005-139: GRID PERFORMANCE MODELS USING DESGIN OF EXPERIMENTS (DoE) METHODS; Michael Tartz, Jan H. Peters, and Horst Neumann, Leibniz-Institute for Surface Modification, Leipzig, Germany

2005-140: RESEARCH ON OPTIMIZATION OF ONBOARD MAGNETIC DIAGNOSTICS SYSTEM OF HALL THRUSTER PLASMA; Binyamin Rubin, Faculty of Aerospace Engineering, Technion, I.I.T., Haifa, 32000, Israel; Alexander Kapulkin and Moshe Guelman, Asher Space Research Institute Technion, I.I.T., Haifa, 32000, Israel

2005-141: AN OVERVIEW OF THE TsNIIMASH/ TsE EFFORTS UNDER VHITAL PROGRAM; Oleg S. Tverdokhlebov, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070; Sergey O. Tverdokhlebov, TsNIIMASH-EXPORT, Pionerskaya 4, Korolev, Moscow region, Russia 141070; Alexander V. Semenkin, TsNIIMASH, Pionerskaya 4, Korolev, Moscow region, Russia, 141070

2005-142: HIGH-FREQUENCY INSTABILITIES IN HALL-EFFECT THRUSTERS: CORRELATION WITH THE DISCHARGE CURRENT AND THRUSTER SCALE IMPACT; A. Lazurenko, Aerothernique Laboratory, CNRS, Orleans, France; L. AlbarÃ©de, and A. Bouchoule, GREMI Laboratory, Orleans University, France

2005-143: PYROLYTIC GRAPHITE AND CARBON-CARBON SPUTTER BEHAVIOUR UNDER XENON ION INCIDENCE; Michael Tartz and Horst Neumann, Leibniz-Institute for Surface Modification, Leipzig, Germany; Hans Leiter, EADS Space Technology, MÃ¶ckmÃ¼hl, Germany; Joachim Esch, Schunk Kohlenstofftechnik, Heuchelheim, Germany

2005-144: PARAMETIC STUDY OF THE ACCELERATION LAYER IN A HIGH POWER HALL EFFECT THRUSTER BY FABRY-PEROT SPECTROSCOPY; D. Gawron and s. Mazouffre,Laboratoire d’AÃ©rothermique, CNRS, 1c Avenue de la recherchÃ© scientific, 45071 OrlÃ©ans, France; C. Boniface, CPAT, CNRS, UniversitÃ© Paul Sabatier, 118 route de Narbonne, 31062 Toulouse, France

2005-145: OPERATION OF TWO-STAGE THRUSTER WITH ANODE LAYER IN “FLOATING ELECTRODE” SCHEME; Alexander E. Solodukhin and Alexander V. Semenkin, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, 141070, Russia

2005-146: INVESTIGATION OF PHYSICAL PROCESSES IN SPT MAG; A. I. Bugrova, A. V. Desyatskov, and V. K. Kharchevnikov, Moscow Institute of Radioengineering, Electronics and Automatics, Moscow, Russia; A. I. Morozov, RSC, Kurchatov Institute, Moscow, Russia; M. Priol, Snecma Moteurs, Satellite Propulsion and Equipment, Villaroche, France

2005-147: EVALUATION OF IMPURITY COMPOSITION AND CONTENT IN THE TAL AT VARIOUS OPERATING REGIMES; G. F. Karabadzhak, A. V. Semenkin, A. e. Solodukhin and O. S. Tverdokhlebov, Central Research Institute of Machine-Building (TSNIIMASH), Korolev, Moscow region, 141070, Russia

2005-149: A MINIATURIZED MICROWAVE DISCHARGE ION THRUSTER WITH HIGH HOLE NUMBER DENSITY GRID SYSTEM; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan; Ikkoh Funaki and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2005-152: HALL EFFECT THRUSTER WITH AN A1N DISCHARGE CHANNEL; S. Barral, Institute of Fundamental Technological Research – PAS, 0009, Warsaw, Poland; Y. Jayet, S. Mazouffre, and M. Dudeck, Laboratoire d’AÃ©rothermique – CNRS, 5071 OrlÃ©ans, France; E. Vron and P. Echegut, Centre de Recherche sur les Matdriaux Haute TempÃ©rature – CNRS, 5071 OrlÃ©ans, France

2005-153: FUNDAMENTALS OF DISCHARGE INITIATION IN GAS-FED PULSED PLASMA THRUSTERS; James E. Cooley and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University, Princeton, New Jersey 08544

2005-155: PERVEANCE AND BEAMLET EXPANSION MODELING OF THE NEXT ION ENGINE; Jerold W. Emhoff, Johns Hopkins University Applied Physics Laboratory, Laurel, Maryland, 20723; Iain D. Boyd, University of Michigan, Ann Arbor, Michigan, 48109; Cody C. Farnelland and John D. Williams, Colorado State University, Fort Collins, Colorado, 80523

2005-156: DEVELOPMENT OF A HIGH POWER ELECTRODELESS THRUSTER; Gregory D. emsellem, The Elwing Company, Wilmington, DE, 19801, USA

2005-158: ATON-TYPE SPT OPERATION AT HIGH VOLTAGES; A. I. Bugrova, A. S. Lipatov, and S. V. Baranov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia; A. I. Morozov, RSC Kurchatov Institute, Moscow, Russia

2005-160: EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF A MODIFIED RING CUSP NSTAR ENGINE; Anita Sengupta, Jet Propulsion Laboratory, Pasadena, CA, 91109, US

2005-161: SPT OPERATION IN “MACHINE-GUN” MODE; A. I. Bugrova, A. S. Lipatov, and S. V. Baranov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia; A. I. Morozov, RSC, Kurchatov Institute, Moscow, Russia; Yu Daren, Harbin Institute of Technology, Harbin, Chinese People’s Republic

2005-162: OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES IN FRANCE; Franck Darnon, Denis Arrat, Enrico Chesta, StÃ©phane d’Escrivan, and Nicolas Pillet; Centre National d’Etudes Spatiales, 18 av. E. Belin, 31401, Toulouse, France

2005-163: EXPERIMENTAL VERIFICATION OF THE NOZZLE SHAPE OPTIMIZATION FOR SELF-FIELD MPD THRUSTER; Daisuke Nakata and Yoshihiro Arakawall, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16, Nakaeho, Koganei-shi, Tokyo 184-8588, Japan; Ikkoh Funaki, Yukio Shimizu, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan

2005-164: THE EMISSIVE MEMBRANE ION THRUSTER CONCEPT; Paul J. Wilbur, Colorado State University, Fort Collins, Colorado, 80523, USA; Merrill Wilson and Kent Hutchings, Ceramatec, Inc., Salt Lake City, Utah, 84119, USA; John D. Williams, Colorado State University, Fort Collins, Colorado, 80523, USA

2005-167: SPECTRAL INVESTIGATION OF SPT MAG INSULATOR EROSION; A. I. Bugrova, A. M. Bishaev, A. V. Desyatskov and M. V. Kozintseva, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia; M. Prioul, Snecma Moteurs, Satellite Propulsion and Equipment, Villaroche, France

2005-168: DIAGNOSTICS FOR IN-SPACE TESTING OF HIGH POWER ELECTRIC THRUSTERS ON THE INTERNATIONAL SPACE STATION; D. Gregory Chavers, Chris Dobson, Jonathan Jones, and Jason Vaughn, NASA Marshall Space Flight Center, Huntsville, AL 35812, USA; Andrew Petro, NASA Johnson Space Center, Houston, Texas, 77058, USA; Franklin Chang-Diaz, Ad Astra Rocket Companny, Houston, Texas 77058, USA; Edgar Bering, University of Houston, Houston, Texas, 77204-5005, USA

2005-169: FROM THE PAST TO THE FUTURE; A. I. Morozov, RSC Kurchatov Institute, Moscow, Russia

2005-170: CHARACTERIZATION OF HIGH-DENSITY FLOWING PLASMAS USING A DIRECTIONAL MICRO-RETARDING POTENTIAL ANALYZER; James Partridge and Nikolaos A. Gatsonis, Worcester Polytechnic Institute, Worcester, MA 01609, USA

2005-171: DETAILS OF AN ANNULAR FIELD REVERSED CONFIGURATION PLASMA DEVICE FOR SPACECRAFT PROPULSION; David Kirtley, Daniel L. Brown, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109

2005-173: TRAJECTORY OPTIMIZATION USING GLOBAL METHODS; Michael A. Paluszek and Stephanie J. Thomas, Princeton Satellite S ystems, Princeton, NJ

2005-174: NUMERICAL REBUIDLING OF SMART-1 PLASMA PLUME-SPACERAFT INTERACTION; A Passaro, A. Vicini, F. Nania, and L. Biagioni, Alta SpA, Pisa, I-56121, Italy

2005-175: ELECTRIC THRUSTER PLUME SIMULATION: APPLICATION TO MPD AND FEED THRUSTERS; A. Passaro, F. Nania, F. Paganucci, L. Biagioni, and L. Priami, Alta S.p.A. Pisa, Italy, 56121

2005-176: SCALABLE FLAT-PANEL NANO-PARTICLE MEMS/NEMS THRUSTER; L. Musinski, T. Liu, B. Gilchrist, A. Gallimore, and M. Keidar, University of Michigan, Ann Arbor, MI 48109, USA

2005-177: RESPONSE OF A CYLINDRICAL PLASMA TO TIME-VARYING EXTERNAL ELECTROMAGNETIC FIELD: NUMERICAL SIMULATION STUDIES; Yasushi Ikeda, Tohru Hada, Syuichi Matsukiyo, and Shunjiro Shinohara, Kyushu University, 6-1 Kasuga-Kohen, Kasuga, Fukuoka 816-8580, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16 Naka-cho, Koganei-shi, Tokyo 184-8588, Japan

2005-181: EVALUATION OF RADIOSOTOPE ELECTRIC PROPULSION FOR SELECTED INTERPLANETARY SCIENCE MISSIONS; David Oh and Eugen Bonfiglio, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109-8099; Mike Cupples and Jeremy Belcher, Science Applications International Corporation, Huntsville, Alabama, 35806

2005-183: ENDURANCE TESTS OF 150 Âµ FEEP MICROTHRUSTERS; M. Andrenucci, L. Biagioni, F. Ceccanti, and M. Saviozzi, Alta S.p.A., Pisa, 56121, Italy; D. Nicolini, European Space Technology Centre – ESA, Noordwijk, AG2200, The Netherlands

2005-184: MEASUREMENT FEATURES AND RESULTS OF TAL D-55 PLUME; Leonid E. Zakharenkov and Alexander V. Semenkin, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, 141070, Russia; Yuri V. Lebedev, Institute of Space Research, Moscow, Russia

2005-185: STUDY OF THE 3-TAL THRUSTER ASSEMBLY OPERATION; Leonid E. Zakharenkov, Alexander V. Semenkin and Valeri I. Garkusha, Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, 141070, Russia; Yurii V. Lebedev, Institute of Space Research, Moscow, Russia

2005-186: HELICON MAGNETOPLASMADYNAMIC (HMPD) THRUSTER CONCEPT; Lachlan Blackhall, University of Sydney, Sydney, NSW, 2999, Australia

2005-187: HALL THRUSTER SCALING METHODOLOGY; Mariano Andrenucci, Alta S.p.A., 56121 Ospedaletto, Pisa, Italy; Francesco Battista and Pietro Piliero, Centrospazio, 56121 Ospedaletto, Pisa, Italy

2005-189: WALL EROSION IN 2D HALL THRUSTER SIMULATIONS; Emmanuelle Sommier, Michelle K. Allis, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305

2005-191: PRELIMINARY TESTING OF A COAXIAL HALL THRUSTER WITH A DIAMOND NOSE CONE; Nicolas Gascon, W. Scott Crawford, Ronald L. Corey, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA; David White, WE Research, LLC, Rosamond, CA 93560, USA

2005-192: PERFORMANCE CHARACTERISITCS OF A LINEAR IONIC LIQUID ELECTROSPRAY THRUSTER; Paulo Lozano, Benajmin Glass and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA 02139, USA

2005-193: PLUME EFFECTS ON RADIATION DETECTION BY SPACECRAFT; Murat Celik and Manuel Martinez-Sanchezy, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2005-194: XE+-SPUTTERED MOLYBDENUM PROPERTIES OF LOW IMPINGEMENT ENERGY; Mark W. Crofton, The Aerospace Corporation, El Segundo, CA 90245, USA; Johnathan C. Murray, The University of Michigan, Ann Arbor, MI 48109-2140, USA; James E. Pollard, The Aerospace Corporation, El Segundo, CA, 90245, USA

2005-195: THE CHARACTERIZATION OF SILICON WETTABILITY AND PROPERTIES OF EXTERNALLY WETTED MICROFABRICATED ELECTROSPRAY THRUSTER ARRAYS; Tanya Cruz Garza, Paulo Lozano, Luis F. VelÃ¡squez-Garc Ãa, and Manuel Martinez Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2005-196: HALL THRUSTER WITH AN EXTERNAL ACCELERATION ZONE; Nicolas Gascon, Ronald L. Corey, and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA; William A. Hargus, Jr., Air Force Research Laboratory, Edwards AFB, 93524, USA

2005-197: A TWO-DIMENSIONAL (Z-0( FLUID/PIC SIMULATION OF COAXIAL HALL THRUSTERS; Eduardo Fernandez, Eckerd College, St. Petersburg, FL 33711; Aaron Knoll and Marck Cappelli, Stanford University, Stanford, CA 94035; Tarik Kaya, Carleton University, Ottawa, ON K1S 5B6, Canada

2005-198: ULTRA-LOW POWER STATIONARY PLASMA THRUSTER; Tsuyohito Ito, Nicolas Gascon, W. Scott Crawford, and Mark A. Cappelli, Stanford University, Stanford, California, 94305-3032, USA

2005-200: NUMERICAL SIMULATION OF THE HOLLOW CATHODE DISCHARGE PLASMA DYNAMICS; Ioannis G. Mikellides, Ira Katz, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2005-201: DEVELOPMENT OF MAGNETOPLASMADYNAMIC SOLAR WIND SIMULATOR FOR MAGSAIL EXPERIMENT; Yukio Shimizu, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), Sagamihara 229-8510, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, Koganei 184-8588, Japan; Ikkoh Funaki, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), Sagamihara 229-8510, Japan; Hidenori Kojima, Graduate School of Systems and Information Engineering, University of Tsukuba, Ibaraki, Japan; Hiroshi Yamakawa, Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), Sagamihara 229-8510, Japan

2005-203: ELECTROSTATIC AND ELECTROMAGNETIC ACCELERATION IN A LASER-ELECTRIC HYBRID THRUSTER; Hideyuki Horisawa and Koki Sasaki, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Akira Igari, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2005-205: FAST ION EMISSION CHARACTERISTICS OF A FORWARD LASER PLASMA ACCELERATOR FOR SPACE PROPULSION APPLICATIONS; Hideyuki Horisawa and Masaya Izumi, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Takehito Takeda, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2005-206: NUMERICAL SIMULATION OF A MW-CLASS SELF FIELD MAGNETOPLASMADYNAMIC THRUSTER USING THE MACH 2 CODE; Brian L. England and Pavlos G. Mikellides, Arizona State University, Tempe, AZ, 85283, United States of America

2005-207: DESIGN RULES FOR HIGH-PERFORMANCE FARAD THRUSTERS; Kurt A. Polzin and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Mechanical and Aerospace Engineering Department, Princeton University, Princeton, New Jersey 08544

2005-208: INVESTIGATION AND OPTIMIZATION OF AN INSTATIONARY MPD THRUSTER IN IRS; Anuscheh Nawaz, Monika Auweter-Kurtz, Georg Herdrich and Helmut L. Kurtz, University of Stuttgart, Institut fÃ¼r Raumfahrtsysteme, 70550 Stuttgart, Germany

2005-209: THE PPS 1350 QUALIFICATION DEMONSTRATION 7500H ON GROUND, ABOUT 5000H IN FLIGHT; FrÃ©dÃ©ric R. Marchandise, Joel Biron, Marc Gambon, and Nicolas Cornu, Snecma, Division Moteurs Spatiaux, Site de Villaroche Nord, 77552 Moissy-Cramayel, France; Frank Darnon, CNES, Avenue Edouard Belin, 31000 Toulouse, France; Denis Estublier, ESTEC, Keplerlaan 1, 22000 Noordwijk ZH, The Netherlands

2005-211: MISSION DESIGN FOR THE INNOVATIVE INTERSTELLAR EXPLORER VISION MISSION; Douglas I. Fiehler, QSS Group, Inc., - NASA Glenn Research Center, Cleveland, OH, 44135, USA; Ralph L. McNutt, Jr., Johns Hopkins University Applied Physics Laboratory, Laurel, MD, 20723, USA

2005-212: A 3.000 HOURS ENDURANCE TESTING OF RIT-22 THRUSTER IN THE NEW AEROSPAZIO TEST FACILITY; E. Bonelli, S. Scaranzin, F. Scortecci and F. Saito, AEROSPAZIO Tecnologie s.r.l., Rapolano Terne, Siena, 53040, Italy; R. Killinger, R. Kukies and H. Leiter, EADS Space Transportation, MÃ¶chmÃ¼hl, 74215, Germany

2005-213: THE THRUSTER MODULE ASSEMBLY (HALL EFFECT THRUSTER) DESIGN, QUALIFICATION AND FLIGHT; Joel Biron, Nicolas Cornu, Hubert Illand, and Marc Serrau, SNECMA, Division Moteurs Spatiaux, Site de Villaroche Nord, Direction Propulsion et Equipements Satellites, AÃ©rodrome de Melun-Villaroche, 77552 Moissy-Cramayel, France; Richard Rigollet, EADS ASTRIUM SAS, 31, rue des cosmonauts, 31402 Toulouse Cedex 4, France; Howard L. Gray, EADS ASTRIUM Ltd., Anchorage Road, Portsmouth, PO3 5PU, UK

2005-214: NUMERICAL SIMULATION OF THE INTERACTIONS BETWEEN SOLAR ARRAYS AND THE SURROUNDING PLASMA ENVIRONMENT; R. Sedmik, C. Scharlemanny, and M. Tajmarz, ARC Seibersdorf research Gmbh., Seibersdorf, A-2444, Austria; J. Gonzalez del Amox, A. Hilgers and D. Estublierk, ESA-ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands; G. Noci and M. Capacciyy, LABEN, Proel, Firenze, Italy; C. Koppelzz, Snecma Safran Group, Site de Villaroche Nord, BP No 93, 77552, Moissy Cramayel Cedex, France

2005-215: THRUST STAND FOR APPLIED-FIELD MPD THRUSTERS; James H. Gilland, Ohio Aerospace Institute, Brookpark, OH, 44142, USA; Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA, 30332, USA; Eric J. Pencil, NASA Glenn Research Center, Cleveland, OH 44135, USA

2005-219: ADEQUATE ELECTRIC PROPULSION SYSTEM PARAMETERS FOR PILOTED MARS MISSIONS; Tanja D. Schmidt, German Aerospace Center (DLR), Cologne, 51147, Germany; Monika Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme (IRS), UniversitÃ¤t Stuttgart, Stuttgart 70550, Germany

2005-221: SPECTRAL CHARACTERISTICS OF RADIATED EMISSION FROM SPT-100 HALL THRUSTERS; Edward J. Beiting, Michael L. Garrett, and James E. Pollard, The Aerospace Corporation, Los Angeles, CA 90009, USA; Bernard Pezet and Patrice Gouvermayre, 31, rue des Cosmonautes, 31402 Toulouse Cedex 4, France

2005-222: TEMPORAL CHARACTERISTICS OF RADIATED EMISSION FROM SPT-100 HALL THRUSTERS IN THE L, S, AND C BANDS; Edward J. Beiting, Michael L. Garrett, and James E. Pollard, The Aerospace Corporation, Los Angeles, CA 90009, USA; Bernard Pezet and Patrice Gouvernayre, 31, rue des Cosmonautes, 31402 Toulouse Cedex 4, France

2005-224: IN-FEEP CLUSTER FOR LISA PATHFINDER; N. Buldrini, A. Genovese, and M. Tajmal, ARC Seibersdorf Research, Seibersdorf A-2444, Austria

2005-226: MISSION ANALYSIS, SPACECRAFT CONCEPT AND ION THRUSTER DESIGN FOR A LOW-COST RENDEZVOUS WITH AND ASTEROID; David G. Fearn, EP Solutions, Fleet, Hampshire, GU52 6HS, UK

2005-227: ORBIT-RAISING, PAST AND PRESENT – THE X-SERIES OF SPACECRAFT AND ARTEMIS; David G. Fearn, EP Solutions, Fleet, Hampshire, GU52 6HS, UK

2005-228: COMBINED PLASMA AND THERMAL HOLLOW CATHODE INSERT MODEL; Ira Katz, James E. Polk, Ioannis G. Mikellides, Dan M. Goebel and Sarah E. Hornbeck, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2005-230: MAGNETIC NOZZLE DESIGN FOR HIGH-POWER MPD THRUSTERS; Robert P. Hoyt, Tethers Unlimited, Inc., Bothell, WA, 98011, USA

2005-231: PERFORMANCE IMPROVEMENT DUE TO KINK INSTABILITY SUPPRESSION IN MPD THRUSTERS; E. Martines, M. Zuin, M. Bagatin, r. Cavazzana, G. Serianni, and V. Antoni, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, corso Stati Uniti 4, 35127 Padova, Italy; P. Rossetti and M. Signori, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy; F. Paganucci and M. Andrenucci, Department of Aerospace Engineering, University of Pisa, via Caruso, 56122 Pisa, Italy

2005-232: MAGNETICALLY GUIDED LASER ABLATION FOR HIGH SPECIFIC IMPLUSE THRUSTERS; Sohail H. Zaidi, Thomas W. Smith, Robert Murray, and Richard B. Miles, Princeton University, Princeton, NJ 08540, USA

2005-233: FEASIBILITY STUDY ON HIGH SPECIFIC IMPULSE ION THRUSTER WITH C/C GRID SYSTEM; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 329-8686, Japan; Ikkoh Funaki and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2005-234: STUDY ON PULSED PLASMA THRUSTER CONFIGURATION TO EXPAND IMPULSE BIT RANGE; Junji Uezu and Junpei Lio, Tokyo Metropolitan Institute of Technology (presently, Tokyo Metropolitan Univeristy), Asahigaoka 6-6, Hino, Tokyo, 191-0065, Japan; Yukiya Kamishima and Haruki Takegahara, Tokyo Metropolitan University, Asahigaoka 6-6, Hino, Tokyo, 191-0065, Japan; Takashi Wakizono, HI-SERVE Corporation, Totohara 780-7, Akiruno, Tokyo, 190-0152, Japan; Mitsuteru Sugiki, Astro Research Corporation, Godo-cho 134, Hodogaya-ku, Yokohama, Kanagawa, 240-0005, Japan

2005-235: DIRECT THRUST MEASUREMENT OF IN-FEEP CLUSTERS; K. Marhold and M. Tajmar, ARC Seibersdorf research GmbH, A-2444 Seibersdorf, Austria

2005-236: EVALUATION ON IMPULSE BIT CHARACTERISTICS OF PULSED PLASMA THRUSTER BY SINGLE IMPULSE MEASUREMENT; Junpei Lio, Junji Uezu, and Tadanori Fukushima, Tokyo Metropolitan Institute of Technology (presently Tokyo Metropolitan University), Japan; Yukiya Kamishima and Haruki Takegahara, Toyko Metropolitan University, Japan

2005-238: AN OVERVIEW OF THE VHITAL PROGRAM: A TWO-STAGE BISMUTH FED VERY HIGH SPECIFIC IMPULSE THRUSTER WITH ANODE LAYER; Anita Sengupta and Colleen Marrese-Reading, Jet Propulsion Laboratory, Pasadena, CA, 91109, US; Mark Cappelli and David Scharfe, Stanford University, Stanford, CA, 94305, US; Sergey Tverdokhlebov, Sasha Semenkin, and Oleg Tverdokhlebov, TsNIIMASH Export, Moscow, Russia; Ian Boyd and Michael Keidar, University of Michigan, Ann Arbor, MI, 48109, US; Azer Yalin and Vijaya Surla, Colorado State University, Fort Collins, CO, 80523, US; Tom Markusic and Kurt Polzin, NASA Marshall Space Flight Center, Huntsville, AL, US

2005-244: GRID GAP MEASUREMENT FOR AN NSTAR ION THRUSTER; Esther M. Diaz and George C. Soulas, National Aeronautics and Space Administration, Cleveland, OH, 44135, United States

2005-245: SMART-1 ELECTRIC PROPULSION OPERATIONAL EXPERIENCE; D. Milligan, D. Gestal, O. Camino, and P. Pardo-Voss, European Space Operations Centre, Robert Bosch Str. 5, 64293, Darmstadt, Germany; D. Estublier, ESA/ESTEC, Kepleraan 1, Noordwijk, The Netherlands; C. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux, Villaroche Nord, France

2005-246: OPERATIONALLY ENHANCED ELECTRIC PROPULSION PERFORMANCE ON ELECTRICALLY PROPELLED SPACECRAFT; D. Milligan, D. Gestal, O. Camino, and P. Bearman, European Space Operations Centre, Robert Bosch Str. 5, 64293, Darnstadt, Germany; C. Koppel, Snecma Moteurs, Division Moteurs-Spatiaux, Villaroche Nord, France

2005-248: CALCULATION OF THERMALLY-INDUCED DISPLACEMENTS IN SPHERICALLY DOMED ION ENGINE GRIDS; George C. Soulas, NASA Glenn Research Center, Cleveland, OH 44135, USA

2005-252: PERFORMANCE MAPPING OF NEW GN-RITS AT GIESSEN, D. Feili, H. W. Loeb, K. H. Schartner, St. Weis, D. Kirmse, and B. K. Meyer, Electric Propulsion, Giessen University, Giessen, D-35390, Germany; R. Kilinger and H. Mueller, EADS-ST, Moekuehl, D-74215, Germany; Davina Mafia Di Cara, ESA/ESTEC – Electric Propulsion Section, Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands

2005-256: PROGRESS ON THE DEVELOPMENT OF A DIRECT EVAPORATION BISMUTH HALL THRUSTER; Dean R. Massey and Lyon B. King, Michigan Technological University Ion Space Propulsion Lab Houghton, MI 49931, United States of America

2005-257: THRUST CHARACTERIZATION OF A T6 HOLLOW CATHODE; Paolo Gessini and Stephen B. Gabriel, University of Southampton, Southampton, Hants, SO17 1BJ, United Kingdom; David G. Fearn, EP Solutions, Fleet, Hants, GU14 0LX, United Kingdom

2005-258: A (RE-) EXAMINATION OF ELECTRON MOTION IN HALL THRUSTER FIELDS; Lyon B. King, Michigan Technological University, Houghton, Michigan, 49931, USA

2005-260: PRELININARY WEAR ANALYSIS FOLLOWING A 2000 H WEAR TEST OF THE HIPEP ION THRUSTER; George J. Williams Jr., The Ohio Aerospace Institute, Cleveland, OH, 44135, USA; Tyler A. Hickman, Thomas W. Haag, John E. Foster, and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2005-265: VACUUM TESTING OF THE MINIATURE RADIO-FREQUENCY ION THRUSTER; Valerie F. Mistoco, Thomas A. Trudel, Sven G. Bilen and Michael M. Micci, The Pennsylvania State University, University Park, PA, 16802 USA

2005-266: ENERGETIC ION PRODUCTION AND KEEPER EROSION IN HOLLOW CATHODE DISCHARGES; Dan M. Goebel, Kristina Jameson, Ira Katz, and Ioannis G. Mikellides, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2005-269: HOLLOW CATHODE AND THRUSTER DISCHARGE CHAMBER PLASMA MEASUREMENTS USING HIGH-SPEED SCANNING PROBES; Kristina K. Jameson, Dan M. Goebel, and Ron M. Watkins, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2005-270: MODELING ION BEAM NEUTRALIZATION AND NEAR-THRUSTER PLUME INTERACTIONS; Lubos Brieda and Douglas VanGilder, Air Force Research Laboratory, Edwards AFB, CA 93524; Joseph Wang, Virginia Polytechnic Institute and State University, Blacksburg, VA, 24061-0203

2005-271: ION PROPULSION SIMULATIONS USING PARALLEL SUPERCOMPUTER; J. Wang, Y. Cao, R. Kafafy, and J. Pierru, Virginia Polytechnic Institute and State University, Blacksburg, VA, 24061, USA; V. Decyk, University of California, Los Angles, CA 90095, USA

2005-272: HIGH POWER ECR ION THRUSTER DISCHARGE CHARACTERIZATION; John E. Foster, Hani Kamhawi, Tom Haag, Christian Carpenter, and George Williams, NASA Glenn Research Center, Cleveland, OH, 44135

2005-274: ELETRON DYNAMICS OF A NON-NEUTRAL ELECTRON PLASMA IN THE DEFINING FIELDS OF A HALL-EFFECT THRUSTER; Emily C. Fossum, Lyon B. King, and Jerry L. Ross, Michigan Technological University, Houghton, MI, 49931, U.S.A.

2005-275: ARCJET STAGE INVESTIGATION AND INDUCTIVE HYDROGEN HEATING IN THE TIHTUS ENGINE; Hannah BÃ¶hrk, Dejan Petkow, Georg Herdrich, Monika Auweter-Kurtz, and Helmut Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2005-276: COMPACT HIGH VOLTAGE POWER PROCESSING FOR FIELD EMISSION ELECTRIC PROPULSION (FEEP); Matthias Gollor, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany and Fachhochschule Konstanz – University of Applied Science – Dept. of Electrical Engineering, 78462 Konstanz, Brauneggerstr. 55D, Germany; Klaus Breier, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany

2005-277: HOLLOW CATHODES STUDY AT ALTA-CENTROSPAZIO; P. Rossetti and M. Signori, Alta SpA-Centrospazio, Pisa, I-56121, Italy; M. Andrenucci and F. Paganucci, University of Pisa, Pisa, I-56100 Italy

2005-278: GENERIC HIGH VOLTAGE POWER MODULE FOR ELECTRICAL PROPULSION; Michael Boss, Frank Herty, and Kurt Rogalla, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany; Matthias Gollo, EADS Astrium, Electronics Division, 88039 Friedrichshafen, Germany and Fachhochschule Konstanz – University of Applied Science – Dept. of Electrical Engineering, 78462 Konstanz, Brauneggerstr. 55D, Germany

2005-281: RESULTS OF A 2000-HOUR WEAR TEST OF THE NEXIS ION ENGINE; John Steven Snyder, Dan M. Goebel, James E. Polk, Analyn C. Schneider, and Anita Sengupta, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2005-282: PERFORMANCE EVALUATION OF A HIGH ENERGY PULSED PLASMA THRUSTER II; Hani Kamhawi, NASA Glenn Research Center at Lewis Field, Cleveland, Ohio, 44135; Lynn Arrington, QSS Group, Cleveland, Ohio, 44135; Eric Pencil and Thomas Haag, NASA Glenn Research Center at Lewis Field, Cleveland, Ohio, 44135

2005-283: INVESTIGATION OF VARIOUS MICROWAVE ELECTRON CYCLOTRON RESONANCE CATHODE CONFIGURATIONS; Hani Kamkawi, and John E. Foster, NASA Glenn Research Center, Cleveland, Ohio 44135

2005-284: INVESTIGATION OF VARIOUS MICROWAVE ELECTRON CYCLOTRON RESONANCE CATHODE CONFIGURATIONS; Hani Kamhawi and John E. Foster, NASA Glenn Research Center, Cleveland, Ohio 44135

2005-285: NEXT MULTI ION ENGINE TEST: PLUME MODELING AND TEST PLANS; Myron J. Mandell, Science Applications International Corporation, San Diego, CA

2005-287: SPECTROSCOPIC INVESTIGATION OF THE STEADY STATE CHARACTERISTICS OF HOLLOW CATHODE INTERNAL PLASMAS; S. J. Pottinger and S. B. Gabriely, University of Southampton, Higheld, Hampshire, SO17 1BJ, United Kingdom

2005-289: MEASUREMENTS OF ION ENERGIZATION BY A PAIR OF BEATING ELECTROSTATIC ION CYCLOTRON WAVES; R. Spektorand and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDyL), Princeton University, Princeton, New Jersey 08544

2005-290: HELICON DOUBLE LAYER THRUSTERS; C. Charles, P. Alexander, C. Costa, O. Sutherland, R. W. Boswell, Plasma Research Laboratory, RSPHYSSE, The Australian National University, Canberra, ACT 0200, Australia; L. Pfitzner and R. Franzen, AUSPACE, Canberra, Australia; J. Kingwell and A. Parfitt, Cooperative Research Centre (CRC) for Satellites Systems, Canberra, Australia; P.E. Frigot, J. Gonzalez del Amo, E. Gengembre, and G. Saccoccia, Propulsion and Aerothermodynamics Division, European Space Agency, ESTEC, The European Space Agency, The Netherlands

2005-292: NUMERICAL SIMULATIONS DEVELOPED AT ALCATEL ALENIA SPACE FOR ELECTRIC PROPULSION EFFECTS ON SATELLITE; Sylvie Brosse, SÃ©bastien Clerc, and VÃ©ronique Perrin, Alcatel Alenia Space, 100 Bd Du MIDI, 06156 Cannes La Bocca, France

2005-293: DIFFERENTIAL SPUTTERING YIELDS OF REFRACTORY METALS BY XENON, KRYPTON, AND ARGON ION BOMBARDMENT AT NORMAL AND OBLIQUE INCIDENCES; Kirk A. Zoerb, John D. Williams, Desiree D. Williams, and Azer P. Yalin, Colorado State University, Fort Collins, CO, 80523, USA

2005-294: DIRECT AND REMOTE MEASUREMENTS OF PLASMA PROPERTIES NEARBY HOLLOW CATHODES; Russell H. Martin, Casey C. Farnell, and John Williams, Dept. of Mechanical Engineering, Colorado State University, Fort Collins, Colorado 80523

2005-295: ELECTROMAGNETIC PUMPS FOR CONDUCTIVE-PROPELLANT FEED SYSTEMS; Thomas E. Markusic, Kurt A. Polzin, and Amado Dehoyos, Propulsion Research Center, NASA – Marshall Space Flight Center, Huntsville, Alabama 35812

2005-296: MULTI-MEGAWATT PROPULSION BASED ON A COMPACT TOROID THRUSTER; John Slough, University of Washington, Seattle, WA, 98195, USA

2005-297: DEVELOPMENT & TEST STATUS OF THE THALES HIGH EFFICIENCY MULTISTAGE PLASMA (HEMP) THRUSTER FAMILY; N. Koch, H.-P. Harmann and G. Kornfeld, THALES Electron Devices GmbH, SÃ¶flingerstr. 100, 89073 Ulm, Germany

2005-298: DEVELOPMENT & TEST STATUS OF THE THALES W/OS MIXED METAL METRIX HOLLOW CATHODE NEUTRALISER HKN5000 G. Kornfeld, N. Koch, and H. –P. Harmann, THALES Electron Devices GmbH, SÃ¶flingerstr. 100, 89077 Ulm, Germany

2005-299: EROSION MEASUREMENTS BY CAVITY RING-DOWN SPECTROSCOPY FOR THE VHITAL PROGRAM; Azer P. Yalin Vijaya Surla, and John D. Williams, Colorado State University, Fort Collins, Colorado, 80523

2005-300: DETERMINATION OF NUMBER DENSITY AND VELOCITY OF SPUTTERED PARTICLES BY CAVITY RING-DOWN SPECTROSCOPY; Azer P. Yalin and Vijaya Surla, Colorado State University, Fort Collins, Colorado, 80523

2005-301: NONAMBIPOLAR ELECTRON SOURCE FOR NEUTRALIZATION OF ION AND HALL THRUSTERS; Ben W. Longmier and Noah Hershkowitz, University of Wisconsin – Madison, Madison, WI 53706, US

2005-302: CHARACTERIZATION OF COLLOID THRUSTER BEAMS; M. Gamero-CastaÃ±o and J. Ziemer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91108, USA

2005-303: ESTIMATION OF HALL THRUSTER EROSION USING HPHALL; M. Gamero-CastaÃ±o and I. Katz, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91108, USA

2005-304: THRUUST IMPROVEMENT OF THE MAGNETICALLY ENHANCED VACUUM ARC THRUSTER (MVAT); Benjamin Tang, Luke Idzkowski, Michael Au, Don Parks, and Mahadevan Krishnan, Alameda Applied Sciences Corporation, San Leandro, CA, 94577, USA; John Ziemer, NASA Jet Propulsion Laboratory, Pasadena, CA, 91109, USA

2005-306: TESTING OF THE NASA GSFC MEMS COLLOIDAL THRUSTER; Eric H. Cardiff, Brad Degen, Abraham Grindle, Brian Jamieson, Loral O’Hara, Kevin Pearce, and Patrick Roman, NASA Goddard Space Flight Center, Greenbelt, MD, 20771, USA

2005-309: TEMPORAL BEHAVIOR OF THE ION VELOCITY DISTRIBUTION FUNCTIONS IN PULSED HELICON PLASMA SOURCES; Costel Biloiu, Xuan Sun, and Earl Scimej, West Virginia University, Morgantown, West Virginia 26506, USA; Edgar Choueiri and Rostislav Spektor, Department of Mechanical and Aerospace Engineering, Princeton University Princeton, New Jersey, 08544, USA

2005-310: LASER PROPULSION FOR GROUND TO ORBIT LAUNCH; David P. Resendes, SÃ©rgio Mota and JosÃ© T. Mendonca, Instituto Superior TÃ©cnico, Lisboa, Portugal; Berry Sanders, TNO Prins Maurits Laboratory Rijswijk, The Netherlands; JoÃ¤o EncarnocÃ¤o, T. U. Delft, Delft, The Netherlands; Jose Gonzalez del Amo, European Space Agency, ESTEC

2005-314: HOLLOW CATHODE IGNITION STUDIES AND MODEL DEVELOPMENT; William G. Tighe and Kuei-Ru Chien, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109; Robert T. Longo, Private Consultant, Arcadia, CA 91007

2005-315: L-C COMMUNICATIONS ETI ELECTRIC PROPULSION OVERVIEW; Kuei-Ru Chien, Stephen L. Hart, William G. Tighe, Michael K De Pano, Thomas A. Bond, and Rafael Spears, L-3 Commmunications Electron Technologies, Inc., 3100 W. Lomita Blvd., Torrance, California 90509, USA

2005-316: INVESTIGATION AND DEVELOPMENT OF A HIGH VOLTAGE PROPELLANT ISOLATOR FOR ION THRUSTERS; Stephen L. Hart, William Tighe, and Charles Pearce, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109

2005-318: A 25NH LOW-NOISE THRUST STAND FOR MICROTHRUSTERS; Claude R. Phipps and James R. Luke, Photonic Associates, LLC, Santa Fe, NM 87508; Wesley D. Helgeson, NMT/IERA, Albuquerque, NM 87106

2005-320: A SOLAR ELECTRIC PROPULSION CARGO VEHICLE TO SUPPORT NASA LUNAR EXPLORATION PROGRAM; Ronald Spores and Jeff Monheiser, Aerojet Corporation, Redmond, WA 98073; Brian P. Dempsey, Darren Wade, and Kenneth Creel, Lockheed Martin, Denver, CO 80201; David Jacobson, NASA Glenn Research Center, Cleveland, OH 44135; Geoff Drummond, Colorado Power Electronics, Inc. Fort Collins, CO 80524

2005-321: CHARATERIZATION OF A HIGH CURRENT, LONG LIFE HOLLOW CATHODE; Jonathan L. Van Noord, Hani Kamhawi and Heather K. McEwen, NASA Glenn Research Center, Cleveland, OH, 44135

2005-323: AMBITIOUS CHALLENGES OF JAPANESE ELECTRIC PROPULSION; Hitoshi Kuninaka, ISAS/JAXA, Yoshinodai, Sagamihara, Kanagawa, Japan

2005-324: CHARACTERIZATION OF A HIGH SPECIFIC IMPULSE XENON HALL EFFECT THRUSTER; James J. Szabo, Busek Co. Inc., Natick, MA, 01760, USA; Yassir Azziz, MIT, Cambridge, MA, 02139, USA

2005 FILE DIRECTORY

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2007 INDEX

2007-001: CALCULATING SPUTTER RATE ANGULAR DEPENDENCE USING OPTICAL PROFILOMETRY; Alexander C. Barrie and Bryan S. Taylor, Advatech Pacific, Inc., Palmdale, CA, 93550, United States; Jared M. Ekholm and William H. Hargus, Air Force Research Laboratory, 1 Ara Rd., Edwards AFB, CA, United States

2007-002: NUMERICAL PROCEDURE PERMITTING CALCULATION OF HOW A VACUUM CHAMBER INFLUENCES ELECTRIC PROPULSION THRUSTER JET EXPANSION; Grigory Toropov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia; Vladimir Chervakov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2007-004: A 3D BOUNDARY SHEATH ANALYSIS ON FARADAY PROBE MEASUREMENTS IN A NON-EQUILIBRIUM PLASMA; Grigory Toropov, Moscow Aviation Institute (State Technical University) MAI, Engineering Plasma Computational Laboratory (EPCLab), 24b-I20, Zalineynaya str., Vologda, 160010, Russia

2007-005: SUMMARY OF THE VHITAL THRUSTER TECHNOLOGY DEMONSTRATION PROGRAM: A TWO-STAGE BISMUTH-FED VERY HIGH SPECIFIC IMPULSE TAL; Anita Sengupta and Colleen Marrese-Reading; Jet Propulsion Laboratory, Pasadena, CA, 91109, US; Alexander Semenkin, Leonid Zakharenkov, Sergey Tverdokhlebov, and Oleg Tverdokhlebov, TsNIIMASH Export, Moscow-Region, Russia; Kurt Polzin and Tom Markusic, NASA Marshall Space Flight Center, Huntsville, AL, US; Marck Cappelli and David Scharfe, Stanford University, Stanford, CA, 94305, US; Ian Boyd and Michael Keidar, University of Michigan, Ann Arbor, MI, 48109, US; Azer Yalin and Vijaya Surla, Colorado State University, Fort Collins, CO, 80523, US

2007-006: PLASMA PARAMETERS INVESTIGATION IN THE NEAR CATHODE ZONE OF THE SPT DISCHARGE; Sergey A. Khartov and Igor P. Nazarenko, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia; Andrey A. Pereslavtsev, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia

2007-007: SPUTTERING PROCESS OF BN BASED CERAMIC BY THE FLOWS OF NONCOMPENSATIED CHARGE PLASMA; Elvira N. Nikiporetz and Alexander A. Semenov, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia; Igor I. Shkarban, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia; Elena S. Khartova, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia

2007-008: ELECTRON-ENHANCED DESORPTION INFLUENCE ON THE SPT ISOLATOR WALL EROISION PROCESSES; Sergey S. Elovikov, Moscow State University, (MGU) Moscow, Russia; Sergey A. Khartov, Moscow Aviation Institute (State University of Aerospace Technologies) MAI, Moscow, Russia

2007-009: RE-IGNITION OF MICROWAVE DISCHARGE ION ENGINES ON HAYABUSA FOR HOMEWARD JOURNEY; Hitoshi Kuninaka, Kazutaka Nishiyama, Yukio Shimizu, Tetsuya Yamada, Ikko Funaki, Satoshi Hosoda, and Hiroyuki Koizumi, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229, Japan

2007-010: SENSITIVITY TESTING OF THE NSTAR ION THRUSTER; Anita Sengupta, John Anderson, and John Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, US

2007-011: A STUDY OF SOME PHYSICAL PROCESSES IN HALL THRUSTER OPERATED IN THE DISCHARGE VOLTAGE UP TO 1000 V; Oghienko (Ogiienko) Sergii, Bilokon Volodymyr, and Oransky Anatoliy, Zhukovski National airspace university “Kharkov Aviation institute”, Ukraine; Bober Alexander, Asher Space Research Institute, TECHNION-Israeli Institute of technology, Israel

2007-012: SEVEN YEARS OF HALL THRUSTER MODELING: AN EUROPEAN COLLABORATION BETWEEN BARI AND GREIFSWALD; F. Taccogna, S. Longo, and M. Capitelli, Dip, Di Chimica, UniversitÃ¡ degli Studi di Bari & IMIP-CNR, Sect. Bari, via Orabona 4, Bari, I-70126, Italy; R. Schneider, Max-Planck Institute fÃ¼r Plasmaphysik, EURATOME Association, Wendelsteinstr. 1, Greifswald, D-17491, Germany

2007-014: INITIATION OF THE NUMERICAL INVESTIGATION OF THE HYBRID PLASMA THRUSTER TIHTUS; Uwe Bauder, Markus Fertig, Hannah BÃ¶hrk, Georg Herdrich, and Dejan Petkow, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, 70550 Stuttgart, Germany; Monika Auweter-Kurtz, UniversitÃ¤t Hamburg, 20146 Hamburg, Germany

2007-015: PLASMA SAIL PROPULSION BASED ON THE PLASMA MAGNET; John Slough, University of Washington, Seattle, WA, 98195, USA

2007-016: MAGNETICALLY ACCELERATED PLASMOID (MAP) THRUSTER – INITIAL RESULTS AND FUTURE PLANS; John Slough, Arthur Blair, Chris Pihl, and George Votroubek, MSNW, Redmond, WA 98052, USA

2007-017: PLASMA HEATING OF INERT GAS HOLLOW CATHODE INSERTS; Ira Katz, Ioannis G. Mikellides, Dan M. Goebel, and James E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2007-018: NUMERICAL SIMULATIONS OF A HALL THRUSTER HOLLOW CATHODE PLASMA; Ioannis G. Mikellides, Ira Katz, Kristina K. Jameson, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2007-019: MICRO-NEWTON RIT POWER CONTROL UNIT DEVELOPMENT; Matthias Gollor, Professor, University of Applied Science Konstanz – Electrical Engineering; Michael Boss, Rafael Braeg, Andreas Franke, Frank Herty, and Bernhard Kiewe, Astrium GmbH – Friedrichshafen – Germany, Dept. Electronics Equipment Germany – ASE2

2007-020: ELECTRIC PROPULSION ELECTRONICS ACTIVITIES IN ASTRIUM GERMANY; Matthias Gollor, Professor, University of Applied Science Konstanz (Germany) – Electrical Engineering; Michael Boss, Astrium GmbH – Friedrichshafen – Germany, Dept. Electronics Equipment Germany – ASE2

2007-021: GENERIC HIGH VOLTAGE POWER SUPPLIES (HVPS) WITH OPTIMUM EFFICIENCY AND MULTI-RANGE; Matthias Gollor, Professor, University of Applied Science Konstanz (Germany) – Electrical Engineering; Michael Boss, Frank Herty, and Bernhand Kiewe, Astrium GmbH – Friedrichshafen – Germany, Dept. of Electronics Equipment Germany – ASE2

2007-023: HOLLOW CATHODE EMISSION AND IGNITION STUDIES AT L-3 ETI; William G. Tighe and Kuei-Ru Chien, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109; Robert T. Longo, Private Consultant, Arcadia, CA, 91007

2007-024: ION THRUSTER DEVELOPMENT AT L-3 ETI FOR SMALL SATELLITE APPLICATIONS; William G. Tighe, Kuei-Ru Chien, and Rafael Spears, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505; Dan M. Goebel, Jet Propulsion Laboratory, Pasadena, CA, 91109

2007-025: TWO-DIMENSIONAL CHARACTERIZATION OF MICROWAVE E-FIELDS AND BEAM PROFILES OF THE ECR ION THRUSTER Âµ20; Kazutaka Nishiyama and Hitoshi Kuninaka, Japan Aerospace Exploration Agency / Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 229-8510, Japan; Tatsuya Nakai, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan

2007-026: INVESTIGATION OF INTEGRAL CHARACTERISTICS OF THE LOW POWER HALL THRUSTER FOR THE SPACECRAFT ORIENTATION PROPULSION SYSTEM DURING TRANSITION TO THE STATIONARY OPERATION MODE AFTER THRUSTER START UP; Oghienko (Ogiienko) Sergii, Zhukovksy National Aerospace University “Kharkov Aviation Institute”, Ukraine

2007-027: IN-SPACE PROPULSION INFLUENCES ON COMSAT MISSIONS; David C. Byers, Las Vegas, NV, 89103, U.S.A.; John W. Dankanich, Gray Research Inc., Cleveland, OH, 44135, U.S.A.

2007-029: NUMERICAL ANALYSIS AND EXPERIMENTS OF A MICROWAVE-EXCITED MICROPLASMA THRUSTER; Takeshi Takahashi, Yoshinori Takao, Koji Eriguchi and Kouichi Ono, Graduate School of Engineering, Kyoto University, Kyoto, 606-8501, Japan

2007-030: SPACECRAFT MOTION AND ATTITUDE CONTROL IN THE HIGH ELLIPTIC ORBIT; V.A. Obukhov, A. I. Pokryshkin, and G. A. Popov, Leningradskoe shosse, 5, 125080 Moscow, Russia; N. V. Yashina, Volokolamskoe shosse, 4. 125871, Moscow, Russia

2007-031: INVESTIGATION OF HIGH-ENERGY IONS WITH HIGH-ANGLE TRAJECTORIES IN HALL THRUSTERS PLUMES; Regina M. Sullivan, California Institute of Technology, Pasadena, CA, 91125, U.S.A.; Paul A. Torrey, Cornell University, Ithaca, NY, 14853, U.S.A.; Lee K. Johnson, Jet Propulsion Laboratory, Pasadenca, CA, 91109, U.S.A.

2007-032: MEASUREMENT OF MAGNETIC DETACHMENT EFFECTS IN A MAGNETIC NOZZLE; Christopher Deline and Brian Gilchrist, University of Michigan, Ann Arbor, MI, 48109; Jared Squire, Ad Astra Rocket Company, Houston, TX, 77058; Jonathan Jones, Greg Chavers, and Chris Dobson, NASA Marshall S pace Flight Center, Huntsville, AL 35805; Roger Bengston, University of Texas, Austin, TX 78712

2007-033: NEXT LONG-DURATION TEST AFTER 11, 570 H AND 237 KG OF XENON PROCESSED; Daniel A. Herman, ASRC Aerospace Corporation, Cleveland, OH, 44135, USA; George C. Soulas and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2007-034: HALL THRUSTER EROSION PREDICTION USING A HYDRODYNAMIC PLASMA MODEL AND SPUTTERING SIMULATION; John T. Yim and Iain D. Boyd, University of Michigan, Ann Arbor, MI, 48109, USA; Michael Keidar, George Washington University, Wasghington, DC, 20052, USA

2007-035: A SIMPLE ELECTRIC THRUSTER BASED ON ION CHARGE EXCHANGE; Joe Khachan and Lachlan Blackhall, University of Sydney, Sydney, NSW, 2006, Australia

2007-036: LONGE RANGE PARTICLE COLLISIONS FOR THE PIC/DSMC SIMULATION CODE PICLAS; Danilo D’Andrea and Rudolf Schneider, Forschungszentrum Karlsruhe – in der Helmholtz-Gemeinschaft, Institut fÃ¼r Hochleistungsimpuls und Mikrowellentechnik, D-76021 Karlsruhe, Germany, Partner of Karlsruhe Institute of Technology; Martin Quandt and Claus-Dieter Munz, Institut fÃ¼r Aerodynamik und Gasdynamik, UniversitÃ¤t Stuttgart, D-70550 Stuttgart Germany; Sabine Roller, HÃ¶chstleistungsrechenzentrum Stuttgart, D-70550 Stuttgart, Germany; Markus Fertig, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, D-70550 Stuttgart, Germany

2007-037: A3D MODEL FOR MFD FLOW SIMULATION; Francesc Battista, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Tommaso Misuri, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Giuliano Ranuzzi, Ph.D, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy; Mariano Andrenucci, Professor, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ de Pisa, Pisa, 56122, Italy, Chairman and CEO, ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-038: REVIEW OF HALL THRUSTER NEUTRAL FLOW DYNAMICS; Bryan M. Reid and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48105, USA

2007-039: DIVERGING CUSPED-FIELD HALL THRUSTER (DCHT); Daniel G. Courtney and Manuel MartÃnez-SÃ¡chez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139

2007-041: HIGH DENSITY MAGNETIZED TOROID FORMATION AND TRANSLATION WITHIN XOCOT: AN ANNULAR FIELD REVERSED CONFIGURATION PLASMA CONCEPT; David Kirtley and Dr. Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109; Dr. James Haas and Michael Reilly, Air Force Research Laboratory, Edwards AFB, CA 93524

2007-042: A HIGH ORDER RELATIVISTIC PARTICLE PUSH METHOD FOR PIC SIMULATIONS; Martin Quandt and Claus-Dieter Munz, Institut FÃ¼r Hochleistungsimpuls und Mikrowellentechnik, Forschungszentrum Karlsruhe, Germany; Rudolf Schneider, Institut FÃ¼r Hochleistungsimpuls und Mikrowellentechnik, Forshungszentrum Karlsruhe, Germany

2007-043: FEASIBILITY STUDY ON VISUALIZED ION THRUSTER; Yoshinori Nakayama and Yasuhiro Teraura, National Defense Academy of Japan, Yokosuka, Kanagawa, 239-8686, Japan

2007-044: MATHEMATICAL MODEL AND CALCULATION METHOD FOR HOLLOW CATHODES LIFETIME FORECAST; Sergey Yu. Nesterenko and Anatoliy I. Oranskiy

2007-045: EXPERIMENTAL STUDY OF HETEROGENEITY IN AN AZIMUTHAL DIRECTION OF HALL THRUSTER PLASMA FLOW; Oghienko (Ogiienko) Sergii, Bilokon Volodymyr, and Setrakova Yana, Zhukovsky National Aerospace University “Kharkov Aviation Institute,” Ukraine

2007-046: DISTRIBUTION OF UNIONIZED PROPELLANT XENON IN A HALL THRUSTER PLUME; Makoto Matsui, Shigeru Yokota, Daichi Sakoh, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2007-048: SEP-SAMPLE RETURN FROM A MAIN BELT ASTEROID; Horst W. Loeb and Karl-Heinz Schartner, Heinrich-Buff-Ring 16, Giessen, D-35394, Germany; Bernd Bachwald, WeÃŸling-Oberpfaffenhofen, D-82234, Germany; Wolfgang Seboldt, Linder HÃ¶he, Porz-Wahnheide, D-51147, Germany

2007-049: THE PLASMA PLUME OF THE ISS PLASMA CONTACTOR UNIT UNDER THE EFFECT OF THE GEOMAGNETIF FIELD; F. F. Gabdullin, A. G. Korsun, E. G. Lavrenko, A. S. Mitroshin, and E. M. Tverdokhlebova, Central Research Institute of Machine Building (TSNIIMASH), Korolev, Moscow region, 141070, Russia

2007-050: THE DESIGN AND OPERATION OF BEAM DIAGNOSTICS FOR THE DUAL STAGE 4-GRID ION THRUSTER; Cristina Bramanti, ESA-ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands; David G. Fearn, EP Solutions, 23 Bownhurst Road, Church Crookham, Fleet, Hants, GU52 6HS, United Kingdom

2007-051: EFFECT OF A MAGNETIC FIELD IN SIMULATING THE PLUME-FIELD OF AN ANODE LAYER HALL THRUSTER; Yongjun Choi, University of Michigan, Ann Arbor, MI 48109; Michhael Keidar, The George Washington University, Washington DC 20052; Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109

2007-052: ELECTRON KINETIC EFFECTS AND BEAM-RELATED INSTABILITIES IN HALL THRUSTERS; I. D. Kaganovich and Y. Raitses, Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA; D. Sydorenko, Department of Physics, University of Alberta, Edmonton, Alberta T6G 2G7, Canada

2007-053: ADVANCES IN RADIATION-TOLERANT SOLAR ARRAYS FOR SEP MISSIONS; Henry W. Brandhorst, Jr., Steve R. Best, and Julie A. Rodiek, Space Research Institute, Auburn University, AL, 36849, U.S.A.; Mark J. O’Neill, ENTECH, Inc., Keller, TX, 76248, U.S.A.; Michael I. Eskenazi, ATK-Space, Inc., Goleta, CA, 93117, U.S.A.; Dale C. Ferguson, NASA Marshall Space Flight Center, Huntsville, AL, 35812, U.S.A

2007-055: MICRO-PLASMAJET ARRAY: NUMERICAL SIMULATION ON THRUST IMPROVEMENT OF MULTI-JET EFFECT; Fujimi Sawada, Hideyuki Horisawa, Kosuke Onodera, and Atushi Koshiyama, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-056: THRUST PERFORMANCE OF ELECTROMAGNETIC ACCELERATION MODE FOR LASER-ELECTRIC HYBRID THRUSTERS; Yusuke Sasaki and Hideyuki Horisawa, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Ikkou Funaki, Japan Aerospace Exploration Agency, 3-1-1 Sagamihara, Kanagawa, 229-8510, Japan; Itsuro Kimura, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-057: ON SUPERSONIC HYDROGEN HEATING: THE TIHTUS ENGINE; Hannah BÃ¶hrk and Monika Auweter-Kurtz, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70550 Stuttgart, Germany

2007-058: RECTANGULAR LASER-ELECTROMAGNETIC HYBRID PULSED PLASMA THRUSTER; Tomohiro Ayabe and Hideyuki Horisawa, Tokai University, Hiratsuka-shhi, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Itsuro Kimura, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-060: PLASMA PROPULSION SYSTEM FUNCTIONAL CHAIN FIRST THREE YEARS IN ORBIT ON EUROSTAR 3000; Astrium Satellites, 31 rue des Cosmonautes, 31402 Toulouse Cedex 4, France; Dr. Howard L. Gray, Astrium Satellites, Anchorage Road, Portsmouth, Hampshire PO3 5PU, United Kingdom

2007-061: LABORATORY EXPERIMENT OF MAGNETOPLASMA SAIL, PART 1: PURE MAGNETIC SAIL; K. Ueno, t. Kimura, and T. Ayabe, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; H. Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; and H. Yamakawa, Kyoto University, Uji, Kyoto, 611-0011, Japan

2007-062: RUSSIAN FLIGHT HALL THRUSTERS SPT-70 & SPT-100 AFTER CATHODE CHANGE START DURING 20-25 MS; Vjacheslav M. Murashko, Aleksandr I. Koryakin, Aleksandr N. Nesterenko, and Sergey V. Olotin, Fakel Experimental Design Bureau, Kaliningrad, Russia; Anatoliy I. Oranskiy, Andriy V. Loyan, Mikola M. Koshelev, Volodimir I. Bilokon, and Sergiy Yu. Nesterenko, Science & Technology Center of Space Power & Engines of National Aerospace University “Kharkiv Aviation Institute” (STC SPE KhAI), Kharkiv, Ukraine

2007-066: ADVANCES ON A HALL THRUSTER HYBRID CODE; I. Maqueda, D. Escobar, and E. Ahedo, Universidad PolitÃ©cnica de Madrid, Madrid 28040, Spain

2007-067: SIMULATION OF WALL EROSION IN HALL THRUSTERS; E. Ahedo and A. AntÃ³n, Universidad PolitÃ©cnica de Madrid, Madrid 28040, Spain; I. Garmendia and I. Caro, Inasmet-Tecnalia, Mikeletegi 2, San SebastiÃ¡n 20009, Spain; J. GonzÃ¡lez del Amo, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2007-069: NON-INVASIVE PLASMA DIAGNOSTIC INSIDE A HALL THRUSTER DISCHARGE; Rostislav Spektor and Edward J. Beiting, The Aerospace Corporation

2007-070: QUASI-LINEAR ANALYSIS OF ANOMALOUS ELECTRON MOBILITY INSIDE A HALL THRUSTER; Rostislav Spektor, The Aerospace Corporation

2007-071: OPERATING CHARACTERISTICS OF CYLINDRICAL AND ANNULAR HELICON SOURCES; Brian E. Beal, Air Force Research Laboratory, Edwards AFB, CA 93524; Fabian Mak, Georgia Institute of Technology, Atlanta, GA 30332

2007-072: SIMPLE PERFORMANCE MODELING OF A RADIO-FREQUENCY ION THRUSTER; Michael M. Tsay and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, U.S.A.

2007-073: EXPERIMENTAL AND NUMERICAL EXAMINATION OF A HALL THRUSTER PLUME; Michael R. Nakles, Lubos Brieda, and Garrett D. Reed, ERC, Inc., Edwards Air Force Base, CA 93524; William A. Hargus, Jr., Air Force Research Laboratory, Edwards Air Force Base, CA 93524; Randy L. Spicer, Virginia Tech, Blacksburg, VA 24061

2007-074: TOTAL AND DIFFERENTIAL SPUTTER YIELDS OF BORON NITRIDE MEASURED BY QUARTZ CRYSTAL MICROBALANCE AND WEIGHT LOSS; Binyamin Rubin, James L. Topper, and Azer P. Yalin, Colorado State University, Fort Collins, Colorado, 80523

2007-075: BORON NITRIDE SPUTTER EROSION MEASUREMENTS BY CAVITY RING-DOWN SPECTROSCOPY; Azer P. Yalin, Lei Tao, and Naoji Yamamoto, Colorado State University, Fort Collins, Colorado, 80523, USA; Timothy B. Smith and Alec D. Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2007-077: ELECTRIC PROPULSION PLUME INTERACTIONS WITH FORMATION FLYING SPACECRAFT; Raed Kafafy, International Islamic University Malaysia, Kuala Lumpur, 50728, Malaysia; Cao Young, Harbin Institute of Technology, Shenzhen, Public Republic of China; Joseph Wang, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061, USA

2007-078: EFFECT OF CATHODE POSITION ON HALL-EFFECT THRUSTER PERFORMANCE AND CATHODE COUPLING VOLTAGE; Jason D. Sommerville and Lyon B. King, Michigan Technological University, Houghton, Michigan 49931, USA

2007-079: LOW FREQUENCY INSTABILITY AND ENHANCED TRANSFER OF ELECTRONS IN NEAR-ANODE REGION OF HALL THRUSTER; A. Kapulkin and M. Guelman, Asher Space Research Institute, Technion, I. I. T., Haifa, 32000, Israel

2007-080: NANOPARTICLE FIELD EXTRACTION THRUSTER (NANOFET): DESIGN AND RESULTS OF THE MICROPARTICLE EMITTER PROTOTYPE; Louis Musinski, Thomas Liu, Brian Gilchrist, Alec Gallimore, and Michael Keidar, University of Michigan, Ann Arbor, MI 48109

2007-081: PRELIMINARY THRUST CHARACTERIZATION OF THE T-SERIES HOLLOW CATHODES FOR ALL-ELECTRIC SPACECRAFT; Angelo N. Grubisic and Stephen B. Gabriel, Astronautics Research Group, University of Southampton, Southampton, SO17 1BJ, United Kingdom; David G. Fearn, Electric Propulsion Solutions, Fleet, Hants, GU14 0LX, United Kingdom

2007-082: CHARACTERIZING SPECIES COMPOSITION IN RADIO-FREQUENCY PLASMA PRODUCED FROM WATER VAPOR; Sonca Nguyen, Kristina Lemmer, John Foster, and Alec Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2007-083: THE DAWN ION PROPULSION SYSTEM – GETTING TO LAUNCH; John r. Brophy, M. Andy Etters, Jason Gates, Charles e. Garner, Marlin Klatte, C. John Lo, Michael G. Marcucci, Steve Mikes, Masashi Mizukami, Barry Nakazono, and Greg Pixler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2007-084: IN ORBIT OPERATION OF 20MN CLASS XENON ION ENGINE FOR ETS-VIII; Toshiyuki Ozaki, Yukikazu Kasai, and Takafumi Nakagawa, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan; Takashi Itoh, Kenichi Kajiwara, and Masafumi Ikeda, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2007-085: DEVELOPMENT AND THRUST PERFORMANCE OF A MIRCOWAVE DISCHARGE HALL THRUSTER; Hirohisa Kuwano, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan; Akira Ohno, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 3-1-1, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Hideki Nakashima, Kyushu University, 6-1, Kasuga-Kouen, Kasuga 816-8580, Japan

2007-086: TWO-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF A CYLINDRICAL HALL THRUSTER; Hae June Lee, Pusan National University, Busan, 609-735, South Korea; Jongho Seon, Satrec initiative, Daejeon, 305-81, South Korea; Wonho Choe, Jungsub Lee, and Youbong Lim, Advanced Institute of Science and Technology, Daejeon 305-701, South Korea

2007-087: NUMERICAL STURDY OF ELECTRODE GEOMETRY EFFECTS ON FLOWFIELD IN TWO-DIMENSIONAL MPD THRUSTERS; K. Kubota, Tokyo Institute of Technology, Yokohama, Kanagawa, 226-8502, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Okuno, Tokyo Institute of Techology, Yokohama, Kanagawa, 226-8502, Japan

2007-088: REALIZATION OF LOW FREQUENCY OSCILLATION FREE OPERATION IN A HALL THRUSTER; Taichiro Tamida and Ikuro Suga, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-honmachi, Amagasaki, Hyogo, 661-8661, Japan; Takafumi Nakagawa, Hiroyuki Osuga, and Toshiyuki Ozaki, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Katsuaki Matsui, Institute for Unmanned Space Experiment Free Flyer 2-12, Kanda-Ogawamachi, Chiyoda-Ku, Tokyo, 101-0052, Japan

2007-089: HOLLOW CATHODE LIFE TEST FOR THE NEXT-GENERATION ION ENGINE IN JAXA; Yasushi Ohkawa, Yukio Hayakawa, Hideki Yoshida, Katsuhiro Miyazaki, Hiroshi Nagano, and Shoji Kitamura, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2007-090: MEASUREMENTS OF HOLE SHAPE ON CARBON-CARBON COMPOSITE GRID AFTER 20,000-HOUR ENDURANCE TEST; Miyuki Usui, University of Tokyo, Hongo, Tokyo, 113-8656, Japan; Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-091: MONTE CARLO SIMULATION OF GAS FLOWS IN SPT-ATON; Yan Guojun, Liu Hui, Wang Chunsheng, and Yu Daren, Harbin Institute of Technology Plasma Propulsion Laboratory, Harbin, 150001

2007-092: INVESTIGATION OF INTERNAL PLASMA STRUCTURE IN AN ANODE-LAYER HALL THRUSTER; Nanako Takahashi, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-kouen, Kasuga, Fukuoka 816-8580, Japan; Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, Department of Aeronautics and Astronautics, The University of Tokyo, Hongo 7-3-1, Bunkyo-ku, Tokyo, 113-8656, Japan

2007-093: DEVELOPMENT STATUS OF POWER PROCESSING UNIT FOR 250MN-CLASS HALL THRUSTER; Hiroyuki Osuga, Kentaro Suzuki, Toshiyuki Ozaki, and Takafumi Nakagawa, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Ikuro Suga and Taichiro Tamida, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-honmachi, Amagasaki, Hyogo, 661-8661, Japan; Yoshiyuki Akuzawa, Fumitoshi Soga, and Hirokazu Suzuki, Department, Kamakura Engineering Office, Mitsubishi Electric Engineering Comp, 730 Kamimachiya, Kamakura, Kanagawa, 247-0065, Japan; Katsuaki Matui, Institute for Unmanned Space Experiment Free Flyer, 2-12 Kanda-Ogawamachi, Chiyoda-Ku, Tokyo, 101-0052, Japan

2007-094: LABORATORY EXPERIMENT OF MAGNETOPLASMA SAIL, PART 2: MAGNETIC FIELD INFLATION; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; T. Kimura, K. Ueno, T. Ayabe, and H. Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; H. Yamakawa, Kyoto University, Uji, Kyoto, 611-0011, Japan; Y. Kajimura and H. Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan

2007-095: NUMERICAL ANALYSIS OF ANODE SHEATH STRUCTURE TRANSITION IN AN ANODE-LAYER TYPE HALL THRUSTER; Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2007-096: FORWARD LASER PLASMA ACCELERATOR FOR RELATIVISTIC PLASMA PROPULSION; Sota Sumida, Masakuni Takagi, and Hideyuki Horisawa, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Itsuro Kimura, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-097: CHEMICALLY-AUGMENTED PULSED LASER-RAMJET; Tomoki Kaneko, Hideyuki Horisawa, and Kazunobu Tamadao, Department of Aeronautics and Astronautics, Tokai University, 1117 Kitakaname, Hiratsuka, Kanagawa, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo Bunkyo-ku, Tokyo, Japan 113-8856

2007-098: DEVELOPMENT OF A TWO-AXIS DUAL PENDULUM THRUST STAND FOR THRUST VECTOR MEASUREMENT OF HALL THRUSTERS; Naoki Nagao, Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656

2007-099: DESIGN AND FABRICATION OF AN INTEGRATED MEMS-BASED COLLOID MICROPROPULSION SYSTEM; R. Krpoun, M. RÃ¤ber, and H. R. Shea, Ecole Polytechnique FÃ©dÃ©rale de Lausanne, CH-1015 Lausanne, Switzerland; K. L. Smith and J. P. W. Stark, Queen Mary University of London, London, E1 4NS, United Kingdom

2007-100: PERFORMANCE INVESTIGATION OF SPT-20M LOW POWER HALL EFFECT THRUSTER; A. V. Loyan and T. A. Maksymenko, National Aerospace University, “KhAI”, 61070 Kharkiv, Ukraine

2007-101: INTERNAL PLASMA STRUCTURE MEASUREMENT IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER; Shinya Kondo, Takayuki Chikaoka, Teppei Tsuru, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, 6-1 Kasuga-koen, kasuga, Fukuoka 816-8580, Japan; Amane Majima, Takao Yamada, Kentaro Tomita, and Kiichiro Uchino, Department of Applied Science for Electronics and Materials, Kyushu University, 6-1 Kasuga-koen, Fukuoka 816-8580, Japan

2007-102: MULTI-MODE THRUSTER WITH ANODE LAYER DEVELOPMENT STATUS; Alexander E. Solodukhin, Alexander V. Semenkin, Leonid E. Zakharenkov, Anatoly V. Rusakov, and Alexander G. Karabadzhak, Central Research Institute of Machine Building (TsNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070; Alexander N. Nesterenko, Experimental Design Bureau “FAKEL”, 181 Moskovsky prospect, Kaliningrad 236001 Russia

2007-103: INVESTIGATION OF HOLLOW CATHODE FOR LOW POWER HALL EFFECT THRUSTER; N. N. Koshelev and A. V. Loyan, National Aerospace University, “KhAI”, 61070 Kharkiv, Ukraine

2007-104: PIC SIMULATIONS ON CHARGE MITIGATION BY PLASMA RELEASE; Hideyuki Usui and Koujirou Imasato, Research Institute for Sustainalbe Humanosphere, Kyoto University, Uji, Kyoto 611-0011, Japan

2007-105: VISUALIZATION OF THE CHARGED PARTICLES MOVEMENT FEATURES IN CONDITIONS, WHICH ARE CHARACTERISTIC FOR THE HALL THRUSTER DISCHARGE INTERVAL AS THE TECHNIQUE FOR THE STUDENTS TRAINING IN SPACE ELECTRIC PROPULSION; Oghienko (Ogiienko) Sergii, Setrakova Yana, Vakulenko Tamara, and Kulish Olga, Zhukovsky National Aerospace University, “Kharkov Aviation Institute”, Ukraine

2007-106: 1D SIMULATIONS ON THE HELICON DOUBLE LAYER; Marco Manente, CISAS University of Padua, Padova Italy; Johan Carlsson, Tech-X Corporation, Boulder, Colorado, USA; Ivano Musso, CISAS University of Padua, Padova Italy – ISTI-CNR Pisa Italy; Cristina Bramanti, Advanced Concept Team ESA ESTEC Noordwijk – The Netherlands; Cinzia Giacomuzzo and Daniele Pavarin, CISAS University of Padua, Padova Italy

2007-107: NUMERICAL INVESTIGATION OF COUPLED ELECTRODYNAMIC TETHER / ELECTROSTATIC PROPULSION SYSTEMS; Torsten Stindl and Markus Fertig, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, 70550 Stuttgart, Germany; Monika Auweter-Kurtz, UniversitÃ¤t Hamburg, 20146 Hamburg, Germany

2007-108: PHYSICS AND EVOLUTION OF HEMP-THRUSTERS; GÃ¼nter Kornfeld, Norbert Koch, and Hans-Peter Harmann, Thales Electron Devices GmbH, SÃ¶flingerstr. 100, 89077 Ulm, Germany

2007-109: DEVELOPMENT AND FLIGHT TESTS OF THE FIRST ELECTRIC PROPULSION SYSTEM IN SPACE; V. A. Khrabrov, Russian Scientific Center “Kurchatov Institute”, Moscow, 123098, Russia

2007-110: STATUS OF THE THALES HIGH EFFICIENCY MULTI STAGE PLASMA THRUSTER DEVELOPMENT FOR HEMP-T 3050 AND HEMP-T 30250; N. Koch, H. –P. Harmann and G. Kornfeld, THALES Electron Devices GmbH, D-89077 Ulm, Germany

2007-111: EUROPEAN STUDENT MOON ORBITER SOLAR ELECTRIC PROPULSION SUBSYSTEM ARCHITECTURE – AN ALL – ELECTRIC SPACECRAFT; M. Coletti and A. Grubisic, University of Southampton, Southampton, SO17 1BJ, United Kingdom; N. Wallace, QinetiQ, Farnborough, GU14 0LX, United Kingdom; N. Wells, QinetiQ, Farnborough, GU14 0LX, United Kingdom

2007-112: SCALING OF A COLLOID THRUSTER SYSTEM FOR MICRONEWTON TO MILLINEWTON THRUST LEVELS; Katharine L. Smith, Matthew S. Alexander, Mark D. Paine, and John P. W. Stark, School of Engineering and Materials Science, Queen Mary University of London, London, E1 4NS, UK

2007-113: NUMERICAL SIMULATION OF THE INSERT CHEMISTRY OF THE HOLLOW CATHODE FROM THE DEEP SPACE 1 ION ENGINE 30,000 HRS LIFE TEST; M. Coletti and A. Grubisic, University of Southampton, Southampton, SO17 1BJ, United Kingdom; S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, United Kingdom

2007-114: LOW COMPLEXITY AND LOW COST ELECTRIC PROPULSION SYSTEM FOR TELECON SATELLITES BASED ON HEMP THRUSTER ASSEMBLY; Hans-Peter Harmann, Norbert Koch, and Guenter Kornfeld, Thales Electron Devices, 89077 Ulm, Germany

2007-115: AN EXPERIMENTAL STUDY OF THE ELECTRODE FALL VOLTAGE IN A MPD THRUSTER; Daisuke Nakata, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16, Nakacho, Koganei-shi, Tokyo 184-8588, Japan; Yukio Shimizu, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Ikkoh Funaki, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Yoshihiro Arakawa, University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2007-116: PULSED PLASMA THRUSTER USING POWDERED PROPELLANT; Takefumi Saito, University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan; Hiroyuki Koizumi and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Institute of Space and Aeronautical Science, Sagamihara, Kanagawa, 229-8510, Japan

2007-117: STATUS OF THE THALES TUNGSTEN/OSMIUM MIXED-METAL HOLLOW CATHODE NEUTRALIZER DEVELOPMENT; N. Koch, H. –P. Harmann, and G. Kornfeld, THALES Electron Devices GmbH, D-89073 Ulm, Germany

2007-118: THRUST MEASUREMENTS WITH THE ONERA MICRONEWTON BALANCE; Denis Packan, Jean Bonnet, and Simone Rocca, ONERA, Chemin de la HuniÃ©re, 91120 Palaiseau, France

2007-119: THE ULAN TEST STATION AND ITS DIAGNOSTIC PACKAGE FOR THRUSTER CHARACTERIZATION; Hans-Peter Harmann, Norbert Koch and Guenter Kornfeld, Thales Electron Devices, 89077 Ulm, Germany

2007-120: ELECTROSTATIC INFLUENCE ON CHARGE TO MASS SPECTRUM IN MIXED ION/DROPLET MODE: IMPLICATIONS FOR COLLOID THRUSTER DESIGN; Sobash Jhuree, Matthew S. Alexander, and John PW Stark, School of Engineering & Materials Science, Queen Mary, University of London, UK

2007-121: MODEL ANALYSIS OF A DOUBLE STAGE HALL EFFECT THRUSTER WITH DOUBLE-PEAKED MAGNETIC FIELD AND INTERMEDIATE ELECTRODE; J. PÃ©rez-Luna, G.J.M. Hagelaar, L. Garrigues, and J. P. Boeuf, Laboratoire Plasma et Conversion d’Energie, LAPLACE, CNRS – UniversitÃ© Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse cedex 9, France

2007-122: STATUS OF THE INDIUM FEEP MICROPROPULSION SUBSYSTEM DEVELOPMENT FOR LISA PATHFINDER; C. Scharlemann, A. Genovese, N. Buldrini, R. Schnitzer, and M. Tajmar, Austrian Research Centers GmbH-ARC, 2444 Seibersdorf, Austria; H. FrÃ¼holz, Astrium Friedrichshafen GmbH, D-88039 Friedrichshafen, Germany; R. Killinger, Astrium Space Transportation, D-74239 Lampoldshausen, Germany

2007-123: FIELD EMISSION PERFORMANCE OF MACROSCOPICALLY GATED MULTIWALLED CARBON NANOTUBES FOR A SPACECRAFT NEUTRALIZER; Karen L. Aplin and Barry J. Kent, Rutherford Appleton Laboratory, Didcot, Oxfordshire, OX11 0QX, UK; Chris Castelli, Science and Technology Facilities Council, Swindon, Wiltshire, SN2 1SZ, UK; Wenhui Song, Brunel University, Uxbridge, Middlesex, UB8 3PH, UK

2007-124: INFLUENCE OF AZIMUTHAL INSTABILITES ON ELECTRON MOTION IN A HALL EFFECT THRUSTER; J. PÃ©rez-Luna, G.J.M. Hagelaar, L. Garrigues, N. Duduit and J. P. Boeuf, Laboratorie Plasma et Conversion d’Energie, LAPLACE, CNRS – UniversitÃ© Paul Sabatier, 118 Route de Narbonne, 31062 Toulouse cedex 9, France

2007-125: MICRO PULSED PLASMA THRUSTER DEVELOPMENT; S. J. Pottinger and C. A. Scharlemann, Austrian Research Centers GmbH – ARC, A-2444 Seibersdorf, Ausria

2007-126: LOW BANK ENERGY APPT FOR MICRO SATELLITES; Nikolay N. Antropov and Garry A. Popov, Research Institute of Applied Mechanics and Electrodynamics, 4, Voloklamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Center Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Enrico Chesta, Centre National D’Etudes Spatiales (CNES), 18, Avenue Edouard Belin, 31401 Toulouse Cedex, France; Vladimir P. Khodnenko, All-Russian Research Institute of Electromechanics, 101000, P.O. Box 496, Moscow, Russia

2007-127: THERMAL STATE INVESTIGATIONS OF TWO-STAGE THRUSTER WITH ANODE LAYER; A. S. Mitroshin, V. I. Garkusha, A. V. Semenkin, and A. E. Solodukhin, Central Research Institute of Machine Building (TsNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070

2007-128: DEVELOPMENT AND STUDY OF THE VERY HIGH SPECIFIC IMPULSE BISMUTH TAL; L. Zakharenkov and A. Semenkin, Central Research Institute of Machine Building (TSNIIMASH), Korolev, Moscow region, Pionerkaya 4, 141070, Russia; S. Tverdokhlebov, JSC “TSNIIMASH-EXPORT”, Russia; A. Sengupta and C. Marrese-Reading, Jet Propulsion Laboratory (JPL), USA

2007-129: DEVELOPMENT OF LOW-POWER HALL THRUSTER WITH LIFETIME UP TO 3000 HOURS; Mikhail B. Belikov, Oleg A. Gorshkov, Evgeny N. Dyshlyuk, Aleksandr S. Lovtzov, and Adrey A. Shagayda, Keldysh Research Center, Moscow, 125438, Russia

2007-130: DEVELOPMENT OF VERNIER PROPULSION SYSTEM FOR MICRO SATELLITE ON THE BASIS OF ABLATIVE PULSED PLASMA THRUSTER; A. V. Bogatiy, Engineer, RIAME; G. A. Diakonov, Senior Researcher, RIAME

2007-131: PROBE MEASUREMENTS IN THE CHANNEL OF 1.5KW HALL THRUSTER WITH DISCHARGE VOLTAGE UP TO 1000 V; M. B. Belikov, O. A. Gorshkov, A. S. Lovtsov, and A. A. Shagayda, Keldysh Research Center, 8 Onezhskaya street, Moscow, 125438, Russia

2007-132: APPT HEAT FLUXES MEASUREMENT AND CALCULATION; Garry A. Popov, Nikolay N. Antropov, Vladimir N. Jakovlev, and Valery K. Tyutin, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev and Vladimir F. Kozlov, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia

2007-133: ANALYSIS OF CERAMIC EROSION CHARACTERISTIC IN HALL-EFFECT THRUSTER WITH HIGHER SPECIFIC IMPULSE; Vladimir V. Abashkin, Oleg A. Gorshkov, Alexander S. Lovtsov, and Andrey A. Shagaida, Keldysh Research Center (KeRC), Moscow, Russia, 125438

2007-134: DEVELOPMENT OF NEXT GENERATION APPT AT RIAME; Garry A. Popov, Director, RIAME; Nikolay N. Antropov, Header Department, RIAME, Research Institute of Applied Mechanics and Electrodynamics (RIAME), Moscow, 125080, Russia

2007-135: SCALING OF THE CURRENT CONDUCTION ZONE IN LITHIUM-FED ARC MULTICHANNEL AND SINGLE-CHANNEL HOLLOW CATHODES; Leonard D. Cassady, Ad Astra Rocket Company, Bay Area Plaza, 141 Bay Area Blvd., Webster, TX 77599, USA; E. Y. Choueiri, Princeton University, Princeton, New Jersey 08544, USA

2007-136: DEVELOPMENT OF HIGH POWER MAGNETOPLASMADYNAMIC THRUSTERS IN THE USSR; O. A. Gorshkov and V. N. Shutov, Keldysh Research Center, Moscow, 125438, Russia; K. N. Kozubsky, EDB “Fakel”, Kaliningrad, Russia; V. G. Ostrovsky, RSC “Energia”, 141070, Russia; V. A. Obukhov, RIAME MAI, Moscow, 125871, Russia

2007-137: SUBSCALE LIFECYCLE TEST OF THERMAL ARCJET THRUSTER TALOS FOR THE LUNAR MISSION BW1; D. Bock, G. Herdich and H. –P. RÃ¶ser, Institut fÃ¼r Raumfahrtsystem, Pfaffenwaldring 31, 70569 Stuttgart, Germany; M. Auweter-Kurtz, UniversitÃ¤t Hamburg, Hamburg, Germany

2007-138: NUMERICAL SIMULATIONS OF MAGNETOPLASMADYNAMIC THRUSTERS WITH COAXIAL APPLIED MAGNETIC FIELD; Daniel Haag and Markus Fertig, UniversitÃ¤t Stuttgart, Institut fÃ¼r Raumfahrtsysteme, Pfaffenwaldring 31, 70569 Stuttgart, Germany; Monika Auweter-Kurtz, UniversitÃ¤t Hamburg, Edmund-Siemers-Allec 1, 20146 Hamburg, Germany

2007-139: LASER INDUCED ELECTRON BURSTS FOR THE DIAGNOSTIC OF HALL THRUSTER PLASMA; T. Gilbert, A. Leufroy, and A. Bouchoule, Groupe de Recherches sur l’EnergÃ©tique des Milieux IonisÃ©s, OrlÃ©ans, 45000, France; A. Lazurenko, Thales Electron Devices GmgH, Ulm, D89077, Germany

2007-140: 3000 HOUR LIFETIME TEST OF AN INDIUM FEEP CLUSTER FOR THE LISA PATHFINDER MISSION; A. Genovese, N. Buldrini, R. Schnitzer, M. Tajmar, and C. Scharlemann, Austrian Research Centers GmbH-ARC, 2444 Seibersdorf, Austria

2007-141: EXPERIMENTAL INVESTIGATIONS OF MAGNETOPLASMADYAMIC THRUSTERS WITH COAXIAL APPLIED MAGNETIC FIELD; Daniel Haag, Markus Fertig, Georg Herdrich, Helmut Kurtz, and Michael Winter, UniversitÃ¤t Stuttgart, Institut fÃ¼r Raumfahrtsysteme, Pfaffenwaldring 31, 70569 Stuttgart, Germany; Monika Auweter-Kurtz, UniversitÃ¤t Hamburg, Edmund-Siemers-Allee 1, 20146 Hamburg, Germany

2007-142: HISTORY OF THE HALL THRUSTERS DEVELOPMENT IN USSR; V. Kim, Research Institute of Applied Mechanics and Electrodynamics (RIAME), Moscow, 125871, Russia; K. N. Kozubsky and V. M. Murashko, Design bureau Fakel, Kaliningrad, 236001, Russia; A. V. Semenkin, Tsentral Research Institute of Machinebuilding (TsNIIMASH), Korolev, 141070, Russia

2007-143: INVESTIGATION OF ELECTRON TRANSPORT PROPERTIES IN HALL THRUSTERS THROUGH MEASUREMENTS OF MAGNETIC FIELD FLUCTUATIONS; G. Coduti, A. Lazurenko, S. Mazouffre, and M. Dudeck, ICARE Laboratory CNRS, Orleans, Centre, 45071, France; A. Bouchoule, GREMI Laboratory, Orleans University, Centre, 45071, France

2007-144: MASS-SPECTROMETRIC MEASUREMENTS OF A PARTICLE CHARGE STRUCTURE IN THE PLASMA JET OF THE STATIONARY PLASMA THRUSTER; A. N. Veselovzorov, E. E. Barkalov, A. A. Pogorelov, E. B. Svirsky, and V. A. Smirnov, Russian Research Centre ‘Kurchatov Institute’ Moscow, Russia

2007-145: FABRICATION AND CHARACTERIZATION OF POROUS METAL EMITTERS FOR ELECTROSPRAY THRUSTERS; Robert S. Legge Jr., Paulo Lozano, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2007-146: 2D OOPIC SIMULATIONS OF THE HELICON DOUBLE LAYER; I. Musso, Center for Studies and Activities for Space, University of Padua, Padova Italy, Institute of Information Science and Technology, National Research Council of Italy, Pisa, Italy; M. Manente, Center for Studies and Activities for Space, University of Padua, Padova, Italy; J. Carlsson, Tech-X Corporation, Boulder Colorado, USA; C. Bramanti, European Space Research and Technology Center, European Space Agency, Noordwijk, The Netherlands; D. Pavarin, Cener for Studies and Activities for Space, University of Padua, Padova, Italy

2007-147: THE BRAZILIAN ELECTRIC PROPULSION PROGRAM; Gilberto M. Sandonato, JosÃ© AmÃ©rico N. Goncalves, Ricardo T. Irita, George F. Fernandes, and Paolo Gessini, Institutio Nacional de Pesquisas Espaciais, Sao JosÃ© doc Campos, SP, 12227-010, Brazil; Rodrigo I. Marques and Stephen B. Gabriel, University of Southampton, Southampton, United Kingdom, SO17, 1BJ

2007-148: ION BEAM CHARACTERIZATION BY ADVANCED PLASMA DIAGNOSTICS WITH LEVITATED PARTICLES; Holger Kersten and Thomas Trottenberg, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany; Ruben Wiese, INP Greifswald, F. –Hausdorff-Strass 02, 17489 Greifswald, Germany; Frank Scholze, Michael Tartz, and Horst Neumann, IOM Leipzig Permoserstrasse 15, 04318 Leipzig, Germany

2007-149: A PENDULUM TARGET BALANCE FOR ION ENGINE THURST MEASUREMENT; Paolo Gessini, Gilberto Marrega Sandonato, Ricardo Toshiyuki Irita, JosÃ© AmÃ©rico Neves Goncalves and George Favale e Fernandes, Instituto Nacional de Pesquisas Espaciais (INPE), Sao JosÃ© dos Campos, SP, 12227-010, Brazil

2007-150: ELECTRIC PROPULSION DIAGNOSTIC PACKAGE FOR THE FEEP THRUSTER ON LISA PATH FINDER; REVIEW OF STATUS OF ACHIEVEMENTS AT TAS-I; M. Cpacci, G. Matticari, M. Materassi, E. Artina, and V. Vettorello, Thales Alenia Space Italia, Florence Site, 50013 Campi Bisenzio, Italy, Thales Alenia Space Italia, Milano Site, 50013 Vimodrone, Italy

2007-151: INVESTIGATION OF THE SPT OPERATION AND DISCHARGE CHAMBER WALL EROISION RATE UNDER INCREASED DISCHARGE VOLTAGES; V. Kim, V. I. Kozlov, A. I. Skrylnikov, and E. K. Sidorenko, Research Institute of Applied Mechanics and Electrodynamics, Moscow, 125871, Russia; V. M. Murashko and A. N. Nesterenko, Design Bureau Fakel, Russia

2007-152: PROGRESS ON RE-GENERABLE FIELD EMISSION CATHODES FOR LOW-POWER ELECTRIC PROPULSION; Jason M. Makela and Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2007-153: CONFINEMENT TIME IN AN ELCTRON TRAP USED FOR ELECTRON-MOBILITY STUDIES IN HALL THRUSTER-LIKE FIELDS; Emily C. Fossum and Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2007-154: DEVELOPMENT AND QUALIFICATION OF A NEUTRALIZER DEVICE FOR THE FEEP MICRO PROPULSION ON MICROSCOPE AND LISA PATH FINDER; M. Capacci, G. Matticari, M. Materassi, and G. Noci, Thales Alenia Space Italia, Florence Site, 50013 Campi Bisenzio, Italy

2007-155: ADVANCED FLUIDIC COMPONENTS FOR ELECTRIC AND COLD GAS PROPULSION APPLICATIONS: REVIEW OF STATUS OF ACHIEVEMENTS AT TAS-I FLORENCE; G. Noci, G. Matticari, P. Siciliano, and L. Fallerini, Thales Alenia Space Italia, Florence Site, 50013 Campi Bisenzio, Italy

2007-157: TWO DIMENSIONAL HYBRID MODEL OF A MINIATURIZED CYLINDRICAL HALL THRUSTER; L. Garrigues, G.J.M. Hagelaar, and J. P. Boeuf, LAPLACE, CNRS-UniversitÃ© Paul Sabatier, 31062 Toulouse, France; Y. Raitses, A. Smirnov, and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543

2007-158: SOLID STATE MPD THRUSTER WITH APPLIED MAGNETIC FIELD; M. Coletti, University of Southampton, Southampton, SO17 1DR, United Kingdom; A. Balestra and M. Sensini, University of Rome “La Sapienza”, Rome, 00185, Italy; G. Paccani, University of Rome “La Sapienza”, Rome, 00185, Italy

2007-159: SPECTROSCOPIC TEMPERATURE MEASUREMENT IN A APPLIED FIELD MPD; M. Coletti, University of Southampton, Southampton, SO17 1DR, United Kingdom; S. Ciampone, Queen Mary University of London, London, E1 4NS, United Kingdom; G. Paccani, University of Rome “La Sapienza”, Rome, 00185, Italy; G. Mazzitelli, ENEA, Frascati, Rome, 00040, Italy

2007-160: A LASER SPECTROSCOPIC STUDY ON XE+ ION TRANSPORT PHENOMENA IN A 5 KW-CLASS HALL EFFECT THRUSTER; S. Mazouffre, D. Gawron, and W. Kulaev, CARE Institute – CNRS, 1c Av. de la Recherche Scientifique, 45071 OrlÃ©ans-France; N. Sadeghi, Laboratoire de SpectromÃ©trie Physique, UniversitÃ© Joseph Fourier – CNRS, 140 Av. de la Physique, BP 87, 38402 Saint Martin d’HÃ©res – France

2007-161: REVIEW OF TWO RETARDING POTENTIAL ANALYZERS FOR USE IN HIGH DENSITY HELICON PLASMA; Kristina M. Lemmer, Alec D. Gallimore, Timothy B. Smith, and Daniel R. Austin, University of Michigan, Ann Arbor, MI, 48109, USA

2007-162: RAM ELECTRIC PROPULSION FOR LOW EARTH ORBIT OPERATION: AN ESA STUDY; D. Di Cara, J. Gonzalez del Amo, A. Santovincenzo, B. Carnicero Dominguez, M. Arcioni, A. Caldwell, and I. Roma; ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands

2007-164: PPS 1350-G QUALIFICATION STATUS 10500 H; Frank Darnon, CNES – Centre Spatial de Toulouse, 18 avenue Edouard Belin, 31401 Toulouse Cedex 4, France; Denis Estublier, ESA/ESTEC – Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands

2007-165: CURRENT SHEET FORMATION IN A CONICAL THETA PINCH FARADAY ACCELERATOR WITH RADIO-FREQUENCY ASSISTED DISCHARGE; Ashley K. Hallock and Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08540, USA; Kurt A. Polzin, NASA – Marshall Space Flight Center, Huntsville, AL, 35812, USA

2007-166: MEASUREMENT AND MODELING OF THE INSIDE CHANNEL DEPOSITION OF THE SPUTTERED CERAMICS ON HET PPSX000-ML. A TOOL TO PREDICT THE EROSION ALONG THE THRUSTER LIFETIME; D. Pagnon, Laboratoire d’Analyse Spectroscopique et d’EnergÃ©tique des Plasmas, UniversitÃ© d’OrlÃ©ans, rue G. Berger, BP 4043 – 18028 Bourges – France; P. Lasgorceix and C. Legentil, Laboratoire d’AÃ©rothermique, 1C Av. de la Recherche Scientifique, 45071 OrlÃ©ans, France

2007-167: SPECIFIC LABORATORY TESTING EQUIPMENT & METHODOLOGY FOR SPUTTERING TESTS OF ELECTRIC PROPULSION MATERIALS; J. Ustarroz, I. Caro, P. Corengia, I. Garmendia, and J. Macros, INASMET-Tecnalia, San SebastiÃ¡n, 20009, Spain; E. Ahedo, Universidad PolitÃ©cnica de Madrid, Madrid 28040, Spain; J. GonzÃ¡lez del Amo, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2007-168: SIMP-LEX: SYSTEMATIC GEOMETRY VARIATION USING THRUST BALANCE MEASUREMENTS; Anuscheh Nawaz, Georg Herdrich, Helmut Kurtz and Tony SchÃ¶nherr, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, 70569, Germany; Monika Auweter-Kurtz, UniversitÃ¤t Hamburg, Edmund-Siemers-Allee 1, Hamburg, Germany

2007-169: MULTI-PHOTON SPECTROSCOPY ON XENON FOR APPLICATION ON ION THRUSTER PLASMA PARAMETER INVESTIGATIONS: EXPERIMENT AND THEORY; Christoph Eichhorn and Michael Winter, Institut fÃ¼r Raumfahrtsysteme IRS, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany; Monika Auweter-Kurtz, UniversitÃ¤t Hamburg, Edmund-Siemers-Allee 1, D-20196 Hamburg, Germany; Stefan LÃ¶hle, DLR Institut fÃ¼r Verbrennungstechnik, Pfaffenwaldring 38-40, D-70569 Stuttgart, Germany

2007-170: DISPENSER TEMPERATURE PROFILE MEASUREMENT AND DISCHARGE CURRENT DIVISION IN THE T5 & T6 KAUFMAN-TYPE ION THRUSTERS; Ismat M. Ahmed Rudwan, N. C. Wallace, and Mike Kelly, Space Division, QinetiQ Plc Ltd, Farnborough, Hampshire, GU14 0LX, UK

2007-171: DEVELOPMENT AND TESTING OF A FIELD-EMISSION NEUTRALISER FOR MICRO-ELECTRIC PROPULSION; Pierre-Etienne Frigot, AOES B.V., Haagse Schouwweg 6G, 2332 KG Leiden, The Netherlands; Karen l. Aplin and Barry J. Kent, Rutherford Appleton Laboratory, Oxfordshire OX11 0QX, United Kingdom; Davide Nicolini and JosÃ© Antonio Gonzalez del Amo, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2007-172: ION VELOCITY MEASUREMENTS WITHIN THE ACCELERATION CHANNEL OF A LOW POWER HALL THRUSTER; William A. Hargus, Jr., Air Force Research Laboratory, Edwards AFB, CA 93524; Michael R. Nakles, E.R.C., Inc., Edwards AFB, CA 93524

2007-173: STATUS ON PLASMA DIAGNOSTIC MEASUREMENTS ON A RIT-10 ION THRUSTER; Michael W. Winter, Christoph Eichhorn, Monika Auweter-Kurtz, and Thomas Pfrommer, UniversitÃ¤t Stuttgart, Institut fÃ¼r Raumfahrtsysteme (IRS), Pfaffenwaldring 31, 70550 Stuttgart, Germany

2007-174: EFFECTS OF VARIED PROPELLANT COMPOSITIONS ON THE ION ENERGY DISTRIBUTIONS IN HOLLOW CATHODES; JoHanna N. Przybylowski, California Institute of Technology, Pasadena, CA, 91125; James E. Polk, Jet Propulsion Laboratory, Pasadena, CA, 91109; Joseph E. Shepard and Angela M. Capece, California Institute of Technology, Pasadena, CA, 91125

2007-177: PERFORMANCE MEASUREMENTS FROM A CLUSTER OF FOUR HALL THRUSTERS; Robert B. Lobbia and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI, 48109, U.S.A.

2007-178: HIGH-POWER ELECTRIC PROPULSION UTILIZING LASER-DRIVEN PONDEROMOTIVE FIELDS; George J. Williams, Jr., The Ohio Aerospace Institute, 22800 Cedar Point Rd., Brookpark, OH 44142

2007-179: FEASIBLITY OF ELECTROSTATIC MICROPARTICLE THRUSTERS; Thomas Trottenberg and Holger Kersten, IEAP, Christian-Albrechts- UniversitÃ¤t zu Kiel, D-24118 Kiel, Germany

2007-181: HIGH POWER VASIMR EXPERIMENTS USING DEUTERIUM, NEON AND ARGON; Jared P. Squire, Franklin R. Chang-DÃaz, Mark D. Carter, Leonardl D. Cassady, William J. Chancery, Tim W. Glover, Verlin T. Jacobson, and Greg E. McCaskill, Ad Astra Rocket Company, Houston, Texas, 77058, USA; Roger D. Bengtson, The University of Texas at Austin, Austin, Texas, 78712, USA; Edgar A. Bering, The University of Houston, Houston, Texas, 77004, USA; Christopher A. Deline, The University of Michigan, Ann Arbor, Michigan, 48109, USA

2007-185: SPECTROSCOPIC ELECTRON TEMPERATURE MEASUREMENT OF THE RECOMBINING PLASMA ON THE VASIMR EXPERIMENT; Ella M. Sciamma and Roger D. Bengtson, The University of Texas at Austin, Austin, TX, 78712, U.S.A.; Franklin R. Chang-Diaz, Verlin T. Jacobson, Jared P. Squire, and W. J. Chancery, Ad Astra Rocket Company, Texas 77058, U.S.A.

2007-186: PHYSICAL MODELS AND PERFORMANCE IMPLICATIONS FOR THE NANOPARTICLE FIELD EXTRACTION THRUSTER; Thomas M. Liu and Louis D. Musinski, University of Michigan, Ann Arbor, MI 48109, USA; Michael Keidar, Alec D. Gallimore, and Brian e. Gilchrist, University of Michigan, Ann Arbor, MI 48109, USA

2007-187: THE PLANAR HALL THRUSTER FOR INVESTIGATING ELECTRON MOBILILTY IN EXB DEVICES; Joshua L. Rovey, Matthew P. Giacomi, Robert A. Stubbers, and Brian e. Jurczyk, Starfire Industries LLC, Champaign, IL, 61820

2007-188: ANALYTICAL EXTRACTION OF PLASMA PROPERTIES USING A HALL THRUSTER EFFICIENCY ARCHITECTURE; Daniel L. Brown, C. William Larson, and James M. Haas, Air Force Research Laboratory, Edwards AFB, CA, 93524, USA; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI, 48109, USA

2007-189: PLASMA FLOW BEHAVIORS AND THEIR EFFECTS ON THE PERFORMANCE OF PULSED PLASMA THRUSTERS; Hiroyuki Koizumi, Institute of Space and Astronautical Science / Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan; Ryosuke Noji, Kimiya Komurasaki, and Third Author, University of Tokyo, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

2007-190: NUMERICAL SIMULATION OF INTERNAL PLASMA IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER; Takayasu Kanagawa, Naoji Yamamoto, Yoshihiro Kajimura, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Graduate School of Engineering Science, Kyushu University, 6-1 Kasuga-koen, Kasuga, Fukuoka 816-8580, Japan; Hirokazu Masui, Department of Electrical Engineering Kyushu Institute of Technology, 1-1 Sensui, Tobata, Kitakyushu, Fukuoka, 804-8550, Japan

2007-191: ION HEATING AND ACCELERATION EXPERIMENT IN HYDROGEN PLASMA FOR THE VASIMR-TYPE THRUSTER; Akira Ando, Yuji Kasashima, Tatsuya Hagiwara, Kunihiko Hattori, and Masaaki Inutake, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2007-192: SCALING AND SYSTEMS CONSIDERATIONS IN PULSED INDUCTIVE THRUSTERS; Kurt A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL 35812

2007-193: XIPS 25-CM THRUSTER CATHODE LIFE QUALIFICATION FOR USE ON DEEP SPACE MISSIONS; James E. Polk and Dan M. Goebel, Jet Propulsion Laboratory, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; William Tighe, L-3 ETI, Torrance, CA 90505

2007-195: MHD ANALYSIS ON PROPULSIVE CHARACTERISTICS OF MAGNETO PLASMA SAIL; Hiroyuki Nishida, University of Tokyo, Hongo, Tokyo, 113-8656, Japan; Ikkoh Funaki, Hiroyuki Ogawa, and Yoshifumi Inatani, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-196: EFFECTS OF HELICON WAVE PROPAGATION BASED ON A CONICAL ANTENNA DESIGN: PART I; Michael P. Reilly and George H. Miley, University of Illinois @ Urbana-Champaign, Urbana, IL, 61801, United States of America; David E. Kirtley University of Michigan, Ann Arbor, MI, 48109, United States of America; William A. Hargus, Jr., Air Force Research Laboratory, Edwards AFB, CA, 93524, United States of America

2007-197: DEVELOPMENT OF NUMERICAL PLASMA PLUME ANALYSIS MODULE FOR SPACECRAFT ENVIRONMENT SIMULATOR; Takanobu Muranaka, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan; Hiroko O. Ueda, Japan Aerospace Exploration Agency, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan; Shinji Hatta and Jeongho Kim, MUSCAT Space Engineering Co., Ltd, 1-1 Sensui-cho, Tobata-ku, Kitakyushu, Fukuoka 229-8510, Japan; Mengu Cho, Kyushu Institute of Technology, 1-1 Sensui-cho, Tobata-ku, Kitakyushu, Fukuoka 804-8550, Japan; Kiyokazu Koga and Tateo Goka, Japan Aerospace Exploration Agency, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505, Japan; Hideyuki Usui, Kyoto University, Gokasho, Ujk, Kyoto 611-0011, Japan; Iku Shinohara, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2007-199: PULSED MAGNETOPLASMADYNAMIC DETONATION PROPULSION; Kyoichi Kuriki, Junichiro Aoyagi, and Haruki T akegahara, Tokyo Metropolitan University, Tokyo, 191-0065, Japan

2007-200: NUMERICAL CALCULATION OF WALL EROSION ON HALL THRUSTERS USING 2D-HYBRID-PIC MODELING; Hiroyuki Koizumi, Institute of Space and Astronautical Science/Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

2007-201: MICRO-PLASMAJET ARRAY: MULTI-JET-EFFECT FOR THRUST PERFORMANCE IMPROVEMENT; Atsushi Koshiyama, Fujimi Sawada, and Hideyuki Horisawa, Dept. of Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, 3-1-1 Sagamihara, Kanagawa, 229-8510, Japan

2007-202: CHARACTERIZATION OF AN ANNULAR HELICON PLASMA SOURCE; Douglas Palmer, Cengiz Akinli, Logan Williams, and Mitchell L. R. Walker II, High-Power Electric Propulsion Laboratory, Georgia Institute of Technology, Atlanta, GA, 30332, USA

2007-203: SPECTRAL MEASUREMENTS OF MHTX HELICON DISCHARGE PLASMA; Murat Celik, Oleg Batishchev, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2007-204: NUMERICAL SIMULATION OF THE FREE MOLECULEMICRO-RESISTOJET FLOW; Mao-lin Chen, Mao Gen-wang, Yang Juan, and Xia Guang-qing, Northwestern Polytechnical University, Xi’an, shannxi, 710072, China

2007-205: MICROWAVE DISCHARGE ION THRUSTER USING ARGON AS A PROPELLANT; Makoto Miyoshi, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Graduate School of Engineering Sciences, Kyushu University, 6-1 Kasuga-kouen, Kasuga, Fukuoka Prefecture, 816-8580, Japan

2007-206: CNES ELECTRIC PROPULSION ACTIVITIES OVERVIEW: FLIGHT PROGRAMS, R&T ACTIONS, NOVEL MISSION DESIGNS; Enrico Chesta, Denis Arrat, RÃ©gis Bertrand, Franck Darnon, StÃ©phane D’Escrivan, and Nicolas Pillet, Centre National d’Etudes Spatiales (CNES), 18 avenue Edouard Belin, F-31401 Toulouse, France

2007-207: THE “NEW GRID SYSTEMS FOR ION ENGINES” TECHNOLOGY PROJECT – FINAL ASSESSMENT; Hans J. Leiter, Ralf Kukies, Werner Kadrnoschka, and Rainer Killinger, Astrium Space Transportation GmbH, P.O. 1119, 74215 MÃ¶ckmÃ¼hl, Germany

2007-209: RIT-ÂµX – THE NEW MODULAR HIGH PRECISION MICRO ION PROPUSLION SYSTEM; Hans Leiter and Rainer Killinger, Astrium GmbH BL Equipment and Propulsion, P.O. 1119, 74215, MÃ¶ckmÃ¼hl, Germany, Michael Boss, Michael Braeg, and Matthias Gollor, Astrium Satellites GmbH, 88039 Friedrichshafen, Germany; Michael Tartz and Horst Neumann, IOM Leipzig, Permoserstr. 15, 04318 Leipiz, Germany; Jens Haderspeck and Dagmar Bock, IRS Stuttgart Pfaffenwaldring 31, 70569, Stuttgart, Germany; Davina Maria Di Cara, ESA ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2007-210: THRUST CONTROL ALGORITHMS FOR THE GOCE ION PROPULSION ASSEMBLY; M. H. Corbett, QinetiQ Ltd, Cody Technology Park, Farnborough, GU14 0LX, U.K.; C. H. Edwards, ESA-ESTEC, Keplerlaan 1, 2200 AG, Noordwijk ZH, The Netherlands

2007-211: NUMERICAL SIMULATION OF MICROWAVE PLASMA THRUSTER FLOW: Mao-Lin Chen, Mao Gen-wang, Yang Juan, and Xia Guang-qing; Northwestern Polytechnical University, Xi’an, shannxi, 710071, China

2007-212: THE ANALYSIS OF INFLUENCE OF ELECTRIAL PROPULSION CHARACTERISTICS ON EFFICIENCY OF TRANSPORT MANEUVERS; M. Konstantinov, Research Institute of Applied Mechanics and Electrodynamics, Moscow, Russia

2007-213: MICROSCOPE MISSION PHASE B PROPULSION SYSTEM ACTIVITIES AT SPACECRAFT LEVEL: REQUIREMENTS CONSOLIDATION AND ASSESSMENT OF NEUTRALIZATION AND CONTAMINATION EFFECTS; Enrico Chesta, Yves AndrÃ©, Laurent Perraud, Benjamin Pouilloux, Pascal Prieur, Thierry Tirolien, Centre National d’Etudes (CNES), 18 Avenue Edouard Belin, F-31401 Toulouse, France; Jean-Francois Russel, Thomas Tondu, Jean-Charles Mateo Velez, ONERA, 2 Avenue Edouard Belin, F-31055 Toulouse, France

2007-214: SIMULATION OF THE ENERGY DEPOSITION ON DIELECTRIC WALL SURFACES IN HALL THRUSTERS; C. Focsa and M. Ziskind, Laboratoire de Physique des Lasers, Atomes et MolÃ©cules (UMR CNRS 8523), Centre d’Etudes et de Recherches Lasers et Applications (FR CNRS 2416), UniversitÃ© de Lille 1, 59655 Villeneuve d’Ascq, France; S. Gurlui, Universitatea “Al. I. Cuza”, Iasi-700506, Romania; D. Pagnon, Laboratoire de Physique des Gaz et des Plasmas, UniversitÃ© de Paris XL, 91405 Orsay, France; S. Pellerin, Laboratoire d’Analyse Spectroscopique et d”EnergÃ©tique des Plasmas, 18028 Bourges, UniversitÃ© d’OrlÃ©ans, France; N. Pellerin, Centre de Recherche sur les MatÃ©riaux Ã¡ Hautes TempÃ©rature, 45071 OrlÃ©ans, France; M. Dudeck, Laboratoire ICARE, CNRS OrlÃ©ans, 45071 OrlÃ©ans, France

2007-215: DISCHARGE MODES AND CHARACTERISTICS OF HOLLOW CATHODE; Shunsuke Sakai, Toshiyuki Katayama, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Tokyo, 191-0065, Japan

2007-217: PERFORMANCE INVESTIGATION OF SPT-20M LOW POWER HALL EFFECT THRUSTER; A. V. Loyan and T. A. Maksymenko, National Aerospace University “KhAI”, 61070 Kharkiv, Ukraine

2007-218: THE ÂµNRIT-4 ION ENGINE: A FIRST STEP TOWARDS A EUROPEAN MINI-ION ENGINE SYSTEM DEVELOPMENT; D. Feili, D. M. Di Cara, H. J. Leiter, J. G. Del Amo, H. W. Loeb, St. Weis, D. Kirmse, P. E. Frigot, M. Orlandi, H. MÃ¼ller, and B. K. Meyer, Giessen University, Electric Propulsion Group, Heinrich-Buff-Ring 16, 35390, Giessen, Germany

2007-219: NEUTRAL VELOCITY VECTOR AND ABSOLUTE NUMBER DENSITY LIF OPTICAL MEASUREMENT WITH APPLICATION TO A FLIGHT MODE MICROSCOPE CESIUM FEEP THRUSTER; Denis Packan, Jean Bonnet, Alexandre Bresson, and Brigitte Attal-Tretout, ONERA, Chemin de la Hunire, 91120 Palaiseau, France

2007-220: OPTIMISED THRUST STEERING OF A GRIDDED ION ENGINE; P. Jameson, QinetiQ Ltd, Cody Technology Park, Farnborough, GU14 0LX, U.K.

2007-221: TWO-MODES OPERATION OF SPT OF SECOND GENERATION; A. I. Bugrova, A. V. Desyatskov, V. K. Kharchevnikov, and A. S. Lipatov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia

2007-222: OVERRUN DISCHARGE CURRENT OPERATION OF LOW POWER CYLINDRICAL HALL THRUSTERS; Yevgeny Raitses, Artem Smirnov, Erik Granstedt, and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543

2007-223: FEASIBILITY STUDY OF PLASMA CHEMICAL THRUSTER; Junichiro Aoyagi, Kyoichi Kuriki, and Haruki Takegahara, Tokyo Metropolitan University, Tokyo, 191-0065, Japan; Jun Yokote, Akira Kakami, and Takeshi Tachibana, Kyushu Institute of Technology, Kitakyushu, 800-0000, Japan

2007-226: PRELIMINARY STUDY ON RADIO FREQUENCY NEUTRALIZER FOR ION ENGINE; Tomoyuki Hatakeyama, Masatoshi Irie, Hiroki Watanabe, Aasami Okutsu, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2007-227: MULTI-CHANNEL HALL-EFFECT THRUSTERS: MISSION APPLICATIONS AND ARCHITECTURE TRADE-OFFS; Olivier Duchemin, Anthony Lorand, Michael Notarianni, and Dominique Valentian, Snecma, Safran Group, Division Moteurs Spatiaux, 27208 Vernon, France; Enrico Chesta, CNES, Centre Spatial de Toulouse, 31401 Toulouse, France

2007-228: FEASIBILITY STUDY OF AN MPD ARCJET AS A PLASMA INJECTOR FOR MARS’S ATMOSPHERE DYNAMICS RESEARCH; Yukio Shimizu, Institute of Space and Astronautical Science of Japan Aerospace Exploration Agency, Sagamihara 229-8510, Japan; Naoki Terada, National Institute of Information and Communications Technology, Koganei 184-8795, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science of Japan Aerospace Exploration Agency, Sagamihara 229-8510, Japan; Daisuke Nakata, Department of Aeronautics and Astronautics, University of Tokyo, Tokyo 113-8656, Japan

2007-229: OPTOGALVANIC AND LASER-INDUCED FLUORESCENCE SPECTROSCOPY OF THE ZEEMAN EFFECT IN XENON, Timothy B. Smith, Wensheng Huang, Bailo B. Ngom, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48105, USA

2007-230: FUNDAMENTAL STUDY OF LASER MICRO PROPULSION USING POWERED-PROPELLANT; S. Yokoyama and H. Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; I Funaki and H. Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2007-231: OPTIMISATION AND ASSESSMENT OF THE TOTAL IMPULSE CAPABILITY OF THE T6 ION THRUSTER; Mr. N. C. Wallace and Dr. Michael Corbett, QinetiQ Ltd., Cody Technology Park, Farnborough, Hampshire, GU14 0LX, UK

2007-232: GEOMETRY AND ELECTRIC POWER EFFECTS ON SPECIFIC IMPULSE AND EFFICIENCY OF AN ARC-JET THRUSTER; A. Kaminska and A. Bialek, IEPE, Poznan University of Technology, Poxnan 60-965, Poland; M. Dudeck, ICARE Laboratory, OrlÃ©ans 45071 and University of Paris 6, Paris 75252, France

2007-233: A FULLY-INTEGRATED MICROFABRICATED EXTERNALLY-WETTED ELECTROSPRAY THRUSTER; B. Gassend, L. F. VelÃ¡squez-GarcÃa, A. I. Akinwande, and M. MartÃnez-SÃ¡nchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA

2007-234: PLUME DIVERGENCE IN THE HALL THRUSTER DUE TO PLASMA PRESSURE; Avi Cohen-Zur and Amnon Fruchtman, Holon Institute of Technology, Holon, 58102, Israel; Alon Gany, Technioin-Israel Institute of Technology, Haifa, 32000, Israel

2007-236: COMPARTISON OF THE THEORETICAL AND EXPERIMENTAL PERFORMANCE OF AN ANNULAR HELICON PLASMA SOURCE; Cengiz B. Akinli, Douglas D. Palmer, and Mitchell L. R. Walker II, Georgia Institute of Technology, Atlanta, GA, 30332, USA

2007-237: FUNDAMENTALS OF DISCHARGE INITIATION IN PULSED PLASMA THRUSTERS: THRESHOLD CRITERIA FOR UNDERVOLTAGE BREAKDOWN; James E. Cooley and Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08544, USA

2007-238: CAPILLARY DISCHARGE BASED PULSED PLASMA THRUSTERS; Jean-Luc Cambier, Air Force Research Lab, 10. E. Saturn Blvd. Edwards AFB, CA 93524, United States; Marcus Young and Leonid Pekker, ERC Inc., 10. E. Saturn Blvd, Edwards AFB, CA 93524, United States; Anthony Pancotti, University of Southern California, 854 W 36^th Place, RRB 101, Los Angeles, CA 90089, United States

2007-239: CURRENT AND PLASMA OSCILLATION INSPECT IN PPS-X000 HET THRUSTER – EMD APPROACH; Jacek Kurzyna, Karol Makowski, and Zbigniew Peradzynski, Institute of Fundamental Technological Research, Polish Academy of Sciences, Swietokrzyska 21, 00049 Warsaw, Poland; Alexey Lazurenko, Stephane Mazouffre, Giovanni Coduti, and Michel Dudeck, ICARE – CNRS, 1C Avenue de la Recherche Scientifique, 45071 OrlÃ©ans Cedex 2, France

2007-240: DEVELOPMENT OF THE ELECTRODELESS PLASMA THRUSTER AT HIGH POWER: INVESTIGATIONS ON THE MICROWAVE-PLASMA COUPLING; Geogory D. Emsellem, The Elwing Company, Wilmington, DE, 19801, USA; Serge Larigaldie, ONERA – Office National d’Etude et Recherche AÃ©ronautique, Palaiseau, 91120, France

2007-243: RESEARCH AND DEVELOPMENT ON COAXIAL PULSED PLASMA THRUSTER FOR SMALL SATELLITES; Masayuki Mukai, Yukiya Kamishima, Tsubasa Sasaki, Kouhei Shintani, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan; Takashi Wakizono, HI-SERVE Corporation, Akiruno, Tokyo, 190-0252, Japan; Mitsuteru Sugiki, Astro Research Corporation, Yokohama, Kanagawa, 190-0152, Japan

2007-244: PROJECTED LUNAR CARGO CAPABILITIES OF HIGH-POWER VASIMR PROPULSION; Tim W. Glover, Franklin R. Chang Diaz, and Andrew V. Ilin, Ad Astra Rocket Company, Houston, Texas, 77058, USA; Robert Vondra, P.O. Box 596, Wrightwood, California 92397, USA

2007-245: LASER-AUGMENTED MICRO-PULSEJET THRUSTER; Sou Eto and Hideyuki Horisawa, Tokai University, Hiratsuka-shi, Kanagawa, 259-1292, Japan; Itsuro Kimura, Professor Emeritus, University of Tokyo, Bunkyo-ku, Tokyo, 113-8856, Japan

2007-246: NEW WALL CONDUCTIVITY IN HALL THRUSTERS. CYLINDRICAL GEOMETRY EFFECT; K. Makowski, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warsaw 00-49, Poland; Z. Peradzynski, Faculty of Mathematics, Informatics and Mechanics, Warsaw University, Warsaw 02-097, Poland; M. Kolanowski, S. Barral, J. Kurzyna, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warsaw 00-049, Poland; M. Dudeck, Laboratoire d’AÃ©rothermique du CNRS, Orleans 45071, France

2007-247: CHARACTERIZATION OF HIGH FREQUENCY PLASMA OSCILLATIONS IN A HALL EFFECT THRUSTER; GÃ©rard Bonhomme, Nicolas Lemoine, and FrÃ©dÃ©ric Brochard, LPMIA, UMR 7040 CNRS-UniversitÃ© Henri PoincarÃ©, BP 239, F-54506 Vandoeuvre-lÃ©s-Nancy, France; Alexey Lazurenko, StÃ©phane Mazouffre, and Michel Dudeck, ICARE, CNRS, 1c Av. de la Recherche Scientifique, 45071 OrlÃ©ans, France

2007-250: MODELING OF HALL THRUSTER LIFETIME AND EROSION MECHANISMS; Shannon Y. Cheng and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA

2007-252: NEAR-FIELD LASER-INDUCED FLUORESCENCE VELOCIMETRY OF NEUTRAL XENON IN A 6-KW HALL THRUSTER PLUME; Timothy B. Smith, Wensheng Huang, Bryan M. Reid, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48105, USA

2007-253: A MEMS CNT-BASED NEUTRALIZER FOR MICRO-PROPULSION APPLICATIONS; Luis F. ValÃ¡squez-GarcÃa and Akintunde I. Akinwande, Massachusetts Institute of Technology, Cambridge, MA 02139, USA

2007-254: NUMERICAL SIMULATION OF THE ZEEMAN EFFECT FROM LASER-INDUCED FLUORESCENCE OF NEUTRAL XENON; Bailo B. Ngom, Timothy B. Smith, Wensheng Huang, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109

2007-255: EXPERIMENTS OF ION ACCELERATION IN A MAGNETIC NOZZLE FOR AN ADVANCED PLASMA THRUSTER; Tatsuya Hagiwara, Akira Ando, Yuji Kasashima, Kunihiko Hattori, and Masaaki Inutake, Department of Electrical Engineering, Graduate School of Engineering, Tohoku University, 6-6-05, Aoba-yama, Sendai, 980-8579, Japan

2007-256: EMITTER DEPLETION MEASUREMENT AND MODELING IN THE T5&T6 KAUFMAN-TYPE ION THRUSTERS; Ismat M. Ahmed Rudwan and N. C. Wallace, Space Division, QinetiQ Plc Ltd, Farnborough, Hampshire, GU14 0LX, UK; Michele Coletti and Stephen B. Gabriel, Astronautics Research Group, SES, Southampton University, Hampshire, SO15 1BJ, UK

2007-257: ENVIRONMENTAL CONSIDERATIONS FOR XENON ELECTRIC PROPULSION; Mark W. Crofton and Toby D. Hain, The Aerospace Corporation, Los Angeles, CA, 90009, U.S.A.

2007-258: THE ROLE OF THE ELECTRON ENERGY BALANCE IN HALL THRUSTER PLASMA INSTABILITIES; Zbigniew Peradzynski, Institute of Applied Mathematics and Mechanics, University of Warsaw, 02-097, Warsaw, Poland, Institute of Fundamental Technological Research, Polish Academy of Sciences, 00-049, Warwaw, Poland; Karol Makowski, Serge Barral, and Jacek Kurzyna, Institute of Fundamental Technological Research, Polish Academy of Sciences, Warsaw, 00-049, Poland; Michel Dudeck, ICARE-CNRS, 45071 Orleans Cedex 2, France

2007-260: IONIZATION EFFICIENCY IN ELECTRIC PROPULSION DEVICES; Jerry L. Ross and Lyon B. King, Michigan Technological University, Houghton, MI

2007-261: THEORETICAL ANALYSIS OF THE INFLUENCE OF THE POWER SUPPLY ON BREATHING OSCILLATIONS IN HALL THRUSTERS; S. Barral, Instytut Podstawowych ProblemÃ³w Techniki – PAN, Warsaw, 00049, Poland

2007-262: DEVELOPMENT HISTORY AND CURRENT STATUS OF DC-TYPE ION ENGINES AT JAXA; Shoji Kitamura, Kenichi Kajiwara, Hiroshi Nagano, and Yukio Hayakawa, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2007-264: EXPERIMENTAL INVESTIGATION OF INFLUENCING FACTORS FOR RELIABLE STARTUP AND STEADY WORK OF 100W MICROWAVE PLASMA THRUSTER; Xia Guang-qing, Mao Gen-wang, Yang Juan, and Chen Mao-lin, Northwestern Polytechnical University, National Key Laboratory of Combustion, Flow and Thermo-Structure, Xi’an, Shaanxi Province, 710072, P. R. China

2007-265: XIPS ION THRUSTER GRID EROSION ASSESSMENT FOR DEEP SPACE MISSIONS; Richard E. Wirz, John R. Anderson, Dan Goebel, and Ira Katz, California Institute of Technology, Jet Propulsion Laboratory, Pasadena, CA, 91109, USA

2007-266: RF PLASMA CATHODE-NEUTRALIZER FOR SPACE APPLICATIONS; Valery Godyak, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ 08543, USA

2007-267: BPT-4000 HALL THRUSTER DISCHARGE CHAMBER EROSION MODEL COMPARISON WITH QUALIFICATION LIFE TEST DATA; Richard R. Hofer, Ioannis G. Mikellides, Ira Katz, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007-268: ABSOLUTE EMISSION FROM THE MID-INFRARED TO THE EXTREME ULTRAVIOLET FROM A PULSED PLASMA THRUSTER (PPT); Edward J. Beiting, Jun Qian, Ray W. Russell, and James E. Pollard, The Aerospace Corporation, Los Angeles, CA 90009; Will Caven and Ron Corey, Space Systems/Loral, Palo Alto, CA 94303

2007-269: ELECTROMAGNETIC EMISSIONS FROM DC TO 17 GHZ FROM A PULSED PLASMA THRUSTER (PPT); Michael L. Garrett and Edward J. Beiting, The Aerospace Corporation, Los Angeles, CA 90009; Will Caven and Ron Cory, Space Systems/Loral, Palo Alto, CA 94303

2007-270: COMPARATIVE HIGH-CURRENT-DENSITY EMITTERS POISONING OF HOLLOW CATHODES ELECTRIC PROPULSION; A. Taran, A. Loyan, and D. Voronovich, National Aerospace University “Kharkiv Aviation Institute”, Kharkiv, 61070, Ukraine

2007-271: QUALIFICATION OF COMMERCIAL ELECTRIC PROPULSION SYSTEMS FOR DEEP SPACE MISSIONS; Thomas M. Randolph, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, 91109, U.S.A.

2007-272: DEVELOPMENT STATUS OF THE NONAMBIPOLAR ELECTRON SOURCE; Ben Longmier and Noah Hershkowitz, University of Wisconsin – Madison, Madison, WI 53706

2007-274: SOLELY EP BASED ORBIT CONTROL SYSTEM ON SMALL GEO SATELLITE; H. LÃ¼bberstedt, Th. Miesner, and A. Winkler, OHB-System AG, D-28359 Bremen, Germany; P. Rathsman and J. Kugelberg, Swedish Space Corporation, SE-17104 Solna, Sweden

2007-275: OVERVIEW OF ELECTRIC PROPULSION ACTIVITY IN RUSSIA; Semenkin A. V., Central Research Institute of Machine Building (TSNIIMASH), Pionerskaya 4, Korolev, Moscow region, Russia 141070; Testoedov N. A., Yakimov E. N., Ermoshkin Yu. M., Volkov D. V., Yukseev S. V., Scientific and Production Association of Applied Mechanic (NPO PM), Krasnoyarsk; Sevast’yanov N. N., Verkhoturov V. I., Romanov S. Yu., Samitov R. M., Borisenko A. A., and Ostrovsky V. G., Rocket and Space Corporation “Energia” (RSC “Energia”), Korolev city, Moscow, region; Makridenko L. A., Volkova S. N., and Khodnenko B. P., All-Russia Scientific Research Institute of Electro-Mechanic (VNIIEM), Moscow; Poletaev B. I., Lyannoy E. G., Romanov A. V., and Pavlov A. Yu, Design Bureau “Arsenal”, Saint-Petersburg; Partola I. S. and Kuznetsov S. V., State Space Scientific and Production Center named after M. V. Khrunichev, Moscow; Resh G. F., Arakin M. V., Savosin G. V., Prokhorchuk Yu. A., Maksimov I.I., Lizunov A. A., Kabanov B. A., Scientific and Production Association of Machine Building (NPO MASH), Reutov city, Moscow, region; Murashko V. M., Experimental Design Bureau “Fakel”, (EDB “Fakel”), Kaliningrad; Popov G. A., Kim V. P., Obukhov V. A, and Antropov N. N., Research Institute of Applied Mechanic and Eletrodynamics, (RIAME) Moscow; Morozov A. I. (Kurchatov Institute), Bugrova A. I., Sigov A. S., Lipatov A. S., and Kharchevnicov V. K., Moscow Institute of Radio Electronic and Automatic (MIREA), Moscoq; Lukyachenko V. I., Semenkin A. V., Garkusha V. I., and Tverdokhlebova E. M., Central Research Institute of Machine Building, (TSNIIMASH), Korolev city, Moscow region

2007-276: ENVIRONMENTAL TESTING OF THE NEXT PM1R ION ENGINER; John Steven Snyder and John R. Anderson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109; Jonathan L. Van Noord and George C. Soulas, NASA Glenn Research Center, Cleveland, OH, 44135

2007-277: PLASMA POTENTIAL BEHAVIOR AND PLUME MODE TRANSITIONS IN HOLLOW CATHODE DISCHARGES; Dan M. Goebel, Kristina K. Jameson, Ira Katz, and Ioannis G. Mikellides, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007-278: CATHODE COUPLING IN HALL THRUSTERS; Kristina K. Jameson, Dan M. Goebel, Richard R. Hofer, and Ron M. Watkins, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007-279: PROPELLANT THROUGHPUT CAPABILITY OF THE DAWN ION THRUSTERS; John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91101, USA

2007-280: MULTIIPLE BARE TETHERS FOR ELECTRODYNAMIC TETHER PROPULSION; Teppei Ikeda, Yasuhiro Nakamura, Yoshiki Yamagiwa, and Hirotaka Otsu, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan; Satomi Kawamoto, Yasushi Ohkawa, and Atsushi Nakajima, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2007-281: SIMULATION OF ARGON PLASMA FLOWS IN MAGNETOPLASMADYNAMIC THRUSTERS; M. H. Moghimi and M. Farshchi, Aerospace Engineering Department, Sharif University of Technology, Tehran, Iran

2007-283: POWER CONTROL UNIT FOR ÂµN FEEP PROPULSION SUBSYSTEM; Luca Ceruti, Andrea Antimiani, and Aldo Polli, Galileo Avoinica S.p.A. Space Business Unit, Via Montefeltro, 8-20156 Milan, Italy

2007-284: FIELD EMISSION ELECTRIC THRUSTER OPTICAL DIAGNOSTICS BASED ON AN INDIUM COLLISIONAL-RADIATIVE MODEL; Konstantinos Katsonis, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, UniversitÃ© Paris-sud, 91405 Orsay, France; J. Bonnet and D. Packan, ONERA, 91761 Palaiseau, France; Marguerite Cornille, LUTH, Observatoire de Paris, CNRS, Univ. Paris Diderot, Place Jules Janssen, 92190 Meudon, France; Chloe Berenguer and Abdoulaziz Ndiaye, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, UniversitÃ© Paris-sud, 91405 Orsay, France

2007-285: A XENON COLLISIONAL-RADIATIVE MODEL FOR PLASMA THRUSTER OPTICAL DIAGNOSTICS AND MODELING; Konstantinos Katsonis and Chloe Berenguer, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, UniversitÃ© Paris-sud, 91405 Orsay, France; J. Bonnet and D. Packan, ONERA, 91761 Palaiseau, France; R.E.H. Clark, NDS, IAEA, Wagramerstr. 5, A-1400 Vienna, Austria; Marguerite Cornille, LUTH, Observatoire de Paris, CNRS, Univ. Paris Diderot, Place Jules Janssen, 92190 Meudon, France; Gilles Maynard, Laboratoire de Physique des Gaz et des Plasmas, UMR 8578, UniversitÃ© Paris-sud, 91405 Orsay, France

2007-286: PRELIMINARY EXPERIMENTAL MEASUREMENTS FOR A GALLIUM ELECTROMAGNETIC (GEM) THRUSTER; Robert E. Thomas, Rodney L. Burton, and Nick G. Glumac, University of Illinois, Urbana, IL, 61801; Kurt A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL 35812

2007-287: ELECTRIC PROPULSION PERFORMANCE FROM GEO-TRANSFER TO GEOSYNCHRONOUS ORBITS; John W. Dankanich and Gordon R. Woodcock, Gray Research Inc., Cleveland, OH, 44135, U.S.A.

2007-288: FLIGHT HARDWARE DEVELOPMENT OF COLLOID MICROTHRUSTER TECHNOLOGY FOR THE SPACE TECHNOLOGY 7 AND LISA MISSIONS; John K. Ziemer, Thomas M. Randolph, and Manuel Gamero-CastaÃ±o, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109; Vlad Hruby, William Connolly, Nathaniel Demmons, Eric Ehrbar, Roy Martin, and Tom Roy, Douglas Spence, Jurg Zwahlen, Busek Co., Natick, MA 01760

2007-290: A PULSED PLASMA THRUSTER USING MERCURY PROPELLANT: A LATE-1960S PROJECT AT THE ROYAL AEROSPACE ESTABLISHMENT, FARNBOROUGH; David G. Fearn, EP Solutions, 23 Bowenhurst Road, Church Crookham, Fleet, Hants, GU62 6HS, UK

2007-291: HALL THRUSTER ELECTRON MOBILITY INVESTIGATION USING FULL 3D MONTE CARLO TRAJECTORY SIMULATIONS; Darren A. Alman, Joshua L. Rovey, Robert A. Stubbers, and Brian E. Jurczyk, Starfire Industries LLC, Champaign, IL, 61820

2007-293: VERIFICATION OF ANALYSIS TOOL OF THRUSTER PLUME INTERACTIONS FOR SPACECRAFT; Satoshi Hosoda, Japan Aerospace Exploration Agency, Sagamihara, Kangagawa, 229-8510, Japan; Naomi Kurahara and Mengu Cho, Kyushu Institute of Technology, Kitakyushu, Fukuoka, 804-8550, Japan; Takanobu Muranaka and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kangagawa, 229-8510, Japan; Hiroko O. Ueda, Kiyokazu Koga, and Tateo Goka, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2007-294: INNOVATIVE ARCHITECTURES DEVELOPED FOR THE POWER SUPPLY CONTROL UNITS OF THE ION THRUSTERS FOR INCOMING PROGRAMS; C. Tato, F. de la Cruz, and J. Palencia, Electronic Engineer, Madrid – Tres Cantos 28760 – Spain

2007-295: POWER CONTROL UNIT FOR ION PROPULSION ASSEMBLY IN GOCE PROGRAM; C. Tato, F. de la Cruz, and J. Palencia, Electronic Engineer, Madrid – Tres Cantos 28760 – Spain

2007-300: HIGH FREQUENCY BURST PULSED PLASMA THRUSTER RESEARCH AT THE UNIVERSITY OF SOUTHAMPTON; R. I. Marques and S. B. Gabriel, University of Southampton, SO17 1BJ, United Kingdom; F. de S. Costa, Instituto Nacional de Pesquisas Espaciais, Cachoeira Paulista, SP, 12630-000, Brazil

2007-301: THALES ALENIA SPACE EXPERIENCE ON PLASMA PROPULSION; Michael Lyszyk and Laurent Lecardonnel, Thales Alenia Space, Cannes, 06150, France

2007-302: IONS FORMATION DENSITY DISTRIBUTION IN SPT ATON CHANNEL; M. V. Kozintseva, G. E. Bugrov, and I. A. Tarelkin, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, Russia

2007-304: POWER CONSTRAINED ELECTRIC PROPULSION MISSIONS TO THE OUTER PLANETS; K. Geurts, C. Casaregola, P. Pergola, and M. Andrenucci, ALTA S.p.A., Via Gherardesca 5, 56121, Pisa, Italy

2007-305: THREE BODY INVARIANT MANIFOLD TRANSITION WITH ELECTRIC PROPULSION; P. Pergola, K. Geurts, C. Casaregola, and M. Andrenucci, ALTA S.p.A., Via Gherardesca 5, 56121, Pisa, Italy

2007-306: A VEGA DEDICATED ELECTRIC PROPULSION TRANSFER MODULE TO THE MOON; C. Casaregola, K. Geurts, P. Pergola, L. Biagioni, M. Andrenucci, Alta S.p.A., Pisa, 56121, Italy

2007-307: ANALYSIS OF HALL-EFFECT THRUSTERS APPLICATION TO FORMATION FLYING AND DRAG COMPENSATION; P. Rossetti, Alta S.p.A., Pisa, 56121, Italia; D. Valentian, Snecma, Vernon, 27208, France

2007-308: NUMERICAL ANALYSIS OF THE ACCELERATION PROCESS IN CLUSTER FRAGMENTATION ION SOURCES; P. Rossetti, F. Paganucci, and F. Nania, Alta SpA, Pisa, 56121, Italia; C. R. Gebhardt, Clustec Gmbh, Munchen, 81475, Germany; H. SchrÃ¶der, Max-Planck-Institut fÃ¼r Quantenoptik, Garching, D-85748, Germany

2007-309: REVIEW OF RF PLASMA THRUSTER DEVELOPMENT; Ivana Hrbud, G. Elijah Kemp, Allen H. Yan, and Jacob G. Gedrimas, Purdue University, West Lafayette, IN 47907, USA

2007-311: HIGH POWER THRUSTERS DESIGN OPTIONS; Tommaso Misuri, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Francesco Battista, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Christian Barbieri, Graduate Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Enrico Alessio De Marco, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Mariano Andrenucci, Professor of Electric Propulsion, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy, Chairman of ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-313: A REVIEW OF THE HALL THRUSTER SCALING METHODOLOGY; Francesco Battista, Research Engineer, CIRA Italian Aerospace Research Centre, Capua, 83100, Italy, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Enrico Alessio De Marco and Tommaso Misuri, Ph.D. Students, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Mariano Andrenucci, Professor of Electric Propulsion, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy, Chairman of ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-316: STUDY ON PLASMA LENS OF HALL THRUSTERS IN DIFFERENT OPERATING MODES; Jie Li, Da-Ren Yu, and Yong Li, harbin Institute of Technology, Harbin, Heilongjiang, 150001, China

2007-317: NUMERICAL SIMULATION FOR MAGNETIC MIRROR EFFECT ON ELECTRON MOVEMENT IN A HALL THRUSTER; Daren Yu, Hui Lu, and Haiyang Fu, HIT Plasma Propulsion Laboratory, Harbin, Heilongjiang, 15001, China

2007-319: VICTOR B. TIKHONOV’S MHD CHANNEL THEORY: A REVIEW; Tommaso Misuri, Ph.D. Student, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy; Mariano Andrenucci, Professor of Electric Propulsion, Dipartimento di Ingegneria Aerospaziale, UniversitÃ¡ di Pisa, Pisa, 56122, Italy, Chairman of ALTA SpA, Ospedaletto, Pisa, 56121, Italy

2007-320: EXPERIMENTAL CHARACTERIZATION OF THE HT-100 HALL THRUSTER IN TWIN ENGINE CLUSTER CONFIGURATION; M. Saverdi, M. Signori, and L. Biagioni, Alta SpA, via A. Gherardesca 5, I-56014 Ospedaletto (PI), Italy

2007-321: THE IV10 SPACE SIMULATOR FOR HIGH POWER ELECTRIC PROPULSION TESTING: PERFORMANCE IMPROVEMENTS AND OPERATION STATUS; M. Saverdi, M. Signori, L. Milaneschi, U. Cesari, and L. Biagioni, Alta SpA, via A. Gherardesca 5, I-56014 Ospedaletto (PI), Italy

2007-325: VALIDATION STATUS OF THE PICPLUS PLUME SIMULATION AND SPACECRAFT ITNERACTION TOOLS: LESSON LEARNT FROM FLIGHT AND GROUND EXPERIMENTAL DATA; A. Passaro, A. Vicini, and F. Nania, Alta SpA, Pisa, 56121, Italy

2007-328: CAPILLARY DISCHARGE BASED PULSED PLASMA THRUSTERS; Jean-Luc Cambier, Air Force Research Lab, 10. E. Saturn Blvd. Edwards AFB, CA 93524, United States; Marcus Young and Leonid Pekker, ERC Inc., 10. E. Saturn Blvd. Edwards AFB, CA 93524, United States; Anthony Pancotti, University of Southern California, 854 W. 36^th Place, RRB 101, Los Angeles, CA 90089, United States

2007-330: EXPERIMENTAL ASSESSMENT OF A PASSIVE METHOD FOR MHD INSTABILITY SUPPRESSION IN MPD THRUSTERS; F. Paganucci and M. Andrenucci, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy, Department of Aerospace Engineering, University of Pisa, via Caruso, 56122 Pisa, Italy; P. Rossetti and M. De Tata, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy; V. Antoni, R. Cavazzana, E. Martines, G. Serianni, and F. Tarallo, Consorzio RFX, Associazione Euratom-Enea sulla Fusione, corso Stati Uniti 4, 35127 Padova, Italy

2007-331: MAGNETIC FLUCTUATIONS IN A MPD THRUSTER WITH PASSIVE SYSTEMS FOR THE CONTROL OF MHD INSTABILITIES; M. Zuin, V. Antoni, R. Cavazzana, E. Matines, G. Serianni, and F. Tarallo, Consorzio RFX, Associazione Euratom-Enea Sulla Fusione, corso Stati Uniti 4, 35127 Padova, Italy; M. Andrenucci and F. Paganucci, Alta/Centrospazio, via A. Gherardesca 5, 56014 Pisa, Italy, Department of Aerospace Engineering, University of Pisa, via Caruso, 56122 Pisa, Italy

2007-334: AEDC PLUME MEASUREMENTS USING BI-DIRECTIONAL ION FLUX PROBES; Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08543, USA; Trevor Moeller, University of Tennessee Space Institute, Tullahoma, TN, 37355, USA; James Szabo, Busek Co., Inc., Natick, MA, 01760, USA

2007-335: PERFORMANCE AND PLASMA CHARACTERISTICS OF A CUSP AND DIVERGENT-NOZZLE APPLIED-MAGNETIC-FIELD MPD THRUSTER; Hirokazu Tahara and Yoichi Kagaya, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-336: INFLUENCES OF MAGNETIC FIELD TOPOGRAPHY AND DISCHARGE CHANNEL STRUCTURE ON PERFORMANCE OF ANODE-LAYER HALL THRUSTERS; Seiro Yuge, Yoshihiro Kuwamura, and Hirokazu Tahara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-337: PERFORMANCE CHARACTERISTICS OF ELECTROTHERMAL PULSED PLASMA THRUSTERS WITH INSULATOR-ROD-ARRANGED CAVITIES AND TEFLON-ALTERNATIVE PROPELLANTS; Hirokazu Tahara, Toshiaki Edamitsu, and Hirokazu Sugihara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-338: EFFECTS OF MAGNETIC FIELD CONFIGURATION AND ELECTRICALLY-FLOATING METAL PLATES IN HALL THRUSTERS WITH CIRCULAR CROSS-SECTIONAL DISCHARGE CHAMBERS; Hirokazu Tahara and Atsushi Shirasaki, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-339: RESEARCH AND DEVELOPMENT OF COMPACT LASER ABLATIVE THRUSTERS FOR SMALL SATELLITES; Hirokazu Tahara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-340: GROUND-BASED EXPERIMENT OF CURRENT COLLECTION TO BARE TETHER IN HIGH-SPEED MAGNETIZED PLASMA; Hirokazu Tahara, Osaka Institute of Technology, Asahi, Osaka 535-8585, Japan

2007-343: A 3D MODEL OF ELECTRON DYNAMICS NEAR THE OUTLET SECTION OF SPT THRUSTER; Grigory Toropov, Moscow Aviation Institute (State Technical University) MAI, Engineering Plasma Computational Laboratory (EPCLab), 24b-120, Zalineynaya str., Vologda, 160010, Russia; Sergey Khartov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2007-346: CONTINUING DEVELOPMENT OF THE PROPORTIONAL FLOW CONTROL VALVE (PFCV) FOR ELECTRIC PROPULSION SYSTEMS; David M. Pehrson, Moog Inc., Space and Defense Group, East Aurora, NY, 14052, USA

2007-347: DEVELOPMENT OF NEUTRALIZER WITH CARBON NANOTUBE CATHODE FOR SMALL SCALE ION ENGINER; Yoshiyuki Takao, Akihiro Kugimiya, and Shinobu Nagai, Oita National College of Technology, 1666 Maki, Oita City, 870-0152, Japan; Naoji Yamamoto and Hideki Nakashima, Kyushu University, Kasuga, 816-8580, Japan

2007-352: ELECTRIC SAIL PROPULSION MODELING AND MISSION ANALYSIS; Pekka Janhunen, Finnish Meteorological Institute, FIN-00101 Helsinki, Finland; Giovanni Mengali and Alessandro A. Quarta, University of Pisa, I-56122 Pisa, Italy

2007-353: APPLICATION OF A VARIATIONAL MHD PRINCIPLE TO THE STUDY OF PLASMA THRUSTERS; Tommaso Andreussi, Scuola Normale Superiore, Pisa, 56100, Italy; Francesco Pegoraro, Phys. Dept., University of Pisa, Pisa, 56127, Italy

2007-354: ELECTRIC PROPULSION REQUIREMENTS AND MISSION ANALYSIS UNDER NASA’S IN-SPACE PROPULSION TECHNOLOGY PROJECT; Leonard A. Dudzinski and Eric J. Pencil, NASA Glenn Research Center, Cleveland, OH 44135, USA; John W. Dankanich, Gray Research, Inc., Cleveland, OH 44135, USA

2007-356: INDIRECT OPTIMIZATION METHOD FOR LOW-THRUST INTERPLANETARY TRAJECTORIES; Lorenzo Casalino, Guido Colasurdo, and Matteo Rosa Sentinella, Politecnico di Torino, Turin, 10129, Italy

2007-357: NUCLEAR ACTIVIATION ENHANCED MHD AND MPD THRUSTER; Samim Anghaie, Innovative Nuclear Space Power & Propulsion Institute (INSPI), University of Florida, Gainesville, FL 32611-8300; Angelo Ferrair, New Era Technology, Inc. (NeTecH) 3720 NW 43^rd Street, Suite 105, Gainesville, FL 32606

2007-358: ADVANCING JAPANESE ELECTRIC PROPULSION; Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, 299-8510, Japan; Kimiya Komurasaki, The University of Tokyo, Kashiwa, 277-8561, Japan

2007-359: THE NEW NASA-STD-4005 AND NASA-HDBK-4006, ESSENTIALS FOR DIRECT-DRIVE SOLAR ELECTRIC PROPULSION; Dale C. Ferguson, NASA Marshall Space Flight Center, Huntsville, Alabama, 35812, USA

2007-360: RELATIONSHIP BETWEEN ANODE SPOTS AND ONSET VOLTAGE HASH IN QUASI-STEADY MAGNETOPLASMADYNAMIC THRUSTERS; Luke Uribarri and E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton Unviersity, Princeton, NJ, 08544

2007-361: UKRAINIAN SPT-20 HALL EFFECT THRUSTER: ANALYSIS OF THE PLUME BY OPTICAL EMISSION SPECTROSCOPY; D. Pagnon, Laboratoire de Physique des Gaz et des Plasmas, Orsay 91405, France; S. Pellerin Laboratoire d’Analyse Spectroscopique et d’EnergÃ©tique de Plasmas, Bourges 18028, France; M. Dudeck, Laboratoire ICARE, OrlÃ©ans 45071, France; A. V. Loyan, T. A. Maksymenko, and N. N. Koshelev, National Aerospace University “KhAI”, 61070 Kharkov, Ukraine

2007-362: SPIS MODELING OF FEEP THRUSTERS FOR LISA PATHFINDER; Bjarne Adnersson, Davide Nicolini, and Eric Gengembre, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2007-363: LISA PATHFINDER FIELD EMISSION THRUSTER SYSTEM DEVELOPMENT PROGRAM; Davide Nicolini, European Space Agency, ESTEC, Noordwijk, 2201 AZ, The Netherlands

2007-364: ANALYSIS OF RF THRUSTERS WITH TOPICA AND A GLOBAL SYSTEM-LEVEL MODEL; Vito Lancellotti, Giuseppe Vecchi, and Riccardo Maggiora, Dipartimento di Elettronica, Politecnico di Torino, Torino, I-10129, Italy; Daniele Pavarin and Simone Rocca, CISAS G. Colombo, Padova, I-35131 Italy; Cristina Bramanti, Advanced Concepts Team, ESA-ESTEC, Noordwijk, The Netherlands

2007-365: ION CURRENT IN HALL THRUSTERS; Ira Katz, Richard R. Hofer, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2007 FILE DIRECTORY

IEPC-2007-001.pdf 03-Sep-2007 02:38 2.7M

IEPC-2007-002.pdf 01-Sep-2007 19:39 2.9M

IEPC-2007-004.pdf 01-Sep-2007 19:31 809K

IEPC-2007-005.pdf 02-Sep-2007 10:11 2.1M

IEPC-2007-006.pdf 29-Aug-2007 10:04 588K

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IEPC-2007-142.pdf 04-Sep-2007 15:05 1.6M

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IEPC-2007-154.pdf 30-Aug-2007 12:57 1.5M

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IEPC-2007-157.pdf 02-Sep-2007 20:10 378K

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IEPC-2007-164.pdf 06-Sep-2007 12:09 1.7M

IEPC-2007-165.pdf 06-Sep-2007 07:35 2.8M

IEPC-2007-166.pdf 31-Aug-2007 23:15 2.6M

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IEPC-2007-168.pdf 02-Sep-2007 22:05 1.4M

IEPC-2007-169.pdf 02-Sep-2007 20:22 278K

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IEPC-2007-181.pdf 02-Sep-2007 21:31 798K

IEPC-2007-185.pdf 01-Sep-2007 23:27 255K

IEPC-2007-186.pdf 05-Sep-2007 09:38 1.8M

IEPC-2007-187.pdf 05-Sep-2007 11:26 319K

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IEPC-2007-190.pdf 03-Sep-2007 05:11 414K

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IEPC-2007-193.pdf 02-Sep-2007 13:43 1.9M

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IEPC-2007-196.pdf 05-Sep-2007 01:37 1.6M

IEPC-2007-197.pdf 02-Sep-2007 05:03 1.1M

IEPC-2007-199.pdf 01-Sep-2007 16:40 917K

IEPC-2007-200.pdf 06-Sep-2007 16:56 817K

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IEPC-2007-202.pdf 04-Sep-2007 01:55 1.0M

IEPC-2007-203.pdf 22-Aug-2007 02:39 2.3M

IEPC-2007-204.pdf 30-Aug-2007 17:26 284K

IEPC-2007-205.pdf 03-Sep-2007 05:13 303K

IEPC-2007-206.pdf 03-Sep-2007 14:28 1.2M

IEPC-2007-207.pdf 03-Sep-2007 01:39 1.2M

IEPC-2007-209.pdf 03-Sep-2007 05:00 415K

IEPC-2007-210.pdf 02-Sep-2007 19:06 1.4M

IEPC-2007-211.pdf 02-Sep-2007 16:25 384K

IEPC-2007-212.pdf 09-Sep-2007 14:08 330K

IEPC-2007-213.pdf 05-Sep-2007 22:51 1.4M

IEPC-2007-214.pdf 03-Sep-2007 14:43 325K

IEPC-2007-215.pdf 02-Sep-2007 23:58 1.2M

IEPC-2007-217.pdf 01-Sep-2007 21:58 1.9M

IEPC-2007-218.pdf 03-Sep-2007 04:55 372K

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IEPC-2007-220.pdf 01-Sep-2007 23:49 2.1M

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IEPC-2007-226.pdf 03-Sep-2007 03:45 1.8M

IEPC-2007-227.pdf 07-Sep-2007 00:06 579K

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IEPC-2007-229.pdf 03-Sep-2007 06:33 1.2M

IEPC-2007-230.pdf 05-Sep-2007 12:45 302K

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2009 INDEX

2009-001: PLASMA PROPULSION WITH ELECTRONEGATIVE GASES; Ane Aanesland, Lara Popelier, Gary Leray, and Pascal Chabert, Laboratoire de Physique des Plasmas, CNRS – Ecole Polytechnique, 91128 Palaiseau, France; StÃ©phane Mazouffre and Dennis Gerst, Institut de Combustion AÃ©rothermique RÃ©activitÃ© et Environnement, CNRS, 45071 Olreans, France

2009-002: ACCELERATION OF A FOCUSED PLASMA JET IN A DIVERGENT MAGNETIC NOZZLE; E. Ahedo and M. Merino Universidad PolitÃ©cnica de Madrid, 28040 Madrid, Spain

2009-006: PRELIMINARY EXPERIMENTS FOR DEMONSTRATING MAGNETIC THRUST CHAMBER CONCEPT IN LASER FUSION ROCKET; A. Maeno, T. Hanaya, N. Yamamoto, and H. Nakashima, Kyushu University, Kasuya, Fukuoka, 816-8580, Japan; S. Fujioka, A. Sunahara, and T. Johzaki, Osaka University, Suita, Osaka, Japan; Y. Mori, The Graduate School for the Creation of New Photonics Industries, Hamamatsu, Shizuoka, Japan

2009-007: A PRELIMINARY STUDY OF MARS AIR-BREATHING ELECTRIC PROPULSION; Yoshinori Nakayama, Department of Aerospace Engineering, National Defense Academy, Yokosuka, Japan

2009-009: FLUCTUATION OF MAGNETOSPHERE IN SCALE-MODEL EXPERIMENT OF MAGNETIC SAIL; Yuya Oshio and Kazuma Ueno, Graduate University for Advanced Studies, Sagamihara, Kanagawa, 229-8510, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2009-010: EXPERIMENTS ON CONTACT CHARGING FOR AN ELECTROSTATIC MICROPARTICLE THRUSTER; Thomas Trottenberg, Viktor Schneider, and Holger Kersten, IEAP, Christian-Albrechts-UniversitÃ¤t zu Kiel, D-24118 Kiel, Germany

2009-011: THRUST CHARACTERISTICS OF PURE MAGNETIC SAIL IN LABORATORY EXPERIMENT; Kazuma Ueno, The Graduate University for Advanced Studies, Sagamihara, Kanagawa, 229-8510, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Yuya Oshio, The Graduate University for Advanced Studies, Sagamihara, Kanagawa, 229-8510, Japan; Hideyuki Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Hiroshi Yamakawa, Kyoto University, Uji, Kyoto, 611-0011, Japan

2009-013: NEUTRALISER FOR FEEPS: REVIEW ON THE DEVELOPMENT STATUS; Marco Capacci, Giovanni Matticari, and Maurizio Materassi, Thales Alenia Space Italia, Florence Site, 50013 Campi Bizencio, Italy; Davide Nicolini and Pierre-Etienne Frigot, The European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

2009-015: MICROWAVE CATHODE FOR AIR BREATHING ELECTRIC PROPULSION; Kevin D. Diamant, The Aerospace Corporation, Los Angeles, CA, 90009, USA

2009-016: COMPARISON OF HOLLOW CATHODE DISCHARGE PLASMA CONFIGURATIONS; Casey C. Farnell and John D. Williams, Electric Propulsion and Plasma Engineering Laboratory, Colorado State University, Fort Collins, CO 80523, USA; Cody C. Farnell, Plasma Controls, LLC, Fort Collins, CO, 80526, USA

2009-018: SIMULATION OF WORK PROCESSES IN LOW POWER HALL THRUSTER; A. V. Loyan, S. S. Levin, and Y u. K. Chernyshev, National Aerospace University “KhAI”, 61070 Kharkiv, Ukraine

2009-020: NEUTRALIZER HOLLOW CATHODE SIMULATIONS AND COMPARISONS WITH GROUND TEST DATA; Ioannis G. Mikellides, John Steven Snyder, Dan M. Goebel, and Ira Katz, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109; Daniel A. Herman, ASRC Aerospace Corporation, Cleveland, OH, 44135

2009-021: OPERATIONAL CHARACTERISTICS OF A MICROWAVE DISCHARGE NEUTRALIZER FOR THE ECR ION THRUSTER Âµ20; Kazutaka Nishiyama, Satoshi Hosoda, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency/Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 229-8510, Japan; Yasuhiro Yoyoda, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan

2009-022: ENDURANCE TESTS OF GRAPHITE ORIFICED HOLLOW CATHODES; Yasushi Ohkawa, Yukio Hayakawa, Hideki Yoshida, Katsuhiro Miyazaki, and Shoji Kitamura, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; Hiroshi Nagano and Kenichi Kajiwara, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505, Japan

2009-024: A PARAMETRIC STUDY OF ELECTRON EXTRACTION FROM A LOW FREQUENCY INDUCTIVELY COUPLED RF-PLASMA SOURCE; Yevgeny Raitses, Jennifer K. Hendryx, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ 08540, USA

2009-025: HOLLOW CATHODES FOR 100-KW MPD THRUSTERS; M. Cherkasova and V. Obukhov, RIAME – MAI, Russia; M. De Tata, F. Paganucci, P. Rossetti, and M. Andrenucci, Alta SpA, Italyl

2009-026: HOLLOW CATHODE DISCHARGE INITIATION AND FAST STARTING CATHODE; Binyamin Rubin and John D. Williams, Department of Mechanical Engineering, Colorado State University, Fort Collins, CO 80523

2009-027: RESEARCH AND DEVELOPMENT ON INDUCTIVELY COUPLED PLASMA CATHODE FOR ION ENGINES; Hiroki Watanabe, Takuji Okuma, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2009-028: THEORETICAL AND EXPERIMENTAL INVESTIGATION OF MICROHOLLOW CATHODE DISCHARGE FOR THE APPLICATION TO MICRO PLASMA THRUSTERS; XIA Guangqing, School of Aeronautics and Astronautics, Faculty of Vehicle Engineering and Mechanics, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian, 116024, China; MAO Genwang and CHEN Maolin, School of Astronautics, Northwestern Polytechnical University, Xi’an, 710072, China; WU Chuijie, School of Aeronautics and Astronautics, Dalian University of Technology, Dalian, 116024, China

2009-029: COLLISIONAL-RADIATIVE MODEL FOR LOW TEMPERATURE NE PLASMAS; ChloÃ© Berenguer and Konstantinos Katsonis, Centre de DonnÃ©es Atomiques GAPHYOR, Lab. de Physique des Gas et des Plasmas, UMR 8578, UniversitÃ© Paris-sud 91405 Orsay, France; Samuel Cohen and Pericles Tsekeris, Physics Department, University of Ioannina, GR-45110 Ioannina, Greece; Marguerite Cornille, LUTH, Observatoire de Paris, CNRS, Univ. Paris Diderot, Place Jules Janssen, 92190 Meudon, France

2009-030: EVALUATION OF PLUME DIVERGENCE AND FACILITY EFFECTS ON FAR-FIELD FARADAY PROBE CURRENT DENSITY PROFILES; Daniel L. Brown, Air Force Research Laboratory, Edwards AFB, CA, 93524, USA; Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA

2009-031: REMOTE DIAGNOSTIC MEASUREMENTS OF HALL THRUSTER PLUMES; Casey C. Farnell, Plasma Controls, LLC, Fort Collins, CO, 80526, USA; Daniel L. Brown, Air Force Research Laboratory, Edwards AFB, CA, 93524, USA; Garret M. Willis and Richard D. Branam, Air Force Institute of Technology, Wright-Patterson AFB, OH, 45433, USA; John E. Williams, Electric Propulsion and Plasma Engineering Laboratory, Colorado State University, Fort Collins, CO 80523, USA

2009-032: EXPERIMENTAL STUDY OF THE NEUTRALIZATION PROCESS IN FIELD-EMISSION ELECTRIC PROPULSION; Pierre-Etienne Frigot, Alexandra Bulit, Davide Nicolini, JosÃ© A. Gonzalez del Amo, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands; Marco Capacci, Thales Alenia Space Italia, Florence Site, 50013 Campi Bizencio, Italy

2009-034: LASER-INDUCED FLUORESCENCE VELOCITY MEASUREMENTS OF A LOW POWER CYLINDRICAL HALL THRUSTER; Natalia A. MacDonald and Mark A. Cappelli, Stanford Plasma Physics Laboratory, Stanford University, Stanford, CA 94305; William A. Hargus Jr., Spacecraft Propulsion Branch, Air Force Research Laboratory, Edwards, AFB, CA 93524

2009-035: A SIMPLE ATOMIC SCHEME FOR AR THRUSTER MULTIDIMENSIONAL MODELING AND OPTICAL DIAGNOSTICS; Konstantinos Katsonis and ChloÃ© Berenguer, Centre de DonnÃ©s Atomiques GAPHYOR, Lab. de Physique des Gaz et des Plasmas, UMR 8578, UniversitÃ© Paris-sub 91405 Orsay, France; Marguerite Cornille, LUTH, Observatoire de Paris, CNRS, Univ. Paris Diderot, Place Jules Janssen, 92190 Meudon, France

2009-036: DEVELOPMENT OF A TELEMICROSCOPY DIAGNOSTIC APPARATUS AND EROSION MODELLING IN HALL EFFECT THRUSTERS; Tommaso Misuri, Andrea Milani, and Mariano Andrenucci, Alta Spa, Ospedaletto, Pisa, 56121, Italy

2009-037: TWO APPROACHES TO THE STUDYING OF A HALL THRUSTER DISCHARGE CHAMBER EROSION PROCESS; Sergey A. Oghienko and HatefDinparasti Saleh, National Aerospace University, “Kharkiv Aviation Institute”, 17 Chkalova str., Kharkiv, 61070, Ukraine; Andrey V. Khitko, Sergey N. Kulagin, and Alexandr N. Petrenko, National State University, 72 Gagarina str., Dnepropetrovsk, 49010, Ukraine

2009-041: PLASMA REFLECTOMETRY APPLIED TO PLUME DENSITY MEASUREMENTS OF ELECTRIC PROPULSION THRUSTERS; SÃ©rgio Mota, David P. Resendes, and Luis Cupido, Instituto de Plasmas e Fusao Nuclear/Instituto Superior TÃ©cnico (IPFN/IST), Av. Rovisco Pais 1, Lisbon, 1049, Portugal

2009-042: TOTAL AND DIFFERENTIAL SPUTTER YIELDS OF BORON NITRIDE MEASURED BY QUARTZ CRYSTAL MICROBALANCE; B. Rubin, J. L. Topper and A. P. Yalin, Colorado State University, Fort Collins, Colorado 80523, USA

2009-044: A NOVEL METHOD FOR THRUST MEASUREMENTS USING MICROPARTICLES; Viktor Schneider, Thomas Trottenberg, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

2009-047: HIGH DELTA V NANOSATELLITE MISSIONS USING A DIVERGING CUSPED FIELD THRUSTER; Ryan M. Daspit, Christopher J. Han, Paulo Lozano, and David Miller, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA

2009-048: ETS-VIII ION ENGINE AND ITS OPERATION ON ORBIT; Kenichi Kajiwara, Masafumi Ikeda, and Hiroki Kohata, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505; Toshiyuki Ozaki, Mitsubishi Electric Corporation, Kamakura, Kanagawa, 247-8520, Japan

2009-050: TEST RESULTS OF THE QUALIFICATION TESTS FOR THE IN-FEEP TECHNOLOGY FOR LISA PF; C. Scharlemann, A. Genovese, R. Schnitzer, N. Buldrini, P. Sattler, and M. Tajmar, Austrian Institute of Technology-AIT, 2444 Seibersdorf, Austria; R. Killinger, Astrium GmbH, D-74239 Lampoldshausen, Germany; H. FrÃ¼holz, Astrium GmbH, D-88039 Friedrichshafen, Germany

2009-051: PROJECT OF OSAKA INSTITUTE OF TECHNOLOGY ELECTRIC-ROCKET-ENGINE ONBOARD SMALL SPACE SHIP; Minetsugu Yamada, Tomoyuki Ikeda, Tatsuya Fujiwara, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-ku, Osaka 535-8585, Japan

2009-052: TEST RESULTS OF DIRECT-DRIVE OF HET USING A HIGH-VOLTAGE MULTI-JUNCTION-CELL CONCENTRATOR ARRAY; Henry W. Brandhorst, Jr., Steve R. Best, and Julie A. Rodiek, Space Research Institute, Auburn University, AL, 36849, USA; Mark J. O’Neill, Entech Solar, Inc., Ft. Worth, TX, 76177, USA; Michael F. Piszczor, Jr., NASA Glenn Research Center, Cleveland, OH, 44135

2009-053: NEW ELECTRIC PROPULSION MISSIONS AT SSC: THE USE OF SMART-1 HERITAGE AND NEW LESSONS LEARNT; Alain DemairÃ©, Bjarne Andersson, Johann Stanojev and Peter Rathsman, Swedish Space Corporation, Box 4207, SE-171 04 Solna, Sweden

2009-054: HALL ELECTRIC PROPULSION SYSTEM ON TECHNOLOGICAL TEST SATELLITE PROGRAM; Kang Xiaolu, Zhao Zhen, Qiao Caixia, Yu Shuilin, Shi Chenyi, Shanghai Institute of Space Propulsion, Shanghai 200233

2009-058: DEVELOPMENT STATUS OF A NEW POWER PROCESSING UNIT OF ION ENGINE SYSTEM FOR THE SUPER LOW ALTITUDE TEST SATELLITE; Hiroyuki Osuga, Toshiyuki Ozaki, Takafumi Nakagawa, and Kazuo Shuto, Space System Department, Kamakura Works, Mitsubichi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan

2009-061: DEVELOPMENT OF XENON FEED SYSTEM FOR A 300-W HALL-THRUSTER; Younho Kim, Seongmin Kang, and Yunhwang Jeong, Satrec Initiative, Daejeon, Yuseong, 305-811, Korea; Jongho Seon, Kyunghee University, Yongin, Kiheung, 446-701, Korea; Junghyun Wee and Hoseong Yoon, Space Solutions, Daejeon, Yuseong, 305-500, Korea; Jongsub Lee, Mihui Seo, and Wonho Choi, Korea Advanced Institute of Science and Technology, Daejeon, Yuseong, 305-701, Korea

2009-062: DEVELOPMENT OF A CESIUM PROPELLANT TANK FOR FEEP APPLICATION; Louis Dandaleix, Elizabeth Estrada, and Christophe Figus, EADS ASTRIUM, Toulouse, 31402 Cedex 4, France; Fabio Ceccanti, Angela Rossodivita, and Mirko Spurio, ALTA S.p.A, Pisa, 56121, Italy; Davide Nicolini and Pierre-Etienne Frigot, European Space Agency, Noordwijk, The Netherlands

2009-064: SIMPLIFIED ION THRUSTER XENON FEED SYSTEM FOR NASA SCIENCE MISSIONS; John Steven Snyder, Thomas M. Randolph, Richard R. Hofer, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2009-065: THE PERFECT ELECTRIC THRUSTER: A SPACECRAFT SYSTEM APPROACH TO ITS DEFINITION; Paolo Bianco, Astrium Satellites Ltd, Anchorage Road, Portsmouth, PO3 5PU, UK

2009-066: HIPER: A ROADMAP FOR FUTURE SPACE EXPLORATION WITH INNOVATIVE ELECTRIC PROPULSION TECHNOLOGIES; C. Casaregola, G. Cesaretti and M. Andrenucci, Alta S.p.A., Pisa, 56121, Italy

2009-068: THEORETICAL MODELING OF IONIZATION PROCESSES IN ANODE CAVITY OF CAMILA HALL THRUSTER; A. Kapulkin and M. Guelman, Asher Space Research Institute – Technion, I.I.T., Haifa, 32805, Israel

2009-069: ELECTRON GUIDING CENTER MODELING FOR HALL THRUSTER SIMULATIONS; Jan Miedzik and Serge Barral, Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland; StÃ©phan Zurbach, Snecma, Safran Group, 27208 Vernon, France

2009-070: A NEW BREATH FOR THE BREATHING MODE; Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland; Zbigniew Peradzynski, Warsaw University, 02-097 Warsaw, Poland

2009-071: ELECTROMAGNETIC EMISSIONS FROM PPS 1350 HALL THRUSTER; Edward J. Beiting, Xuan Le Eapen, and James E. Pollard, The Aerospace Corporation, P.O. Box 92957 – M2/341, Los Angeles, CA 90009-2957; Marc Gambon, FrÃ©dÃ©ric R. Marchandise, Michael Ã¶berg, SNECMA, Division Moteurs Spatiaux, Site de Vernon, B.P. 820, 27208 Vernon, France

2009-072: PARAMETERS INFLUENCING THE GENERATION OF THE L, S, AND C-BANDS (1-8 GHZ) EMISSION FROM HALL THRUSTERS; Edward J. Beiting, Rostislav Spektor, and Xuan Le Eapen, The Aerospace Corporation, P.O. Box 92957 – M2/341, Los Angeles, CA 90009-2957

2009-073: SELF-CONSISTANT CALCULATION OF ELECTRON TRANSPORT IN A CYLINDRICAL HALL THRUSTER; Lubos Brieda and Michael Keidar, The George Washington University, Washington, D.C. 20052; Yevgeny Raitses and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ 08543

2009-074: INVESTIGATION OF LOW DISCHARGE VOLTAGE HALL THRUSTER OPERATING MODES AND IONIZATION PROCESSES; Daniel L. Brown, Air Force Research Laboratory, Edwards AFB, CA, 93524, USA; Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA

2009-075: HYBRID SIMULATIONS OF HALL THRUSTERS OPERATING ON VARIOUS PROPELLANTS; Eunsun Cha, David B. Scharfe, Michelle K. Scharfe, and Mark A. Cappelli, Standford University, Stanford, CA, 94305; Eduardo Fernandez, Eckerd College, St. Petersburg, FL, 33711

2009-076: A REVIEW OF FACILITY EFFECTS ON HALL EFFECT THRUSTERS; David Byers, Las Vegas, NV, 89103; John W. Dankanich, Gray Research Inc., Cleveland, OH, 44135

2009-077: ELEMENTARY SCALING LAWS FOR SIZING UP AND DOWN HALL EFFECT THRUSTERS: IMPACT OF SIMPLIFYING ASSUMPTIONS; K. Dannenmayer and S. Mazouffre, Institut de Combustion, AÃ©rothermique, RÃ©activitÃ© et Environnement, CNRS, 1C avenue de la Recherche Scientifique, 45071 OrlÃ©ans, France

2009-078: 3D TRANSIENT MODELING OF HALL THRUSTERS: A FULLY FLUID APPROACH; De Marco Enrico A., University of Pisa, Pisa, 56126, Italy; Andrenucci Mariano, University of Pisa, Pisa, 56126, Italy

2009-081: ROTATING PLASMA EFFECTS IN CYLINDRICAL HALL THRUSTERS; Nathaniel J. Fisch and Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ 08544

2009-082: DETERMINATION OF THE AXIAL ELECTRON MOBILITY PROFILE IN THE PPS X000-LM THRUSTER; L. Garrigues, J. PÃ©rez-Luna, J. Lo, G.J.M. Hagelaar, and J. P. Boeuf, Laboratoire Plasma et Conversion d’Energie, UniversitÃ© de Toulouse, Batiment 3R2, 118 route de Narbonne, 31062 Toulouse, France; S. Mazouffre, Institut de Combustion, AÃ©rothermique, RÃ©activitÃ© et Environnement, 1C Avenue de la Recherche Scientifique, 45071 OrlÃ©ans, France

2009-083: CHARACTERISTICS OF A PERMANENT MAGNET LOW POWER HALL THRUSTER; A. Leufroy, T. Gilbert, and A. Bouchoule, GREMI Laboratory, OrlÃ©ans University & CNRS, 45067, OLEANS Cedex2, France

2009-084: SPECTRAL ANALYSIS OF SIMULATED HALL THRUSTER DISCHARGE CURRENT OSCILLATIONS; Paul N. Giuliano and Iain D. Boyd, The University of Michigan, Ann Arbor, MI, 48109, USA

2009-085: BPT-4000 HALL THRUSTER EXTENDED POWER THROTTLING RANGE CHARACTERIZATION FOR NASA SCIENCE MISSIONS; Richard R. Hofer, Dan M. Goebel, John Steven Snyder, and Izabella Sandler, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA

2009-087: LASER-INDUCED FLUORESCENCE STUDY OF NEUTRAL XENON FLOW EVOLUTION INSIDE A 6-KW HALL THRUSTER; Wensheng Huang and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109, USA

2009-088: USING NONLINEAR ZEEMAN SPECTROSCOPY TO OBTAIN IN-SITU MAGNETIC FIELD MEASUREMENT IN A HALL THRUSTER; Wensheng Huang, Bailo B. Ngom, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109, USA

2009-089: MODELING OF VIRTUAL DIAGNOSTICS FOR HALL THRUSTER PLUMES IN A VACUUM-CHAMBER; Tyler D. Huismann and Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109, USA

2009-090: EFFECTS ON NON-MAXWELLIAN ELECTRON VELOCITY DISTRIBUTION FUNCTION ON TWO-STREAM INSTABILITY IN LOW-PRESSURE DISCHARGES; D. Sydorenko, Department of Physics, University of Alberta, Edmonton, Alberta T6G 2G7, Canada; I. D. Kaganovich and Y. Raitses, Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA; A. Smolyakov, Department of Physics and Engineering Physics, University of Saskatchewan, Saskatoon, Saskatchewan S7N 5E2, Canada

2009-091: ABSENCE OF AS STEADY-STATE SPACE CHARGE LIMITED REGIME FOR A SHEATH IN A WEAKLY COLLISIONAL PLASMA BOUNDED BY WALLS WITH HIGH SECONDARY ELECTRON EMISSION; A. Khrabrov, I. Kaganovich, and Y. Raitses, Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jersey 08543, USA; D. Sydorenko, Department of Physics, University of Alberta, Edmonton T6G 2G7, Canada; A. Smolyakov, Dept. of Physics and Eng. Physics, Univ. of Saskatchewan, Sakatoon, Saskatchewan S7N 5E2, Canada

2009-092: Hani Kamhawi, David Manzella, Luis Pinero, and Thomas Haag, National Aeronautics and Space Administration Glenn Research Center, Cleveland, Ohio, 44135; Alex Mathers, Aerojet Corporation, Redmond, Washington, 98052

2009-093: PRELIMINARY PERFORMANCE CHARACTERIZATION OF THE HIGH VOLTAGE HALL ACCELERATOR ENGINEERING MODEL THRUSTER; Hani Kamhawi and Thomas Haag, National Aeronautics and Space Administration Glenn Research Center; Alex Mathers, Aerojet Corporation, Redmond, Washington, 98052

2009-094: PEFORMANCE CHARACTERISTICS OF CYLINDRICAL HALL THRUSTERS; Seongmin Kang, Younho Kim, Yunhwang Jeong, Satrec Initiative, Daejeon, 305-811, Korea; Jongho Seon, Kyunghee University, Yongin, 446-701, Korea; Jongsub Lee, Mihui Seo, and Wonho Choe, KAIST, Daejeon, 305-701, Korea

2009-095: A NEW ALGORITHM FOR THE NEUTRAL GAS IN THE FREE-MOLECULE REGIMES OF HALL AND ION THRUSTERS; Ira Katz and Ioannis G. Mikellides, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2009-097: ANALYSIS OF ENERGY BALANCE IN THE DISCHARGE OF SPT USING RESULTS OF ITS INTEGRAL PARAMETERS AND PLUME CHARACTERISTICS MEASUREMENTS; A. S. Arkhipov, V. Kim, and E. K. Sidorenko, Research Institute of Applied Mechanics and Electrodynamics (RIAME), Moscow 125080, Russia; S. A. Khartov, Moscow Aviation Institute, Moscow, 125080, Russia

2009-098: ALEXEY MOROZOV-LEADER OF THE SPT DEVELOPMENT IN THE USSR; V. Kim and G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics (RIAME), Moscow, 125080, Russia; K. N. Kozubsky and V. M. Murashko, Design Bureau “Fakel”, Kaliningrad, Russia; V. P. Khodnenko, All-Russian Institute of Electromechanics, Moscow, Russia; I. P. Nazarenko, Moscow Aviation Institute, Moscow, Russia

2009-099: EXPERIMENTAL CHARACTERIZATION OF HIGH FREQUENCY INSTABILITIES WITHIN THE DISCHARGE CHANNEL OF A HALL THRUSTER; Aaron K. Knoll and Mark A. Cappelli, High Temperature Gasdynamics Laboratory, Stanford University, Stanford, CA, 94305, USA

2009-101: ELECTRIC PROBE MEASUREMENTS OF PLASMA OSCILLATIONS IN THE 100-500 KHZ RANGE WITHIN THE DISCHARGE OF THE PPS—X000 HALL THRUSTER; Jacek Kurzyna, Institute of Plasma Physics and Laser Microfusion, 23 Hery Str, 01-497 Warsaw, Poland; Stephane Mazouffre and Vladimir Kulaev, ICARE-CNRS, 1C Avenue de la Recherche Scientifique, 45071 OrlÃ©ans Cedex 2, France

2009-102: TWO-DIMENSIONAL (Z-0) SIMULATIONS OF HALL THRUSTER ANOMALOUS TRANSPORT; Cheryl M. Lam, Aaron K. Knoll, and Mark A. Cappelli, High Temperature Gasdynamics Laboraotry, Stanford University, Stanford, CA 94305-3032, USA; Eduardo Fernandez, Department of Mathematics and Physics, Eckerd College, St. Petersburg, FL, 33711 94305

2009-105: HALL THRUSTER ELECTRON MOTION CHARACTERIZATION BASED ON INTERNAL PROBE MEASUREMENTS; Jesse A. Linnell and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109, USA

2009-106: TWO-DIMENSIONAL TIME-RESOLVED BREATHING MODE PLASMA FLUCTUATION VARIATION WITH HALL THRUSTER DISCHARGE SETTINGS; Robert B. Lobbia and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI, 48109, U.S.A.

2009-107: DEVELOPMENT OF A MAGNESIUM AND ZINC HALL-EFFECT THRUSTER; Jason M. Makela, Robert L. Washeleski, Dean R. Massey, and Lyon B. King, Michigan Technological University, Houghton, Michigan, 49931, USA; Mark A. Hopkins, Aerophysics Inc, Houghton, Michigan, 49931, USA

2009-110: KINETIC SIMULATION OF THE STATIONARY HEMP THRUSTER INCUDING THE NEAR-FIELD PLUME REGION; K. Matyash, O. Kalentev, and R. Schneider, Max-Planck-Institut fÃ¼r Plasmaphysik, EURATOM Association, Greifswald, D-1749, Germany; F. Taccogna, Istituto di Metodologie Inorganiche e dei Plasmi-CNR, Via Amendola 122/D, 70126 Bari, Italy; N. Koch and M. Schiraa, THALES Electron Devices GmbH, D-89077 Ulm, Germany

2009-111: EXAMINATION OF THE TEMPORAL CHARACTERISTICS OF THE ELECTRIC FIELD IN A HALL EFFECT THRUSTER USING A PHOTON-COUNTING TECHNIQUE; G. Bourgeois and S. Mazouffre, Institut de Combustion, AÃ©rothermique, RÃ©activitÃ© et Environnement, CNRS, 1C avenue de la Recherche Scientifique, 45071 OrlÃ©ans, France; N. Sadeghi, Laboratoire de SpectromÃ©trie Physique, UniversitÃ© Joseph Fourier, CNRS, 140 av. de la Physique, 38402 St. Martin d’Hyeres, France

2009-112: HIGH SPEED INTERROGATION OF THE NEAR-FIELD PLUME OF A 6-KW LABORATORY HALL THRUSTER; M. S. McDonald, R. B. Lobbia, and A. D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), University of Michigan, Ann Arbor, MI 48109, USA

2009-113: CATHODE POSITION AND ORIENTATION EFFECTS ON CATHODE COUPLING IN A 6-KW HALL THRUSTER; M. S. McDonald and A. D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), University of Michigan, Ann Arbor, MI 48109, USA

2009-114: HALL-EFFECT THRUSTER SIMULATIONS WITH 2-D ELECTRON TRANSPORT AND HYDRODYNAMIC IONS; Ioannis G. Mikellides, Ira Katz, Richard R. Hofer, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2009-115: A PLUME COMPARISON OF XENON AND KRYPTON PROPELLANT ON A 600 W HALL THRUSTER; Michael R. Nakles and Ryne R. Barry, ERC, Inc., Edwards Air Force Base, CA 93524; C. William Larson and William A. Hargus, Jr., Air Force Research Laboratory, Edwards Air Force Base, CA 93524

2009-116: WAYS AND METHODS OF ACCURACY INCREASING OF THRUSTER PLASMA PARAMETERS DETERMINING BY AN ELECTRIC PROBE; Sergey A. Oghienko and Volodimir D. Olendarev, National Aerospace University “Kharkiv Aviation Institute”, 17 Chkalova str., Kharkiv, 61070, Ukraine; Andrey V. Khiko, Sergey N. Kulagin, and Alexandr N. Petrenko, National State University, 72 Gagarina str., Dnepropetrovsk, 49010, Ukraine

2009-117: PERFORMANCE OF POWER PROCESSING UNIT FOR 250MN-CLASS HALL THRUSTER; Hiroyuki Osuga, Kentaro Suzuki, Takafumi Nakagawa, and Toshiyuki Ozaki, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Taichiro Tamida, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-honmachi, Amagasaki, Hyogo, 661-8661, Japan; Katsuaki Matsui, Institute for Unmanned Space Experiment Free Flyer, 2-12 Kanda-Ogawamachi, Chiyoda-Ku, Tokyo, 101-0052, Japan

2009-118: QCM AND OES: TWO WAYS USED TO STUDY SIMULTANEOUSLY HET THRUSTER CHAMBER CERAMIC EROSION. FIRST QCM RESULTS ON PPS100-ML VALIDATE PREVIOUS OES MEASUREMENTS; D. Pagnon, Laboratoire de Physique des Gaz et des Plasmas UniversitÃ© Paris XI – 91405 Orsay Cedex – France; L. Balika and S. Pellerin, GREMI, UniversitÃ© d’OlÃ©ans, rue G. Berger, BP 4043 – 18028 Bourges – France

2009-119: EXPERIMENTAL INVESTIGATION OF BACKPRESSURE EFFECTS ON THE IONIZATION AND ACCELERATION PROCESSES IN A HALL THRUSTER; Peng E, Daren Yu, and Binhao Jiang, Harbin Institute of Technology, Harbin, Heilongjiang, 150001, China

2009-122: DISCHARGE OSCILLATIONS IN A PERMANENT MAGNET CYLINDRICAL HALL-EFFECT THRUSTER; K. A. Polzin and E. S. Sooby, NASA-Marshall Space Flight Center, Huntsville, AL 35812; Y . Raitses, E. Merino and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ 08543

2009-123: PLUME NARROWING AND SUPPRESSION OF LOW FREQUENCY OSCILLATIONS IN CYLINDRICAL HALL THRUSTERS; Yevgeny Raitses, Jeffrey B. Parker, and Nathaniel J. Fisch, Princeton University Plasma Physics Laboratory, Princeton, NJ 08540, USA

2009-124: NEAR-FIELD ION CURRENT DENSITY MEASUREMENTS OF A 6-KW HALL THRUSTER; Bryan M. Reid and Alec D. Gallimore, University of Michigan, Ann Arbor, MI 48109, USA

2009-126: HT-100 DEVELOPMENT STATUS; P. Rossetti and M. Andrenucci, Alta SpA, Pisa, 56121, Italy

2009-129: PREDICTING ELECTRON TRANSPORT USING SIMULATED AXIAL WAVES IN A RADIAL-AXIAL HYBRID HALL THRUSTER MODEL; Michelle K. Scharfe, ERC Inc., Edwards AFB, CA, 93524, USA; Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA; Eduardo Fernandez, Eckerd College, St. Petersburg, FL, 33711, USA

2009-131: EFFECT OF WALL SHEATHS ON ION TRAJECTORIES IN A HALL THRUSTER NUMERICAL MODEL; Regina M. Sullivan and Joseph E. Shepherd, California Institute of Technology, Pasadena, CA, 91125, USA; Michelle K. Scharfe, ERC, Inc., Edwards AFB, CA, 93524, USA; Ioannis G. Mikellides and Lee K. Johnson, Jet Propulsion Laboratory, Pasadena, CA, 91109, USA

2009-132: THE EFFECT OF ELECTRON DISTRIBUTION FUNCTION ANISOTROPY ON SPACE CHARGE SATURATED SHEATH CRITICAL PARAMETERS IN HALL THRUSTERS; Daren Yu, Shaowei Qing, and Yongiie Ding, Lab of Plasma Propulsion, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China; Xiaogang Wang, State Key Lab of Nuclear Physics & Technology, School of Physics, Peking University, Beijing 100871, China

2009-133: NEW-WALL PLASMA CHARACTERIZATION OF A 6-KW HALL THRUSTER; Rohit Shastry and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI 48109; Richard R. Hofer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2009-134: THE INFLUENCE OF POTENTIAL AZIMUTHAL OSCILLATIONS ON OUTGOING IONS DYNAMICS IN SPT; A. N. Vesselovzorov, E. D. Dlougach, A. A. Pogorelov, E. B. Svirskiy, and V. A. Smirnov, Russian Research Centre ‘Kurchatov Institute’ Moscow, Russia

2009-135: TIME AND SPACE-CORRELATED PLASMA PROPERTY MEASUREMENTS IN THE NEAR-FIELD OF A COAXIAL HALL DISCHARGE; Andrew W. Smith and Mark A. Cappelli, Stanford Plasma Physics Laboratory, Stanford University, Stanford, CA, 94305-3032, USA

2009-136: SINGLE PARTICLE SIMULATIONS OF ELECTRON TRANSPORT IN THE NEAR-FIELD OF HALL THRUSTERS; Andrew W. Smith and Mark A. Cappelli, Stanford Plasma Physics Laboratory, Stanford University, Stanford, CA, 94305-3032, USA

2009-137: LIF MEASUREMENTS OF THE CYLINDRICAL HALL THRUSTER PLUME; R. Spektor, K. D. Diamant, and E. J. Beiting, The Aerospace Corporation, Y. Raitses and N. J. Fisch, Princeton Plasma Physics Laboratory

2009-138: LIGHT METAL PROPELLANT HALL THRUSTERS; James Szabo, Mike Robin, and John Duggan, Busek Co. Inc, Natick, MA, 01760, USA; Richard R. Hofer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2009-139: ANOMALOUS TRANSPORT INDUCED BY SHEATH INSTABILITY IN HALL EFFECT THRUSTERS; Francesco Taccogna and Pierpaolo Minelli, Isituto di Metodologie Inorganiche e dei Plasmi-CNR, via Amendola 122/D, 70126 Bari, Italy; Savino Longo and Mario Capitelli, Dipartimento di Chimica, Universita degli Studi di Bari, via Orabona 4, 70120 Bari, Italy; Ralf Schneider, Max Planck Institute fÃ¼r Plasmaphysik, Wendelsteinstrasse 1, D-17491 Greifswald, Germany

2009-140: PERFORMANCE PREDICTION IN LONG OPERATION FOR MAGNETIC-LAYER-TYPE HALL THRUSTERS; Hirokazu Tahara, Tsuyoshi Fujita, and Yudai Shimizu, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan

2009-141: IN-SITU TEMPERATURE, GRID CURVATURE, EROSION, BEAM AND PLASMA CHARACTERIZATION OF A GRIDDED ION THRUSTER RIT-22; C. Bundesmann, M. Tartz, F. Scholze, and H. Neumann, Leibniz-Institute of Surface Modification, Leipzig, 04318, Germany; H. J. Leiter, Astrium Space Transporation Moeckmuehl, 74215, Germany; F. Scortecci, Aerospazio Tecnologie s.r.l., Rapolano Terme, 53040, Italy; D. Feili, Justig-Liebig-UniversitÃ¤t Giessen, Giessen, 35392, Germany; P.-E. Frigot and J. Gonzalez del Amo, ESA/ESTEC, 2200 AG Noordwijk, The Netherlands

2009-142: ERT IN VACUUM CHAMBERS. 3D SIMULATIONS OF THE MOST INTERESTING FEATURES; Grigory Toropov, Russia, Kaliningrad, Rinskaya 29,79; Sergey Khartov, Moscow Aviation Institute (State Technical University) MAI, Electric Propulsion and Space Power Plants Department, 4, Volokolamskoe sh., Moscow, 125971, Russia

2009-143: SMALL-SCALE DENSITY FLUCTUATION MODES IN A HALL PLASMA THRUSTER: EXPERIMENTAL STUDIES VIA COLLECTIVE LIGHT SCATTERING; Sedina Tsikata, Dominique GrÃ©sillon, Cyrille HonorÃ©, and Vitaliy Pisarev, Ecole Polytechnique, Laboratoire de Physique des Plasmas, UMR 7548, Palaiseau 91128, France; Nicolas Lemoine, Institut Jean Lamour, UniversitÃ© Henri PoincarÃ©, Nancy 54506, France

2009-144: PERFORMANCE VARIATION IN BPT-4000 HALL THRUSTERS; Alex Mathers and Kristi de Grys, Aerojet General Corp, Redmond, WA, 98073; Jonathan Paisley, Lockheed Martin, Sunnyvale, CA, 94089

2009-146: DEVELOPMENT OF A CAVITY RING-DOWN SPECTROSCOPY SENSOR FOR BORON NITRIDE EROSION IN HALL THRUSTERS; Lei Tao, Brian Lee, and Azer Yalin, Colorado State University, Fort Collins, CO, 80521, USA; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 8168580, Japan; Alec Gallimore, University of Michigan, Ann Arbor, Michigan, 48109, USA

2009-147: CAVITY RING-DOWN SPECTROSCOPY SENSOR FOR REAL TIME IN SITU MEASUREMENT OF SPUTTER EROSION IN ANODE LAYER TYPE HALL THRUSTERS; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan; Lei Tao, Binyamin Rubin, John D. Williams, and Azer P. Yalin, Colorado State University, Fort Collins, CO, 80523, USA

2009-148: DISCHARGE STABILIZATION METHOD OF AN ANODE LAYER TYPE HALL THRUSTER BY ON-UNIFORM PROPELLANT FLOW; Yasuhiro Fukushima, Shigeru Yokota, Daosike Takahashi, Kentaro hara, Shinatora Cho, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, Japan

2009-149: MEASUREMENT OF ION NUMBER DENSITY AND VELOCITY DISTRIBUTION IN AN ANODE-LAYER TYPE HALL THRUSTER BY LASER INDUCED FLORESCENCE METHOD; Shigeru Yokota, Kentaro Hara, Shinatora Cho, Daisuke Takahashi, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo Bunkyo, Tokyo, 113-0033, Japan

2009-150: NASA’S EVOLUTIONARY XENON THRUSTER (NEXT) ION PROPULSION TECHNOLOGY DEVELOPMENT STATUS IN 2009; Scott W. Benson and Michael J. Patterson, NASA Glenn Research Center, Cleveland, Ohio, 44135, USA

2009-151: IN-SITU MEASUREMENTS OF DISCHARGE PLASMA CHARACTERISTICS DURING THRUST OPERATION OF THE T6 GRIDDED ION THRUSTER; M. H. Corbett, QinetiQ Ltd, Cody Technology Park, Farnborough, GU14 0LX, U.K.

2009-152: EVALUATION OF 25-CM XIPS THRUSTER LIFE FOR DEEP SPACE MISSION APPLICATIONS; Dan M. Goebel, James E. Polk, Izabela Sandler, Ioannis G. Mikellides, and J. R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, CA, 91109; William G. Tighe and Kuei-Ru Chien, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505

2009-153: KEEPER WEAR MECHANISMS IN THE XIPS 25-CM NEUTRALIZER CATHODE ASSEMBLY; Dan M. Goebel, Ioannis G. Mikellides, James E. Polk, and Jack Young, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, CA, 91109; William G. Tighe and Kuei-Ru Chien, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505

2009-154: NEXT LONG-DURATION TEST NEUTRALIZER PERFORMANCE AND EROSION CHARACTERISTICS; Daniel A. Herman, ASRC Aerospace Corporation, Cleveland, OH, 44135, United States; George C. Soulas and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, United States

2009-155: INTERMEDIATE REPORT OF MU-20 MICROWAVE DISCHARGE ION THRUSTER DEVELOPMENT; Satoshi Hosoda, Kazutaka Nishiyama, Yasuhiro Yoyoda, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kangagawa, 229-8510, Japan

2009-156: PRIMARY ELECTRON TRANSPORT AND LOSSES IN A RING-CUSP DISCHARGE CHAMBER; Aimee A. Hubble and John E. Foster, University of Michigan, Ann Arbor, Michigan, 48109, USA

2009-157: DUAL STAGE FOUR GRID (DS4G) ION ENGINE FOR VERY HIGH VELOCITY CHANGE MISSIONS; R. Intini Marques and S. B. Gabriel, University of Southampton, Astronautics Research Group, Southampton, SO17 1BJ, United Kingdom

2009-159: COMPARISON OF SPT AND HEMP THRUSTER CONCEPTS FROM KINETIC SIMULATIONS; K. Matyash, R. Schneider, A. Mutzke, and O. Kalentev, Max-Planck-institut fÃ¼r Plasmaphysik, EURATOM Association, Greifswald, D-1749, Germany; F. Taccogna, Istituto di Metodologie Inorganiche e dei Plasmi-CNR, Via Amendola 122/D, 70126 Bari, Itally; N. Koch and M. Schirra, THALES Electron Devices GmbH, D-89077 Ulm, Germany

2009-160: IN-SITU TEMPERATURE, GRID CURVATURE, EROSION, BEAM AND PLASMA CHARACTERIZATION OF A GRIDDED ION THRUSTER RIT-22; C. Bundesmann, M. Tartz, F. Scholze, and H. Neumann, Leibniz-Institute of Surface Modification, Leipzig, 04318, Germany, H. J. Leiter, Astrium Space Transportation, Moeckmuehl, 74215, Germany; F. Scortecci, Aerospazio Tecnologie s.r.l., Rapolano Terme, 53040, Italy; D. Feile, Justig-Leibig-UniversitÃ¤t Giessen, Giessen 35392, Germany; P.-E. Frigot and J. Gonzalez del Amo, ESA/ESTEC, 2200 AG Noordwijk, The Netherlands

2009-161: THE 25 CM XIPX LIFE TEST AND POST-TEST ANALYSIS; William G. Tighe, Kuei-Ru Chien, Zeke Solis, and Rafael Spears, L-3 Communications Electron Technologies, Inc., Torrance, CA, 90505

2009-162: PLASMA LUMINESCENCE MEASUREMENTS IN THE ECR ION THRUSTER Âµ10 USING AN OPTICAL FIBER PROBE; Ryudo Tsukizaki, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan; Hiroyuki Koizumi, Satoshi Hosoda, Kazutaka Nishiyama, and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2009-163: NEXT PM1R ION THRUSTER AND PROPELLANT MANAGEMENT SYSTEM WEAR TEST RESULTS; Jonathan L. Van Noord and George C. Soulas, NASA Glenn Research Center, Cleveland, OH, 44135, USA; James S. Sovey, Alphaport, Inc., Cleveland, OH, 44135, USA

2009-164: LONG DURATION ASSESSMENT OF ELECTRON BACKSTREAMING FOR ION OPTICS; Richard E. Wirz, University of California of California, Los Angeles, CA, 90095, USA

2009-165: DIAGNOSTICS OF A PLASMA IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER USING LASER THOMSON SCATTERING TECHNIQUE; Naoji Yamamoto, Tomoaki Kurita, Kentaro Tomita, Kiichiro Uchino, and Hideki Nakashima, Kyushu Unviersity, Kasuga, Fukuoka, 816-8580, Japan

2009-166: PRELIMINARY CHARACTERIZATION OF A DIVERGING CUSPED FIELD (DCF) THRUSTER; Christopher V. Young, Andrew W. Smith, and Mark A. Cappelli, High Temperature Gasdynamics Laboratory, Stanford University, Stanford, CA 94305-3032, USA

2009-167: DESIGN AND PERFORMANCE TESTING OF A 1-CM MINIATURE RADIO-FREQUENCY ION THRUSTER; Thomas A. Trudel, Sven G. BilÃ©n, and Michael M. Micci, The Pennsylvania State University, University Park, Pennsylvania 16802, USA

2009-168: DESIGN AND TESTING OF A LOW POWER RADIO-FREQUENCY ELECTROTHERMAL THRUSTER; Jeffrey R. Hopkins, Michael M. Micci, and Sven G. BilÃ©n, The Pennsylvania State University, University Park, PA 16802, USA

2009-169: INITIAL DEVELOPMENT OF THE MICROCAVITY DISCHARGE THRUSTER; Rodney L. Burton, J. Gary Eden, Sung-Jin Park, Je Kwon Yoon, Mark de Chadenedes, and Steven Garrett, University of Illinois at Urbana-Champaign, Urbana, IL, 61801; Laxminaraya L. Raja and Hariswaran Sitaraman, University of Texas at Austin, Austin, TX, 78712; Julia Laystrom-Woodard, Gabriel Benavides, and David Carroll, CU Aerospace, Champaign, IL, 61820

2009-170: 3200 HOURS ENDURANCE TESTING OF THE LISA PATHFINDER FT-150 THRUSTER; F. Ceccanti, L. Paita, U. Cesari, M. De Tata, N. Giusti, P. Balducci, and M. Del Pistoria, Alta SpA, Pisa, 56121, Italy; D. Nicolini and L. Di Napoli, European Space Agency, Noordwijk, The Netherlands

2009-171: THE MIDGIT THRUSTER: DEVELOPMENT OF A MULTI-MODE THRUSTER; Cheryl M. Collingwood and Stephen B. Gabriel, Astronautics Research Group, University of Southampton, Highfield, Southampton, Hants, SO17 1BJ, UK; Michael H. Corbett and Peter Jameson, Electric Propulsion Group, QinetiQ, Farnborough, Hants, GU14 0LX, UK

2009-172: WATER CONTAMINANT MITIGATION IN IONIC LIQUID PROPELLANT; Dr. David Conroy and Dr. John Ziemer, Jet Propulsion Laboratory, Pasadena, CA, 91109-8099

2009-173: THREE-COMPONENT LIF DOPPLER VELOCIMETRY TO MEASURE THE NEUTRAL CESIUM FLOW RATE FROM A CESIUM-FED FEEP THRUSTER; Paul-Quentin Elias, Denis Packan, and Jean Bonnet, ONERA, Palaiseau, 91176, France; Fabio Ceccanti, Ugo Cesari, and M. De Tata, Alta SpA, Pisa, 56121, Italy; Eric Gengembre, Davide Nicolini, and Pierre-Etienne Frigot, ESA-ESTEC, Noordwijk, 2200 AG, Netherlands

2009-174: ÂµNRIT-2.5 – A NEW OPTIMIZED MICROTHRUSTER OF GIESSEN UNIVERSITY; D. Feili, B. Lotz, St. Bonnet, B. K. Meyer, and H. W. Loeb, Justus Liebig University Giessen, Heinrich-Buff-Ring 16, 35392 Giessen; N. Puetmann, Deutsches Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR), KÃ¶nigswinterer Strasse 522-524, 53227 Bonn

2009-175: THE EXPANSION OF COLLOID THRUSTER BEAMS; M. Gamero-CastaÃ±o, University of California, Irvine, California, 91697, USA

2009-176: UNDERSTANDING HOLLOW CATHODE THRUST PRODUCTION MECHANISMS; A. N. Grubisic and S. B. Gabriel, University of Southampton, Southampton, S017 1BJ, United Kingdom

2009-177: PROPELLANT LOADING EFFECTS ON FERROELECTRIC PLASMA THRUSTER PERFORMANCE AND POSSIBLE APPLICATIONS; Brian T. Hutsel, Scott D. Kovaleski, and Craig Kluever, University of Missouri, Columbia, MO, 65211, USA

2009-178: ION BEAM EXTRACTION AND ELECTRON EMISSION FROM THE MINIATURE MICROWAVE DISCHARGE ION ENGINE Âµ1; Hiroyuki Koizumi and Hitoshi Kuninaka, Institute of Space and Astronautical Science of the Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2009-179: DESIGN DEVELOPMENT AND TEST OF THE RIT-ÂµX MINI ION ENGINE SYSTEM

2009-181: MOLECULAR DYNAMICS SIMULATION OF LIQUID GALLIUM ELECTROSPRAY THRUSTERS; Dae Young Kim and Michael M. Micci, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA, 16802, USA

2009-182: NANOBALANCE: THE EUROPEAN BALANCE FOR MICRO-PROPULSION; Stefano Cesare, Fabio Musso, Filippo D’Angelo, and Giuseppe Castorina, Thales Alenia Space Italia, Strada Antica di Collegno 253, 10146 Turin, Italy; Marco Bisi and Paolo Cordiale, Istituto Nazionale de Ricerca Metrologica, Strada delle Cacce 73, 10135 Turin, Italy; Enrico Canuto, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Turin, Italy; Davide Nicolini Eliseo Balaguer, and Pierre-Etienne Frigot, ESA-ESTEC, Keplerlaan 1, 2201 AZ Noordwijk ZH, The Netherlands

2009-183: DIRECT THRUST AND THRUST NOISE MEASUREMENTS ON THE LISA PATHFINDER FIELD EMISSION THRUSTER; Davide Nicolini and Pierre-Etienne Frigot, European Space Agency, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands; Fabio Musso, Stefano Cesare and Giuseppe Castorina, Thales Alenia Space Italia SpA, Torino, 10146, Italy; Luca Ceruti, Furio Bartola, and Pietro Zanella, Galileo Avionica SpA, Milano, 20014, Italy; Fabio Ceccanti, Leonardo Priami and Luca Paita, Alta SpA, Pisa, 56121, Italy

2009-184: NUMBER DENSITY AND VELOCITY MEASUREMENT IN THE PLUME OF A MICRONEWTON COLD GAS THRUSTER BY ELECTRON BEAM FLUORESCENCE AND LASER INDUCED FLUORESCENCE; D. Packan, J. Bonnet, and S. Rocca, ONERA, Palaiseau, 91120, France

2009-185: THRUST MEASUREMENTS WITH THE ONERA MICRONEWTON BALANCE; D. Packan, J. Bonnet, and S. Rocca, ONERA, Palaiseau, 91120, France

2009-186: ALTA’S FT-150 FEEP MICROTHRUSTER: DEVELOPMENT AND QUALIFICATIONS STATUS; L. Paita, F. Ceccanti, M. Spurio, U. Cesari, L. Priami, F. Nania, A. Rossodivita, and Mariano Andrenucci, ALTA SpA, Pisa, 56121, Italy

2009-187: PEFORMANCE MODULATION OF COLLOID THRUSTERS BY THE VARIATION OF FLOW RATE WITH APPLIED VOLTAGE; Charles N. Ryan, Katharine L. Smith, Matthew S. Alexander, and John P. W. Stark, Queen Mary University of London, London, E1 4NS, UK

2009-188: MICROFABRICATED OUT-OF-PLANE ARRAYS OF INTEGRATED CAPILLARY NANO-ELECTROSPRAY EMITTERS; Renato Krpoun and Herbert R. Shea, Ecole Polytechnique FÃ©dÃ©rale de Lausanne (EPFL), 2002 Neuchatel, Switzerland

2009-189: PEFORMANCE OF A MICRO-FABRICATED COLLOID THRUSTER SYSTEM; Katharine L. Smith and John P. W. Stark, Queen Mary University of London, London E1 4NS, United Kingdom; Renato Krpoun, CSEM Brazil, Belo Horizonte, Minas Gerais, 30.170-020, Brazil; Herbert Shea, EPFL, Sch Engn, Microsyst Space Technol Lab, CH-2002 Neuchatel, Switzerland

2009-190: MICROWAVE-EXCITED MICROPLASMA THRUSTER: DESIGN IMPROVEMENT FOR IMPLEMENTATION TO SATELLITE; Takeshi Takahashi, Shunsuke Kitanishi, Yoshinori Takao, Koji Eriguchi, and Kouichi Ono, Kyoto University, Sakyo-ku, Kyoto, 606-8501, Japan

2009-191: NUMERICAL SIMULATION OF CONE-JET FORMATION IN COLLOID THRUSTER; Chao-Jin Qin, Hai-Bin Tang, and Hai-Xing Wang, Beijing University of Aeronautics and Astronautics, Beijing, 100191, P. R. China; Jiang-Hong Wu, South China University of Technology, Guangzhou, 510641, P. R. China

2009-192: DEVELOPMENT OF MICRO-VACUUM ARC THRUSTER WITH EXTENDED LIFETIME; TaiSen Zhuang, Alexey Shashurin, Lubos Brieda, and Michael Keidar, Mechanical & Aerospace Engineering, The George Washington University, Washington, DC 20052

2009-193: CYLINDRICAL MODEL OF A HELICON-GENERATED PLASMA; Eduardo Ahedo, Universidad PolitÃ©cnica de Madrid, Madrid 28040, Spain

2009-196: EXPERIMENTAL INVESTIGATION OF WAVE-PLASMA COUPLING ON THE HIGH POWER ELECTRODELESS PLASMA THRUSTER IN PRINCETON UNIVERSITY; Gegory D. Emsellem, The Elwing Company, Irvine, CA, 92612, USA

2009-197: PLASMA SOURCES AS THRUSTERS; A. Fruchtman and G. Makrinich, H.I.T. – Holon Institute of Technology, Holon 58102, Israel

2009-199: EXPERIMENT FOR PLASMA ENERGIZATION WITH BEATING ELECTROSTATIC WAVES; Benjamin Jorns and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ, 08540

2009-201: EVALUATION AND OPTIMIZATION OF AN 8-GHZ MICROWAVE ELECTROTHERMAL THRUSTER; Jacob H. Blum, Jeffrey R. Hopkins, Michael M. Micci, and Sven G. BilÃ©n, The Pennsylvania State University, University Park, PA 16802, USA

2009-203: ENERGY BALANCE IN A RADIO FREQUENCY ELCTRO-THERMAL THRUSTER WITH WATER PROPELLANT; M. Oya, N. Ymamoto, and H. Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan

2009-204: EXPERIMENTAL SET-UP TO TEST A 50 W HELICON PLASMA THRUSTER; D. Pavarin, F. Ferri, M. Manente, D. Curreli, Y. GÃ¼clÃ¼, D. Rondini, M. Mariutto, and L. Tasinato, CISAS “G.Colombo”, Center of Studies of Activities for Space, Padua University, Italy; J. Carlsson, Tech-X Corporation, Boulder, Colorado 80303, USA; R. De Angelis, ENEA Frascati Itay; D Pakan, ONERA France; K. Grue, Rovsing Denmark, P. Van Put and R. Tijsterman, Bradford Engineering, The Netherlands; A. Selmo, RESIA, Italy; A. Loyan, KHAI, Ukraine; and K. Katsonia, CNRS-LPGP

2009-205: DESIGN OF 50 W HELICON PLASMA THRUSTER; D. Pavarin, F. Ferri, M. Manente, D. Curreli, Y. GÃ¼clÃ¼, D. Melazzi, D. Rondini, and S. Suman, CISAS “G. Colombo”, Center of Studies of Activities for Space, Padua University, Italy; J. Carlsson, Tech-X Corporation, Boulder, Colorado 80303, USA; C. Bramanti, European Space Agency, The Netherlands; E. Ahedo, Universitad Politecica de Madrid, Spain; V. Lancellotti, Eindhoven University of Technology, The Netherlands; K. Katsonis, CNRS-LPGP; G. Markelov, AOES, The Netherlands

2009-206: NON INVASIVE MEASUREMENT ON THE PULSED AND STEADY-STATE, HIGH POWER MADHEX HELICON PLASMA THRUSTER; Matt Wiebold, John e. Scharer, and He. Ren, University of Wisconsin – Madison, Madiosn, WI 53711

2009-209: SUPERCONDUCTING 200 KW VASIMR EXPERIMENT AND INTEGRATED TESTING; Jared P. Squire, Leonardl D. Cassady, Franklin R. Chang DÃaz, Mark D. Carter, Tim G. Glocer, Andrew V. Ilin, Benjamin W. Longmier, Greg E. McCaskill, and Chris S. Olsen, Ad Astral Rocket Company, Webster, Texas, 77598, USA; Edgar A. Bering, III, University of Houston, Houston, Texas, 77004, USA

2009-210: DESIGN OF AN ECR GASDYNAMIC MIRROR THRUSTER; Ricky Tang, Alec D. Gallimore, and Terry Kammash, University of Michigan, Ann Arbor, MI, 48109, USA

2009-211: INITIAL PERFORMANCE OF A ECR WAVEGUIDE PLASMA CATHODE WITH PERMANENT MAGNETS; Brandon R. Weatherford and John E. Foster, University of Michigan, Ann Arbor, MI, 48104, USA

2009-214: HELIOCENTRIC INTERPLANETARY LOW-THRUST TRAJECTORY OPTIMIZATION PROGRAM CAPABILITIES AND COMPARISON TO NASA’S LOW-THRUST TRAGJECTORY TOOLS; Jerry L. Horsewood, SpaceFlightSolutions, Bowie, Maryland, 20720, U.S.A.; John W. Dankanich, Gray Research, Inc., Cleveland, Ohio, 44135, U.S.A.

2009-218: COMPASS FINAL REPORT: NEAR EARTH ASTEROIDS RENDEZVOUS AND SAMPLE EARTH RETURNS (NEARER); Steven R. Oleson and Melissa L. McGuire, In Space Propulsion; COMPAS Team Members: Les Balkanyi, Laura Burke, Tony Colozza, John Dankanich, Jon Drexler, Doug Fiehler, James Fincannon, John Gyekenyesi, Joe Hemminger, Jeff Juergens, Tom Krivanek, Nelson Morales, T. C. Nguyen, Tom Packard, Tom Parkey, Carl Sandifer, Tim Sarver-Verhey, Paul Schmitz, Anita Tenteris, Joe Warner, and Jeff Woytach

2009-219: AN ALGORITHM FOR GENERATING FEASIBLE LOW THRUST INTERPLANETARY TRAJECTORIES; Prashant R. Patel, Institute for Defense Analysis, Alexandria, VA, 22311, USA; Alec D. Gallimore and Thomas H. Zurbuchen, University of Michigan, Ann Arbor, MIM, 48109, USA; Daniel J. Scheeres, University of Colorado, Boulder, CO, 80309, USA

2009-220: DEVELOPMENT OF METHODS FOR RAPID ELECTRIC PROPULSION SYSTEM DESIGN AND OPTIMIZATION; Krzysztof Z. Pennar and Pavlos G. Mikellides, Arizona State University, Tempe, AZ, 85287; John K. Ziemer, Jet Propulsion Laboratory, Pasadena, CA, 91108

2009-222: OPTIMUM LOW-THRUST TRANSFER BETWEEN ARBITRARY ELLIPTIC ORBITS FOR POWER-LIMITED SPACECRAFT USING ASYMPTOTIC EXPANSIONS AND AVERAGING; Zahi Tarzi, Jason Speyer, and Richard Wirz, UCLA, Los Angeles, CA, 90024, USA

2009-224: RESULTS OF EXPERIMENTAL STUDY OF HOLLOW CATHODES IN HIGH CURRENT PLASMA DISCHARGE; Ryan T. Downey, University of Southern California, Los Angeles, CA 90089, USA; Paul Giuliano, University of Michigan, Ann Arbor, Michigan 48109, USA; Keith Goodfellow, University of Southern California, Los Angeles, CA 90089, USA; Dan Erwin, University of Southern California, Los Angeles, CA 90089, USA

2009-225: INDIRECT IMPULSE BIT MEASUREMENT FOR A QUASI-STEADY MPD WITH APPLIED MAGNETIC FIELD; Francesco Guarducci, Jan Lehnert, and Giorgio Paccani, Sapienza UniversitÃ¡ di Roma, 00185, Roma, Italia

2009-226: PERFORMANCE OF TWO-DIMENSIONAL APPLIED-FILED MAGNETO-PLASMA-DYNAMIC THRUSTER; Akira Iwakawa, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Daisuke Nakata, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Hitoshi Kuninaka, Institute of Space and Astronautical Science, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan

2009-227: NUMERICAL ANALYSES ON PLASMA ACCELERATION PROCESSES IN APPLIED-FIELD MAGNETOPLASMADYNAMIC THRUSTER; K. Kubota and I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Y. Okuno, Tokyo Institute of Technology, Tokohama, Kanagawa, 226-8502, Japan

2009-229: BOOSTING MPD THRUSTER PROPULSION EFFICIENCY THROUGH OPTIMIZATION; Masao Nagao, Nihon University, Funabashi, Chiba, 271-8501, Japan; Kenichi Kubota, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan; Masakatsu Nakane and Yoshio Ishikawa, Nihon University, Funabashi, Chiba, 274-8501, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2009-230: VOLTAGE HASH OF VARIOUS PROPELLANTS IN SELF-FIELD MAGNET OPLASMADYNAMIC THRUSTERS; Daisuke Nakata, Japan Aerospace Exploration Agency, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Kyoichiro Toki, Tokyo University of Agriculture and Technology, 2-24-16, Nakacho, Koganei-shi, Tokyo 184-8588, Japan; Yukio Shimizu, Japan Aerospace Exploration Agency, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan; Hitoshi Kuninaka, Japan Aerospace Exploration Agency, 3-1-1, Yoshinodai, Sagamihara-shi, Kanagawa 229-8510, Japan

2009-231: INVESTIGATION OF MHD INSTABILITIES IN AN APPLIED FIELD MPD THRUSTER BY MEANS OF MEASUREMENTS OF MAGNETIC FIELD FLUCTUATIONS; M. Zuin, R. Cavazzana, and E. Martines, Consorzioi RFX, Padova, Italy; P. Rossetti, M. Signori, M. Andrenucci, and F. Paganucci, Alta SpA, Pisa, Italy

2009-232: NUMERICAL STUDY ON THE EFFECTS OF PROPELLANT SPECIES IN A SELF-FIELD MAGNETOPLASMADYNAMIC ARCJET; H. Sato, The Graduate University for Advanced Studies, Sagamihara, Kanagawa, 229-8510, Japan; K. Kubota and I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2009-233: GALLIUM ELECTROMAGNETIC (GEM) THRUSTER PERFORMANCE MEASUREMENTS; Robert E. Thomas and Rodney L. Burton, University of Illinois, Urbana, IL, 61801; Kurt A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL, 35812

2009-234: FUTURE THRUSTER APPLICATION: COMBINATION OF NUMERICAL SIMULATION OF ECR ZONE AND PLASMA X-RAY BREMSSTRAHLUNG MEASUREMENT OF THE SWISSCASE ECR ION SOURCE; M. Bodendorfer, K. Altwegg, and P. Wurz, University of Bern, 3012 Bern Switzerland; H. Shea, Ecole Polytechnique FÃ©dÃ©rale de Lausanne, 2002 Neuchatel, Switzerland

2009-235: VICTOR KHRABROV - P–ONEER OF THE FIRST SPACE ELECTRIC PROPULSION SYSTEM DEVELOPMENT AND SPACE TESTS; M. N. Kazeev, Russian Research Center “Kurchatov Institute”, Moscow, Russia; K. N. Kozubskiy, Experimental Design Bureau, “Fakel”, Kaliningrad, Russia; G. A. Popov, Research Institute of Applied Mechanics and Electrodynamics of MAI

2009-236: USE A HELICON SOURCE TO SIMULATE ATMOSPHERIC RE-ENTRY PLASMA DENSITIES; Kristina M. Lemmer, Central Michigan University, Mt. Pleasant, MI, 48859, USA; Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA

2009-236a: ESA PROPULSION LAB AT ESTEC; J. Gonzalez del Amo, G. Saccoccia, and P. –E. Frigot, European Space Agency, ESTEC, Keplerlaan 1, 2201 AG Noordwijk, The Netherlands

2009-237: ELECTRIC PROPULSION ACTIVITIES AT ESA; J. Gonzalez del Amo and G. Saccoccia, European Space Agency, ESTEC, Keplerlaan 1, 22001 AG Noordwijk, The Netherlands

2009-237a: ELECTRIC PROPULSION ACTIVITIES AT ESA; J. Gonzalez del Amo and G. Saccoccia, European Space Agency, ESTEC, Keplerlaan 1, 22001 AG Noordwijk, The Netherlands

2009-238: DEVELOPMENT OF A 3D SPECTRAL BOLTZMANN SOLVER FOR PLASMA MODELING; Jacques C. Richard, Aerospace Engineering Department, Texas A&M University, College Station, Texas, 77843-3141

2009-239: NON-CHEMICAL SPACE PROPULSION RESEARCH ACTIVITIES AT NAGOYA UNIVERSITY; Akihiro Sasoh, Department of Aerospace Engineering, Nagoya University, Nagoya 464-8603, Japan

2009-240: MEASURING SPUTTER YIELDS OF CERAMIC MATERIALS; Michael Tartz, Thomas Heyn, Carsten Bundesmann and Horst Neumann, Leibniz-Institute of Surface Modification, Leipzig, 04318, Germany

2009-241: CHARACTERIZATION OF A HALL-EFFECT RADIAL PLASMA SOURCE; Robert L. Washeleski, Jason M. Makela, and Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2009-242: PERFORMANCE OF ELECTROSPRAY THRUSTERS; Jet Propulsion Laboratory California Institute of Technology, Pasadena, CA, 91109, USA

2009-244: DESIGN OF A TWO-STAGE PPT FOR CUBESAT APPLICATION; M. Coletti, Mars Space Ltd., Southampton, SO16 3QD, United Kingdom; R. Intini Marques and S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, United Kingdom

2009-246: EXPERIMENTAL AND NUMERICAL CHARACTERIZATION OF AN ABLATION-FED PULSED PLASMA THRUSTER PROTOTYPE; Erik M. Henrikson and Pavlos G. Mikellides, Arizona State University, Tempe, Arizona, 85287; Hani Kamhawi, NASA Glenn Research Center, Cleveland, Ohio, 44135

2009-248: HIGH THRUST APPTS FOR SPACECRAFT ORBIT CONTROL; Nickolay N. Antropov, Research Institute of Applied Mechanics and Electrodynamics, 4, Voloklamskoye shosse, Moscow, 125810, Russia; Michael N. Kazeev, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia; Vladimir P. Khodnenko, All-Russian Research Institute of Electromechanics, 101000, P. O. Box 496, Moscow, Russia

2009-249: ABLATION-FED DISCHARGE CHARACTERISTICS; Michel N. Kazeev and Vladimir F. Kozlov, Russian Research Centre Kurchatov Institute, 1, Kurchatov sq., Moscow, 123182, Russia

2009-250: THE TWO-STAGE PULSED PLASMA THRUSTER; R. Intini Marques and S. B. Gabriel, University of Southampton, Southampton SO17 1BJ, United Kingdom; F. de Souza Costa, Combustion and Propulsion Laboratory (LCP) of the Brazilian National Institute for Space Research (INPE), Cachoeira Paulista-SP, Brazil

2009-251: COOPERATION ACTIVITIES BETWEEN IRS AND THE UNIVERSITY OF TOKYO IN THE FIELD OF PULSED PLASMA THRUSTER DEVELOPMENT; Tony SchÃ¶nherr and Kimiya Komurasaki, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan; Matthias Lau, Georg Herdich, and Hans-Peter RÃ¶ser, UniversitÃ¤t Stuttgart, Stuttgart, Baden-WÃ¼rttemberg, 70569, Germany; Shigeru Yokota and Yoshihiro Arakawa, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan

2009-253: FLOWFIELD CALCULATION OF ELECTROTHERMAL PULSED PLASMA THRUSTERS FOR OSAKA INSTITUTE OF TECHNOLOGY SMALL SATELLITE; Yusuke Ishii, Hiroki Takagi, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan

2009-254: PERFORMANCE ENHANCEMENT OF ELECTROTHERMAL PULSED PLASMA THRUSTERS FOR OSAKA INSTITUTE OF TECHNOLOGY SMALL SATELLITE; Hiroki Takagi, Yusuki Ishii, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-Ku, Osaka 535-8585, Japan

2009-255: RESEARCH AND DEVELOPMENT ON COAXIAL PULSED PLASMA THRUSTER WITH FEED MECHANISM; Kyohei Umeda, Kouhei Shintani, Yuki Kubota, Yohei Kitazono, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Department of Aerospace Engineering, 6-6 Asahigaoka hino, Tokyo, 191-0065, Japan

2009-257: COMPATIBILITY STUDY OF LOW TOXICITY PROPELLANT DECOMPOSED GAS FOR DC ARCJET THRUSTERS; Hirokazu Tahara, Yusuke Okamachi, and Sadanori Nakagawa, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan; Taiichi Nagata, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki, 305-8505

2009-258: TWO-DIMENSIONAL LTE MODELING OF A LOW-POWER ARGON ARCJET THRUSTER; Hai-Xing Wang and Shao-Xia Jia, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China; Xi Chen, Tsinghua University, Beijing, 100084, China; Wenxia Pan, Institute of Mechanics, Chinese Academy of Sciences, Beijing, 100190

2009-259: EXPERIMENTALLY CHARACTERIZING THE PLUME OF A DIVERGENT CUSPED-FIELD THRUSTER; Stephen R. Gildea and Manuel MartÃnez-SÃ¡nchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA; Michael R. Nakles and William A. Hargus, Jr., Air Force Research Laboratory Spacecraft Propulsion Branch, Edwards Air Force Base, California, 93524, USA

2009-260: DIVERGENCE OF A PROPULSIVE PLASMA FLOW EXPANDING THROUGH A MAGNETIC NOZZLE; Justin M. Little and Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08544, USAA

2009-262: MAGNETIC DETACHMENT AND PLUME CONTROL IN ESCAPING MAGNETIZED PLASMAS; Paul F. Schmit and Nathaniel J. Fisch, Princeton University, Princeton, NJ, 08540, USA

2009-263: KINETIC SIMULATIONS OF ION BEAM NEUTRALIZATION; Joseph Wang, University of Southern California, Los Angeles, CA 90089-1192, USA; Hideyuki Usui, Kobe University, Kobe, Japan

2009-265: PULSED PLASMOID PROPULSION: THE ELF THRUSTER; John Slough and David Kirtley, MSNW, Redmond, WA 98052, USA; Thomas Weber, University of Washington, Seattle, WA 98195, USA

2009-267: HAYABUSA ASTEROID EXPLORER POWERED BY ION ENGINES ON THE WAY TO EARTH; Hitoshi Kuninaka, Kazutaka Nishiyama, Yukio Shimizu, Ikko Funaki, Hiroyuki Koizumi, Satoshi Hosoda, and Daisuke Nakata, Lunar Planetary Program Group, Japan Aerospace Exploration Agency, Yoshinodai, Sagamihara, Kanagawa 229, Japan

2009-270: ELECTRIC PROPULSION AT SPACE SYSTEMS/LORAL; Ronald L. Corey and David J. Pidgeon, Space Systems/Loral, Palo Alto, CA, 94303

2009-272: PERFORMANCE CHARACTERISTICS OF VERY LOW POWER CYLINDRICAL HALL THRUSTERS; Hirokazu Tahara and Takuma Tonari, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan

2009-274: SURFACE MORPHOLOGY AND LIFETIME ASSESSMENT OF RE-GENERABLE FIELD-EMISSION CATHODES AT ELEVATED BACKGROUND PRESSURE; Jason M. Makela, Rob Washeleski, and Lyon B. King, Michigan Technological University, Houghton, Michigan, 49931, USA

2009 FILE DIRECTORY

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2011 INDEX

2011-001: VERNIER PROPULSION SYSTEM FOR SMALL EARTH REMOTE SENSING SATELLITE “CANOPUS-V”; Alexander V. Gorbunov, Vladimir P. Khodnenko, and Alexander V. Khromov, Federal Government Unitary Research and Production Enterprise – All Russian Research Institute of Electromechanics with Plant Named After A. G. Iosifian, VNIIEM: POB 496, Glavpochtamt, Moscow, 101000, Russia; Vyacheslav M. Murashko, Alexander I. Koryakin, Valery S. Zhosan, and Gennady S. Grikhin, FSUE Experimental Design Bureau “Fakel” (OKB “Fakel”): 181. Moskovsky avenue, Kaliningrad Region, 236001, Russia; Vladimir N. Galayko and Nikolay M. Katasonov, JSC Scientific & Industrial Centre “Polus”: 56 ”B”, Kirov avenue, Tomsk, 634050, Russia

2011-002: PHYSICAL FEATURES AND PARAMETERS CALCULATIONS OF A HALL THRUSTER; M. H. Moghimi, M.Sc. in Aerospace Engineering, Sharif University of Technology, Tehran, 1581955711, Iran

2011-003: A PERFORMANCE COMPARISON OF XENON AND KRYPTON PROPELLANT ON AN SPT-100 HALL THRUSTER; Michael R. Nakles, ERC, INc., Edwards Air Force Base, CA, 93524; William A. Hargus, Jr., Air Force Research Laboratory, Edwards Air Force Base, CA 93524; Jorge J. Delgado and Ronald L. Corey, Space Systems/Loral, Palo Alto, CA 94303

2011-004: ESA PROPULSION LABORATORY (EPL); J. Gonzalez del Amo and A. Bulit, European Space Agency, ESTEC, 2201 AZ Noordwijk ZH, The Netherlands

2011-007: THE MAIN PHYSICAL FEATURES OF THE MOROZOV’S TYPE SPT AND ELECTRIC PROPULSION CLASSIFICATION; V. Kim, Dr, Moscow Aviation Institute, Moscow, 125080, Russia

2011-008: RESULTS OF THE PLUME CHARACTERISTICS STUDY FOR SPT OPERATION ON DIFFERENT MODES; V. Kim, A. S. Arkhipov, and E. K. Sidorenko, Moscow Aviation Institute, Moscow, 125080, Russia

2011-009: OVERVIEW OF INDIUM LMIS FOR THE NASA-MMS MISSION AND ITS SUITABILITY FOR AN IN-FEEP THRUSTER ON LISA; M. Tajmar, Department of Aerospace Engineering, KAIST, Daejeon, Republic of Korea, Department of Aerospace Engineering, University of Applied Sciences, 2444 Wiener Neustadt, Austria

2011-010: A SIMPLE SEMI-ANALYTIC MODEL FOR OPTIMUM SPECIFIC IMPULSE INTERPLANETARY LOW THRUST TRAJECTORIES; David Y. Oh and Damon Landau, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2011-011: DEVELOPMENT STATUS OF THE ESA MICRO-NEWTON THRUST BALANCE; J. PÃ©rez Luna, C. H. Edwards, and J. Gonzalez del Amo, European Space Agency, ESTEC, Noordwijk, 2201 AZ, The Netherlands; B. Hughes, National Physical Laboratory, Teddington, Middlesex, United Kingdom

2011-012: SIMULATION OF THE SPACECRAFT ELECTRIC PROPULSION INTERACTION ON DUBAISAT-2 USING SPIS; Juyoung Lee, Alexander Reissner, and Martin Tajmar, Department of Aerospace Engineering, KAIST, Daejeon, Republic of Korea; Yunhwang Jeong, Satrec Initiative, Daejeon, Republic of Korea

2011-013: PEFORMANCE VERIFICATION OF THE ÂµNRIT-2.5 THRUSTER ON THE NANOBALANCE FACILITY; D. Di Cara and L. Massotti, ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands; S. Cesare, F. Musso, and G. Castorina, Thales Alenia Space Italia S.p.A., Strada Antica di Collegno, 253, 10146 Turin – Italy; D. Feili and B. Lotz, I. Physics Institute of Justus Liebig University, Giessen, D-35392, Germany

2011-014: EXPERIMENTAL INVESTIGATIONS ON THE INFLUENCE OF THE FACILITY BACKGROUND PRESSURE ON THE PLUME OF THE RIT-4 ION ENGINER; A. Bulit, J. Perez Luna, and J. Gonzalez Del Amo, European Space Agency, ESTEC, 2201AZ Noordwijk ZH, The Netherlands; B. Lotz and D. Feili, University of GieÃŸen, 35392 GieÃŸen, Germany; H. Leiter, Astrium GmbH BL equipment and Propulsion, 7421 MÃ¶ckmÃ¼hl, Germany

2011-015: PULSED PLASMOID PROPULSION: AIR-BREATHING ELECTROMAGNETIC PROPULSION; David Kirtley, John Slough, and Chris Pihl, MSNW LLC, Redmond, WA 98052, USA; Eric Meier and Richard Milroy, University of Washington, Seattle, WA, USA

2011-017: HIGH HEAT RESISTANT COATINGS BY MEANS OF GAS TUNNEL TYPE PLASMA SPRAYING; Akira Kobayashi, Osaka University, Ibaraki, Osaka 567-0047, Japan; Yasutaka Ando, Ashikaga Institute of Technology, Ashikaga, Tochigi 326-8558, Japan; Kazuya Kurokawa, Hokkaido University, Sapporo, Hokkaido 060-8628, Japan

2011-018: DEMONSTRATION OF LASER-INDUCED FLUORESCENCE ON A KRYPTON HALL EFFECT THRUSTER; William A. Hargus, Jr., Gregory M Azarnia, and Michael R. Nakles, Air Force Research Laboratory, Edwards Air Force Base, CA 93524

2011-019: IMPACT OF THE CHANNEL WIDTH ON HALL THRUSTER DISCHARGE PROPERTIES AND PERFORMANCES; A. Lejeune, K. Dannenmayer, G. Bourgeois, and S. Mazouffre, ICARE – CNRS, 1c Av. de la Recherche Scientifique, 45071 OrlÃ©ans, France; M. Guyot and S. Denise, GEMaC, Versailees St-Quentin University, 78035 Versailles, France

2011-020: PERFORMANCE EVALUATION OF A 20 KW HALL EFFECT THRUSTER; S. Zurbach and N. Cornu, Snecma, Safran Group, Space Propulsion Division, 27208 Vernon, France; P. Lasgorceix, CNRS, ICARE Laboratory, 45071 OrlÃ©ans, France

2011-021: SPACECRAFT PLASMA ENVIRONMENT: FORMING, MODELING AND IMPACT EFFECTS; Ekaterina M. Tverdokhlebova, Anatoly G. Korsun, Flur F. Gabdullin, and Michail Yu. Kurshakov, Central Research Institute of Machine Building (FGUP TsNIImash), Korolev, Moscow region, 141070, Russia; Andrey B. Nadiradze, Moscow Aviation Institute (MAI (GTU)), Moscow, Russia

2011-023: ROLE OF HIGH-FREQUENCY WAVES IN PROCESS OF ELECTRON CONDUCTIVITY IN SPT WITH HIGH SPECIFIC IMPULSE; Dmitriy A. Tomilin and Oleg A. Gorshkov, SSC Keldysh Research Centre, Moscow, 125438, Russia

2011-024: INVESTIGATION OF DISCHARGE POWER INFLUENCE ON EROSION RATE OF SPT DISCHARGE CHAMBER USING SPECTROSCOPIC METHOD; Arseniy V. Shmelev and Alexander S. Lovtsov, SSC Keldysh Research Centre, Moscow, 125438, Russia

2011-025: THE EFFECT OF WALL EROSION ON THE PERFORMANCE OF HALL THRUSTERS; Andrey A. Shagayda, Oleg A. Gorshkov, and Dmitry A. Tomilin, SSC Keldysh Research Centre, Moscow, 125438, Russia

2011-026: THE DEVICE FOR ELECTRIC PROPULSION LATERAL THRUST VECTOR COMPONENTS MEASUREMENT; V. A. Muravlev, E. R. Khabibullin and V. N. Shutov, SSC Keldysh Research Centre, Moscow, 125438, Russia

2011-028: THE ASSESSMENT OF INTERACTIONS BETWEEN SPACECRAFT AND ELECTRIC PROPULSION SYSTEMS PROJECT; MatÃas Wartelski, Carlos Ardura, and Christophe Theroude, Astrium Satellites, Toulouse, 31400, France; Alexander Reissner, FOTEC Forschungs – und Technologietransfer GmbH, 2700 Wiener Neustadt, Austria, Korea Advanced Institute of Science and Technology, Daejeon 3035-701, South Korea; Martin Tajmar, University of Applied Sciences Wiener Neustadt, 2700 Wiener Neustadt, Austria, Korea Advanced Institute of Science and Technology, Daejeon 305-702, South Korea; Eric Gengembre, European Space Agency, ESTEC, 2201AZ Noordwijk ZH, The Netherlands

2011-030: THE TECHNICAL CHALLENGES OF USING CAVITY RING-DOWN SPECTROSCOPY TO STUDY HALL THRUSTER CHANNEL EROSION; Wensheng Huang, Alec D. Gallimore, and Timothy B. Smith, University of Michigan, Ann Arbor, MI, 48109, U.S.A.; Azer P. Yalin, Colorado State University, Fort Collins, CO 80521, U.S.A.

2011-031: ANALYSIS OF MICRO-VACUUM ARC THRUSTERS FOR EARTH-ORBITING AND LUNAR MISSIONS; Therese R. Suaris, George Washington University, Washington, D.C. 20052, USA; NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA; Michael Keidar, George Washington University, Washington, D.C. 20052, USA

2011-032: OPTIMIZATION OF THE OPERATING PARAMETERS FOR A 20 MN CLASS ION THRUSTER; Hiroshi Nagano and Kenichi Kajiwara, Japan Aerospace Exploration Agency, Tsukuba, 305-8505, Japan; Yukio Hayakawa, Japan Aerospace Exploration Agency, Chofu, 182-8522, Japan; Toshiyuki Ozaki and Yukikazu Kasai, Mitsubishi Electric Corporation, Kamakura, 247-8520, Japan

2011-033: OPTIMUM DESIGN GUIDELINES ON MPD THRUSTERS AROUND CRITICAL CURRENT; Yoshitaka Takahashi, Ryo Ohtake, Masakatsu Nakane, and Yoshio Ishikawa, Nihon University, Fumabashi, Chiba 274-8501, Japan; Kenichi Kubota, Japan Aerospace Exploration Agency, Chofu, Tokyo 182-8522, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 229-8510, Japan

2011-034: DEVELOPMENT OF ELECTROTHERMAL PULSED PLASMA THRUSTER SYSTEM FLIGHT-MODEL FOR THE PROITERES SATELLITE; Masamichi Naka, Ryuta Hosotani, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan; Yosuke Watanabe, Osaka University, Toyonaka, Osaka 560-8531, Japan

2011-035: DEVELOPMENT OF OSAKA INSTITUTE OF TECHNOLOGY NANO-SATELLITE “PROITERES” WITH ELECTROTHERMAL PULSED PLASMA THRUSTERS; Jun-ichi Ozaki, Tomoyuki Ikeda, Tatsuya Fujiwara, Masaya Nishizawa, Shunsuke Araki, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan; Yosuke Watanabe, Osaka University, Toyonaka, Osaka 560-8531, Japan

2011-036: COMPATIBILITY STUDY OF LOW TOXICITY PROPELLANT GAS “HAN” FOR DC ARCJET THRUSTERS; Hirokazu Tahara, Yusuke Okamachi, Katsuya Fujita, Kazuya Nakagawa, and Masamichi Naka, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan; Taiichi Nagata and Ideo Masuda, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505, Japan

2011-037: FLOWFIELD CALCULATION OF ELECTROTHERMAL PULSED PLASMA THRUSTERS FOR THE PROITERES SATELLITE; Hirokazu Tahara, Yusuke Ishii, Masato Tanaka, and Masamichi Naka, Osaka Institute of Technology, Asahi-Ku, Osaka, 535-8585, Japan; Yosuke Watanabe, Osaka University, Toyonaka, Osaka 560-8531, Japan

2011-038: OPTIMIZATION OF ACCELERATION CHANNEL STRUCTURE AND MATERIAL FOR MAGNETIC-LAYER-TYPE HALL THRUSTERS; Tomoyuki Ikeda, Tsuyoshi Fujita, Naru Sugimoto, Jun-ichi Ozaki, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-ku, Osaka 535-8585, Japan; Yosuke Watanabe, Osaka University, Toyonaka, Osaka 560-8531, Japan

2011-039: RESEARCH AND DEVELOPMENT OF VERY LOW POWER CYLINDRICAL HALL THRUSTERS FOR NANO-SATELLITES; Tomoyuki Ikeda, Kazuya Togawa, Takahiro Nishida, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-ku, Osaka 535-8585, Japan; Yosuke Watanabe, Osaka University, Toyonaka, Osaka 560-8531, Japan

2011-041: NEW GENERATION OF SPT-100; O. A. Mitrofanova, R. Yu. Gnizdor, V. M. Murashko, A. I. Koryakin and A. N. Nesterenko, EDB “Fakel”, Kaliningrad, 236001, Russia

2011-042: CHARACTERISTIC RELATIONSHIP BETWEEN DIMENSIONS AND PARAMETERS OF A HYBRID PLASMA THRUSTER; M. Yu. Potapenko and V. V. Gopanchuk, FSUE EDB Fakel, Kaliningrad, 236001, Russia

2011-043: MODELING PHYSICAL PROCESSES IN CAMILA HALL THRUSTER BY PIC METHOD; Igal Kronhaus, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; Alexander Kapulkin, Asher Space Research Institute, Technion – Israel Institute of Technology, Haifa 32805, Israel; Moshe Guelman, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa 32000, Israel; Benveniste Natan, Faculty of Aerospace Engineering, Technion-Israel Institute of Technology, Haifa 32000, Israel

2011-044: PERFORMANCE STUDY OF PULSED PLASMA THRUSTER USING OF A NEW KIND OF ELECTRODE; DONG Lei, KANG Xiaoming, and ZHAO Wansheng, School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai, 200240, China; HOU Dali, PetroChina, Shanghai, 200240, China

2011-045: THE THRUST OF A COLLISIONAL MAGNETIZED PLASMA; A. Fruchtman and G. Makrinich, H.I.T. – Holon Institute of Technology, Holon 58102, Israel

2011-046: CAMILA HALL THRUSTER: NEW RESULTS; A. Kapulkin, V. Balabanov, M. Rubanovich, and E. Behar, Asher Space Research Institute – Technion, I. I. T., Haifa, 32000, Israel; L. Rabinovich and A. Warshavsky, Rafael, Haifa, 31021, Israel

2011-047: PLASMA-WAVE INTERACTION IN A HELICON THRUSTER; Daniel MartÃnez and Eduardo Ahedo, Universidad PolitÃ©cnica de Madrid, Madrid 28040, Spain

2011-048: HYBRID MODEL SIMULATION OF A PLASMA PLUME IN A MAGNETIC NOZZLE; Jaume Navarro and Eduardo Ahedo, E.T.S. Ingenieros AeronÃ¡uticos, Plaza Cardenal Cisneros, Madrid 28040, Spain

2011-049: CONSTANT-POWER PERFORMANCE AND PLUME MEASUREMENTS OF A NESTED-CHANNEL HALL-EFFECT THRUSTER; Raymond Liang and Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA

2011-050: ON ELECTRON INERTIA AND CURRENT AMBIPOLARITY IN MAGNETIC NOZZLE MODELS; Eduardo Ahedo and Mario Merino, E.T.S. Ingenieros AeronÃ¡uticos, Plaza Cardenal Cisneros, Madrid 28040, Spain

2011-051: FLIGHT TIMES TO THE HELIOPAUSE USING A COMBINATION OF SOLAR AND RADIOISOTOPE ELECTRIC PROPULSION; Andreas Ohndorf, German Aerospace Center (DLR), P.O. 1116, Wessling, 82230, Germany; Bernd Dachwald, FH University of Applied Sciences, Hohenstaufenallee 6, Aachen, 52064, Germany; Wolfgang Seboldt, German Aerospace Center (DLR), Linder Hoehe, Cologne, 51147, Germany; Horst W. Loeb and Karl-Heinz Schartner, University of Giessen, Heinrich Buff Ring 16, Giessen, 35392, Germany

2011-052: AN INTERSTELLAR – HELIOPAUSE MISSION USING A COMBINATION OF SOLAR/RADIOISOTOPE ELECTRIC PROPULSION; Horst W. Loeb and Karl-Heinz Schartner, University of Giessen, Heinrich-Buff-Ring 16, Giessen, D-35392 Giessen, Germany; Bernd Dachwald, FH University of Applied Sciences, Hohenstaufenalle 6, Aachen, D-52064, Germany; Andreas Ohndorf, German Aerospace Center (DLR), P.O. 116, Wessling, D-82230, Germany; Wolfgang Seboldt, German Aerospace Center (DLR), Linder HÃ¶he, Cologne, 51147, Germany

2011-053: HIGH CURRENT LANTHANUM HEXABORIDE HOLLOW CATHODES FOR HIGH POWER HALL THRUSTERS; Dan M. Goebel and Emily Chu, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109 USA

2011-054: A POTENTIAL OF MINIATURE ELECTRODYNAMIC TETHERS TO ENHANCE CAPABILITIES OF FEMTOSATELLITES; Iverson C. Bell, III, and Brian E. Gilchrist, The University of Michigan, Ann Arbor, Michigan 48109, USA; Jesse K. McTernan and Sven G. BilÃ©n, The Pennsylvania State University, University Park, Pennsylvania 16802, USA; Robert P. Hoyt and Nestor R. Voronka, Tethers Unlimited, Inc. Bothell, Washington 98011, USA; Mason A. Peck, Cornell University, Ithaca, New York, 14853, USA

2011-055: VALIDATION DATA FOR ION THRUSTER BEAM OPTICS SIMULATION; Yoshinori Nakayama, National Defense Academy of Japan, Yokosuka, Kanagawa 239-8686, Japan

2011-056: RESEARCH AND DEVELOPMENT OF ELECTRODELESS PLASMA THRUSTERS USING HIGH-DENSITY HELICON SOURCES: THE HEAT PROJECT; S. Shinohara, H. Nishida, K. Yokoi, and T. Nakamura, Tokyo University of Agriculture and Technology, Koganei, Tokyo 184-8588, Japan; T. Tanikawa, Tokai University, Hiratsuka, Kanagawa 259-1292, Japan; T. Hada, F. Otsuka, T. Motomura, and E. Ohno, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; I. Funaki and T. Matsuoka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252-5210, Japan; K. P. Sharmrai and T. S. Rudenko, Institute of Nuclear Research, Nauki, Kiev 03680, Ukraine

2011-057: BASIC EXPERIMENT ON A MAGNETOPLASMA THRUSTER DRIVEN BY PHASE-CONTROLLED RF; Y. Yasaka, M. Yamamoto, Y. Hayashi, S. Nakamoto, H. Takeno, and H. Yonemori, Graduate School of Engineering, Kobe University, Nada-ku, Kobe 657-8501, Japan

2011-058: ELECTRIC SOLAR WIND SAIL PROPULSION SYSTEM DEVELOPMENT; Pekka Janhunen, Petri Toivanen, Sini Merikallio and Jouni Polkko, Finnish Meteorological Institute, Helsinki, POB 503, FI-00101, Finland; Edward HaeggstrÃ¶m, Henri SeppÃ¤nen, Risto Kurppa, Jukka Ukkonen and Tuomo Ylitalo, University of Helsinki, Department of Physics, Helsinki, Finland; Sergiy Kiprich, National Science Center Kharkov Institute of Physics and Technology, Kharkov, Ukraine; Hannu Koivisto, Taneli Kalvas, Olli Tarvainen, and Janne Kauppinen, University of JyvÃ¤kylÃ¤, Accelerator Laboratory, JyvÃ¤kylÃ¤, Finland; Gregor Thornell, Henrik Kratz and Johan Sundqvist, AngstrÃ¶m Space Technology Centre, Uppsola University, Sweden; Tor-Arne GrÃ¶nland, Hakan Johansson and Pelle Rangsten, Nanospace, Uppsala, Sweden; Emil Vinterhav, OHB Sweden, Stockholm, Sweden; Mart Noorma, Jouni Envall, Silver LÃ¤tt, Viljo Allik, and Kaupo Voormansik, Tartu Observatory and University of Tartu, Estonia; Urmas Kvell and Jean-Pierre Lebreton, ESA/ESTEC, Noordwijk, The Netherlands; Martti Hallikainen and Jaan Praks, Aalto U niversity, Espoo, Finland; Olaf KrÃ¶mer and Roland Rosta, German Aerospace Center DLR, Bremen, Germany; Pekka Salminen, Skytron Oy, Toijala, Finland; Giovanni Mengali, Alessandro Quarta, and Generoso Aliasi, University of Pisa, Italy; Salvo Marcuccio, Pierpaolo Pergola, and Nicola Giusti, Alta, Pisa, Italy

2011-059: TRANSITIONAL REGIME IN THE START-UP PROCESS OF CONVENTIONAL HALL THRUSTERS; R. Santos and E. Ahedo, EIAE, Universidad Politecnica de Madrid, Madrid, 28040, Spain; Y. Raitses and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ 08543, USA

2011-060: LOW-FREQUENCY WAVE EXPERIMENTAL INVESTIGATIONS, TRANSPORT AND HEATING OF ELECTRONS IN STATIONARY PLASMA THRUSTER SPT; A. N. Vesselovzorov and E. D. Dlougach, National Research Centre ‘Kurchatov Institute’ Moscow, Russia; V. A. Smirnov, National Research Centre ‘Kurchatov Institute’ Moscow, Russia

2011-061: HIGH POWER NUCLEAR ELECTRIC PROPULSION; Richard Blott, Director, Space Enterprise Partnerships Ltd, Eastergate, West Sussex, PO20 3SJ, UK; Anthony Donaldson, Specialist System Concepts, Rolls Royce plc, Derby, DE21 7XX, UK; Professor Marino Mazzini, Director, Acta Srl, Pisa, 56100, Italy

2011-062: VERIFICATION – ELECTRIC PROPULSION’S ACHILLES HEEL; Richard Blott, Director, Space Enterprise Partnerships Ltd. Eastergate, West Sussex, PO20 3SJ, UK; Dr. David Robinson, Director, Psi-tran Ltd. Sunbury, Middlesex, TW16 5AR, UK; Professor Stephen Gabriel, Head of Aeronautics and Astronautics, Southampton University, Southampton, Hampshire, SO16 3QD, UK

2011-063: EXPERIMENTAL INVESTIGATION AND NUMERICAL MODELING OF ELECTRIC HEATING RATE IN A GENERIC ELECTRIC PROPULSION; S. Reichel, R. Groll, and H. J. Rath, ZARM – University of Bremen, Bremen, 28359, Germany

2011-064: FEASIBILITY OF HIGH POWER MULTI-MODE EPS DEVELOPMENT BASED ON THE THRUSTER WITH ANODE LAYER; Alexander V. Semenkin, Leonid E. Zakharenkov, and Alexander E. Solodukhin, SSC Keldysh Research Center, 8 Onezhskaya street, Moscow, 125438, Russia

2011-065: POROUS TUNGSTEN CROWN MULTIEMITTER TESTING PROGRAMME USING THREE DIFFERENT GRAIN SIZES AND SINTERING PROCEDURES; I. Vasiljevich, N. Buldrini, and F. Plesescu, Fotec Forshungs-und Technologietransfer GmbH, Wr. Neustadt, Austria; M. Tajmar, University of Applied Sciences Wiener Neustadt, Austria, Korea Advanced Institute of Science and Technology (KAIST), Daejeon 305-701, Korea; M. Betto, J. Gonzales del Amo, ESA-ESTEC, Noordwijk, The Netherlands

2011-066: EFFECT OF ION SPUTTERING ON TRANSMISSION OF COVERGLASS WITH MAGNESIUM FLUORIDE COATING; Azer Yalin, James Topper, Casey Farnell, and Greg Yoder, Colorado State University, Fort Collins, CO, 80523, USA; Bao Hoang and Ron Corey, Space Systems/Loral, Palo Alto, CA, 94303, USA

2011-067: VELOCITY PROFILES OF BORON ATOMS SPUTTERED FROM BORON NITRIDE BY LOW ENERGY XENON IONS; Lei Tao and Azer Yalin, Colorado State University, Fort Collins, CO, 80523, USA

2011-068: SENSITIVITY IMPROVEMENTS TO LASER SENSOR FOR BORON NITRIDE EROSION IN HALL THRUSTERS; Brian C. Lee, Lei Tao, Joshua M. Taylor, and Azer P. Yalin, Colorado State University, Fort Collins, CO, 80523, USA; Alec Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA

2011-070: NUMERICAL INVESTIGATIONS OF A CYLINDRICAL HALL THRUSTER; K. Matyash, Max-Planck-Institut fÃ¼r Plasmaphysik, EURATOM Association, Greifswald, D-17491, Germany; R. Schneider, Greifswald University, Greifswald, D-17487, Germany; O. Kalentev, Max-Planck-Institut fÃ¼r Plasmaphysik, EURATOM Assocation, Greifswald, D-17491, Germany; Y . Raitses and N. J. Fisch, Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543, USA

2011-073: THE APPLICATION OF THE LASER PLASMA COMBINED PROPULSION SUBSYSTEM IN GOD’S GRACE SYSTEM; Guo Zongshuai, N.E. Zhukovskiy National Aerospace University “Kharkov Aviation Institute” 61070, Khakov, Kharkov oblast, Ukraine, Nan Chang Institute of Technology, 330013, Nan Chang, Jiangxi, China; Qiu Xiaolin and Guo Pengfei, Nan Chang Institute of Technology, 330013, Nan Chang, Jiangxi, China; Qian Weiding, Kharkov National Automobile and Highway University, 61024, Khakov, Kharkov oblast’, Ukraine

2011-076: TWO-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF A MICRO RF ION THRUSTER; Yoshinori Takao, Koji Eriguchi, and Kouichi Ono, Kyoto University, Kyoto, 606-8501, Japan

2011-077: NEAR-WALL CONDUCTIVITY EFFECT UNDER SPACE-CHARGE-SATURATED SHEATH IN THE HALL THRUSTER; Fengkui Zhang and Yongjie Ding, College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, People’s Republic of China, HIT Plasma Propulsion Laboratory, Harbin Institute of Technology, Harbin 150001, People’s Republic of China; Xudong Na and Xiande Wu, College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, People’s Republic of China

2011-078: EXPERIMENTAL AND NUMERICAL STUDY ON A HALL THRUSTER INSULATOR EROSION; Shinatora Cho, The University of Tokyo, Tokyo, 113-8656, Japan; Shigeru Yokota, Nagoya University, Nagoya, 464-8603, Japan; Ryotaro Kaneko, Kimiya Komurasaki, and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2011-079: PROGRESS IN DEVELOPMENT FOR HELICON PLASMA THRUSTERS BY USED OF THE ROTATING ELECTRIC FIELD (LISSAJOUS ACCELERATION); Takeshi Matsuoka and Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan; Timofei S. Rudenko and Konstantin P. Shamrai, Institute of Nuclear Research, Nauki, Kiev 03680, Ukraine; Shuhei Satoh and Takayasu Fukino, University of Tsukuba, Tsukuba, Ibaraki, 305-8573, Japan; Takahiro Nakamura, Kenji Yokoi, Hiroyuki Nishida, and Shunjiro Shinohara, Tokyo University of Agriculture and Technology, Koganei, Tokyo 184-8588, Japan; Tohru Hada, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Takao Tanikawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan

2011-080: DEVELOPMENT OF VACUUM ARC THRUSTERS AND DIAGNOSTIC TOOLS; Mathias Pietzka, Stefan Kirner, Marina Kauffeldt, Claudia Arens, JosÃ©-Luis Marques-Lopez, GÃ¼nter Forster and Jochen Schein, University of the Federal Armed Forces, Werner-Heisenberg-Weg 39, 85577 Neubiberg, Germany

2011-083: NANOCRYSTALLINE GRAPHITE: ADVANCED FIELD EMISSION CATHODE MATERIAL FOR A SPACECRAFT NEUTRALIZER; Alexander Y. Poroykov, Yuri A. Mankelevich, Andrewy A. Pilevsky, Alexander T. Rakhimov, Boris V. Seleznev, Nikolay V. Suetin and Mikhail A. Timofeyev, Moscow State University, Skobeltsyn Nuclear Physics Institute, Moscow, 111991, Russia

2011-084: HYDROGEN CHEMISTY AND TRANSPORT COEFFICIENTS FOR SIMULATION OOF THE DC-RF THRUSTER TIHTUS WITH THE LOOSELY COUPLED NAVIER-STOKES CODE SINA; U. Bauder, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart, 70569 Stuttgart, Germany; M. Auweter-Kurtz, German Aerospace Academy ASA, 71304 BÃ¶blingen, Germany

2011-085: ELECTRON PROPULSION CABLES FOR MILLI-NEWTON THRUSTERS

2011-086: HYPERSONIC PLASMA PLUME EXPANSION IN SPACE; Mario Merino, Eduardo Ahedo, Claudio Bombardelli, Hodei Urrutxua, and JesÃºs PelÃ¡ez, Universidad PolitÃ©cnica de Madrid, 28040 Madrid (Spain)

2011-087: A REORBITER FOR GEO LARGE SPACE DEBRIS USING ION BEAM IRRADIATION; Shoji Kitamura, Yukio Hayakawa, and Satomi Kawamoto, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan

2011-088: THREE-DIMENSIONAL FULLY KINETIC PARTICLE-IN-CELL MODEL FO HALL-EFFECT THRUSTER; F. Taccogna and P. Minelli, Istituto di Metodologie Inorganiche e di Plasmi, Consiglio Nazionale delle Ricerche, Bari, 70126, Italy

2011-089: THREE-DIMENSIONAL PLUME SIMULATION OF MULTI-CHANNEL HALL EFFECT THRUSTER; F. Taccogna and P. Minelli, Istituto di Metodologie Inorganiche e di Plasmi, Consiglio Nazionale delle Ricerche, Bari, 70126, Italy; G. Coduti, D. Pagano and F. Scortecci, AEROSPAZIO Tecnologie S.r.l., Rapolano Terme, Siena, 53040, Italy; A. Garulli, Dipartimento di Ingegneria dell’Informazione, UniversitÃ¡ di Siena, Siena, 53100, Italy

2011-090: EXTRA-ZODIACAL-CLOUD ASTRONOMY VIA SOLAR ELECTRIC PROPULSION; Scott W. Benson, Robert D. Falck, and Steven R. Oleson, NASA Glenn Research Center, Cleveland, Ohio, 44135, USA; Matthew A. Greenhouse, Jeffrey W. Kruk, Jonathan P. Gardner, Harley A. Thronson, and Frank J. Vaughn, NASA Goddard Space Flight Center, Grennbelt, Maryland, 20771, USA; Dale J. Fixsen, University of Maryland, College Park, Maryland, 20742, USA

2011-093: THE NEW DLR HIGH VACUUM TEST FACILITY STG-ET; Andreas Neumann, AndrÃ© Holz, Georg Dettleff and Klaus Hannemann, DLR Deutsches Zentrium fÃ¼r Luft-und Raumfahrt, 37073 GÃ¶ttingen, Bunsenstrasse 10, Germany; Hans-Peter Harmann, Dr. Harmann Technologieberatung, 88131 Lindau, Bleicheweg 20a, Germany

2011-094: STUDY FOR THE INFLUENCE OF STATIONARY PLASMA THRUSTER OPERATING MODES ON ITS ELECTROMAGNETIC EMISSION; Andrey Plokhikh, Nikolay Vazhenin, Vladimir Kim, Evgeniy Sidorenko, and Galina Soganova, Research Institue of Applied Mechanics and Electrodynamics of MAI, 5 Leningradskoye shosse, Moscow, 125080 Russia

2011-095: POWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE ETCA; Eric Bourguignon, StÃ©phane Fraselle, and Thierry Scalais, Thales Alenia Space ETCA, B-6032 Mont-sur-Marchienne, Belgium

2011-096: USE OF A “WIDE DYNAMIC RANGE” ELECTRONIC FLOW REGULATOR TO INCREASE THE FLEXIBILITY AND VERSATILITY OF ELECTRIC AND COLD GAS SMALL PROPULSION SYSTEMS; G. Matticari, M. Materassi, G. Noci, L. Fallerini, and P. Siciliano, Thales Alenia Space Italia, Site of Campi Bisenzio (Florence), 50013, Italy

2011-097: HELICON DOUBLE LAYER THRUSTER PERFORMANCE ENHANCEMENT VIA MANIPULATION OF MAGNETIC TOPOLOGY; S. J. Pottinger, T. Harle and V. J. Lappas, University of Surrey, Guildford, GU2 7XH, United Kingdom; C. Charles and R. W. Boswell, The Australian National University, Canberra, ACT 0200 Australia; M. Perren, EADS Astrium, 6 rue Laurent Pichat, 75216 Paris Cedex 16, France

2011-098: EFFECTS OF HYDROGEN PARTIAL PRESSURE WITHIN THE VACUUM FACILITY ON PLUME FOCUSING OF A HALL THRUSTER; Li Jie, Yu Daren, Ning Zhongxi, and Li Yong, Harbin Institute of Technology, Harbin, Heilongjiang, 150001, China

2011-099: THE QUAD CONFINEMENT THRUSTER – PRELIMINARY PERFORMANCE CHARACTERIZATION AND THRUST VECTOR CONTROL; Aaron Knoll, Byron Melly, and Vaios Lappas, University of Surrey, Guildford, Surrey, GU2 7XH, United Kingdom

2011-101: MULTISCALE MODELING OF HALL THRUSTERS; Lubos Brieda and Michael Keidar, The George Washington University, Washington, D.C. 20052

2011-102: LOW-THRUST MANEUVERS FOR THE EFFICIENT CORRECTION OF ORBITAL ELEMENTS; A. Ruggiero and P. Pergola, Alta, Pisa, 56100, Italy; S. Marcuccio and M. Andrenucci, University of Pisa, Pisa, 56100, Italy

2011-103: THRUST MEASUREMENTS OF A SMALL SCALE HELICON DOUBLE LAYER THRUSTER; T. Harle, S. J. Pottinger, and V. J. Lappas, University of Surrey, Guildford, GU2 7XH, United Kingdom; C. Charles and R. W. Boswell, The Australian National University, Canberra, ACT 0200 Australia; M. Perren, EADS Astrium, 6, rue Laurent Pichat, 75216 Paris Cedex 16, France

2011-105: TOTAL ELECTRON EMISSION YIELD OF ELECTRIC PROPULSION MATERIALS; Thomas Tondu and Mohamed Belhaj, Onera – The French Aerospace Lab, Toulouse, F-31055, France; S. Zurbach, Snecma, Safran Group, Space Engines Division, forÃ©t de Vernon, 27200, Vernon, France

2011-106: SPUTTERING YIELD OF POTENTIAL CERAMICS FOR THE HALL EFFECT THRUSTER DISCHARGE CHANNEL; Thomas Tondu and Jean-Pierre Chardon, Onera – The French Aerospace Lab, Toulouse, F-31055, France; S. Zurback, Snecma, Safran Group, Space Engines Division, forÃ©t de Vernon, 27200, Vernon, France

2011-107: ACTIVE CHARGING COMPENSATOR BASED ON THE FEEP NEUTRALIZER: REVIEW OF THE INSTRUMENT DEVELOPMENT ACTIVITIES AT TAS-I; G. Matticari, M. Materassi, G. Noci, and M. Capacci, Thales Alenia Space Italia, Site of Campi Bisenzio (Florence), 50013, Italy; E. Gengembre, ESA/ESTEC Noordwiik

2011-108: 100-HR ENDURANCE TEST ON A TUNGSTEN MULTI-ROD HOLLOW CATHODE FOR MPD THRUSTERS; M. De Tata and R. Albertoni, University of Pisa, Pisa, 56100, Italy; P. Rossetti, F. Paganucci, and M. Andrenucci, Alta S.p.A., Pisa, 56100, Italy; M. Cherkasova, V. Obukhov, and V. Riaby, RIAME-MAI, Moscow, Russia

2011-109: ALTERNATIVE MANUFACTURE TECHNOLOGIES FOR THE MANUFACTURE OF HET LARGER CERAMIC CHAMBER; J. Ibarzo, I. Caro, and J. Marcos, TECNALIA, San SebastiÃ¡n, 20009, Spain; J. Gonzalez Del Amo, ESA/ESTEC, Keplerlaan, 1, Noordwijk, The Netherlands

2011-110: EXPERIMENTAL STUDY OF A 100-KW CLASS APPLIED-FIELD MPD THRUSTER; R. Albertoni, P. Rossetti, F. Paganucci, M. Andrenucci, Alta SpA, Via A. Gherardesca 5, 56121, Ospedaletto, Pisa, Italy; M. Zuin, E. Martinez, and R. Cavazzana, Consorizio RFX, Corso Stati Uniti 4, 53127, Padova, Italy

2011-111: COMPACT HALL EFFECT ASSEMBLY PROPULSION SUBSYSTEM PPSX00, FIRST TEST RESULTS IN THE RANGE 300W-500W; F. Marchandise and N. Cornu, Snecma Division Moteurs Spatiaux, Vernon, Haute-Normandie, 27200, France; N. Arcis and D. Arrat, Centre National d’Etudes Spatiales, Toulouse, Midi-PyrÃ©rÃ©es, 31000, France

2011-112: EFFECTS OF DETAILED CHARGE EXCHANGE INTERACTIONS IN DSMC-PIC SIMULATION OF A SIMPLIFIED PLASMA TEST CELL; Paul N. Giuliano and Iain D. Boyd, Nonequilibrium Gas and Plasma Dynamics Laboratory, University of Michigan, Ann Arbor, MI, 48109, USA

2011-114: A HIGH CURRENT CATHODE PLASMA JET FLOW MODEL FOR THE PULSED PLASMA THRUSTER; Shaw P. V. and Lappas V. J., University of Surrey, Guildford, Surrey, GU2 7XH, UK

2011-115: DESIGN DEVELOPMENT AND EVALUATION OF A 8 ÂµPPT PROPULSION MODULE FOR A 3U CUBESAT APPLICATION; Shaw P. V., Lappas V. J., and Underwood C. I., University of Surrey, Guildford, Surrey, GU2 7XH, UK

2011-116: THREE-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF A PULSED PLASMA THRUSTER: MODELING AND CHALLENGES; J. Neudorfer, Institut fÃ¼r Aerodynamik und Gasdynamik, UniversitÃ¤t Stuttgart, 70550 Stuttgart, Germany, German Research School for Simulation Sciences GmbH, 52062 Aachen, Germany; T. Stindl, Institut fÃ¼r Raumfahrtsysteme, UniversitÃ¤t Stuttgart,n70550 Stuttgart, Germany; R. Schneider, Karlsruher Institut fÃ¼r Technologie, Institute fÃ¼r Hochleistungsimpuls – und Mikrowellentechnik, 76021 Karlsruhe, Germany; S. Roller, German Research School for Simulation Science GmbH, 52062 Aachen, Germany; C.-D. Munz, Institut fÃ¼r Aerodynamik und Gasdynamik, UniversitÃ¤t Stuttgart, 70550 Stuttgart, Germany; M. Auweter-Kurtz, German Aerospace Academy ASA, 71304 BÃ¶blingen, Germany

2011-117: INVESTIGATIONS OF LOW POWER HALL THRUSTER SPT-20M ON INCREASED VOLTAGE MODE; Andriy V. Loyan, Taras A. Maksymenko, Nikolay N. Koshelev, and Oleg P. Rybalov, National Aerospace University, Kharkiv, 61070, Ukraine

2011-118: XPS PLASMA PROPULSION SYSTEM ON ALPHABUS; Michel Lyszyk, Pierre-Philippe Baubias, Anthony Naulin, Ronan Pin, and Laurent Lecardonnel, Thales Alenia Space, France, Cannes, 100 Boulevard du Midi, 06156 Cannes La Bocca Cedex

2011-119: PPS1350-G PERFORMANCE ASSESSMENT WITH PERMANENT MAGNETS; V. Vial, L. Godard, and N. Cornu, Snecma, Safran Group, Space Engines Division, 27200 Vernon, France; E. Coulaud and D. Arrat, Centre National d’Etudes Spatiales, 31000 Toulouse, France

2011-120: PPS NG: HALL EFFECT THRUSTER FOR NEXT GENERATION SPACECRAFT; V. Vial and N. Cornu, Snecma, Safran Group, Space Engines Division, 27200 Vernon, France; E. Coulaud and D. Arrat, Centre National d’Etudes Spatiales, 31000 Toulouse, France

2011-122: WELL-CHARACTERIZED PLASMA EXPERIMENTS FOR VALIDATION OF COMPUTATIONAL MODELS; Richard E. Wirz, Lauren Chu, Marlene Patino, Hann-Shin Mao, and Samuel Araki, University of California, Los Angeles, CA 90095

2011-123: ION VELOCITY EVOLUTION WITH CHANNEL WIDTH, MAGNETIC TOPOLOGY AND PROPELLANT IN A 200 W HALL THRUSTER; G. Bourgeois, A. Lejeune, and S. Mazouffre, ICARE-CNRS, OrlÃ©ans, France

2011-124: ANALYSIS OF SOME REASON OF ANOMALOUS ELECTRON TRANSPORATION IN THE HALL THRUSTER; Sergey A. Oghienko, Anatoliy I. Oranskiy, Volodimir D. Olendarev, and Sergey V. Veryutin, Zhukovsky National Aerospace University “Kharkiv Aviation Institute”, Kharkiv, 61070, Ukraine

2011-125: TWIN ENGINE TESTS OF THE T6 ION ENGINE FOR ESA’S BEPICOLOMBO MERCURY MISSION; Ismat M. Ahmed Rudwan, Mars-space Ltd, Southampton, Hampshire, SO16 3QD, UK; Neil Wallace and Steve Clark, Space Division, QinetiQ Plc Ltd, Farnborough, Hampshire, GU14 0LX, UK

2011-126: LOW-THRUST MISSIONS FOR EXPANDING FOAM SPACE DEBRIS REMOVAL; P. Pergola, A. Ruggiero, and M. Andrenucci, University of Pisa, Pisa, 56100, Italy; L. Summerer, ESA Advanced Concepts Team, 2201 Noordwijk, The Netherlands

2011-127: INVESTIGATION OF ION-ION PLASMAS FOR APPLICATION IN ELECTRIC THRUSTERS; Dennis Gerst, Mihaela Cirisan, and StÃ©phane Mazouffre, ICARE-CNRS, 45071 OrlÃ©ans, France; Ane Aanesland, LPP Ecole Polytechnique, 91128 Palaiseau, France

2011-129: TELEMICROSCOPY AND THERMOGRAPHY DIAGNOSTIC SYSTEMS FOR MONITORING HALL EFFECT THRUSTERS; Tommaso Misuri, Tina Vrebosch, Luca Pieri, and Mariano Andrenucci, ALTA S.p.A., Ospedaletto, Pisa, 56121, Italy, University of Pisa; Massimiliano Tordi, Enrico Marcuzzi, and Massimo Bartolozzi, AIEM S.r.l., Borsea, Rovigo, 45030, Italy; Simone Renzetti, OptronItalia S.r.l., Grosseto, 58100, Italy; JosÃ© Gonzalez Del Amo, ESA/ESTEC, Keplerlaan 1, Noordwijk, The Netherlands

2011-131: MICROFABRICATION OF CAPILLARY ELECTROSPRAY EMITTERS AND TOF CHARACTERIZATION OF THE EMITTED BEAM; S. Dandavino, C. Ataman, and H. Shea, Ecole Polytechnique FÃ©dÃ©rale de Lausanne (EPFL), Neuchatel, 2000, Switzerland; C. Ryan and J. Stark, Queen Mary University of London, London, E1 4NS, United Kingdom

2011-132: HIGH PRECISION BEAM DIAGNOSTICS FOR ION THRUSTERS; Benjamin van Reijen, Norbert Koch, Alexey Lazurenko, Stefan Weis, Martin Schirra, Angelo Genovese, and Jens Haderspeck, Thales Electron Devices GmbH, SÃ¶flingerstr. 100, 89075 Ulm, Germany; Eberhard Gill, Delft University of Technology, Kluyverweb 1, 2629HS Delft, The Netherlands

2011-134: OVERVIEW ON ELECTRIC PROPULSION DEVELOPMENTS AT IRS; Georg Herdrich, Uwe Bauder, Adam Boxberger, Christoph Eichhorn, Matthias Lau, Marcel Pfeiffer, Torsten Stindl, Constanze Syring, Birk Wollenhaupt, Hans-Peter RÃ¶ser, and Stefanos Fasoulas, Institute of Space Systems (IRS), University of Stuttgart, 70569 Stuttgart, Germany; Dejan Petkow, ESA-ESTEC, Advanced Concepts Team, Noordwijk, The Netherlands; Tony SchÃ¶nherr and Kimiya Komurasaki, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan

2011-135: PRELIMINARY PERFORMANCE RESULTS OF A 5-CM KAUFMAN-TYPE ION THRUSTER; Gilberto M. Sandonato, JosÃ© AmÃ©rico N. Goncalves, and Ricardo T. Irita, National Institute for Space Research-INPE, Sao JosÃ© dos Campos, SP, 12227-010, Brazil; Paolo Gessini, University of Brasilia at Gama – UnB Gama, Gama, DF, 72405-610, Brazil

2011-136: AZIMUTHAL SYMMETRY BREAKING, CURRENT FILAMENTATION AND ONSET REGIME IN MPD THRUSTERS; Sebastiano Giannelli, University of Pisa, Pisa, Italy; Mariano Andrenucci, University of Pisa, Pisa, Italy, Alta S.p.A., Pisa, Italy

2011-137: FUNDAMENTAL PROPERTIES OF MAGNETIZED PLASMA FLOWS; T. Andreussi, Alta S.p.A., Pisa, 56121, Italy; S. Giannelli, University of Pisa, Pisa, 56122, Italy; F. Pegoraro, University of Pisa, Pisa, 56127, Italy; M. Andrenucci, University of Pisa, Pisa, 56122, Italy, Alta S.p.A., Pisa, 56121, Italy

2011-138: FEASIBLITY OF A DOWN-SCALED HEMP-THRUSTER; Andreas Keller, University of Giessen, I. Physikalisches Institut, 35392 Giessen, Germany, Astrium GmbH – Satellites, 88039 Friedrichshafen, Germany; Peter KÃ¶hler, Waldemar GÃ¤rtner, Benjamin Lotz and Davar Feili, University of Giessen, I. Physikalisches Institut, 35392 Giessen, Germany; Philipp Dold and Marcel Berger, Astrium GmbH – Satellites, 88039 Friedrichshafen, Germany; Claus Braxmaier, HTWG Konstanz, Institute for Optical Systems, 78462 Konstanz, Germany; Dennis Weise and Ulrich Johann, Astrium GmbH – Satellites, 88039 Friedrichshafen, Germany

2011-140: A THERMAL PULSED PLASMA TRUSTER FOR MICROSATELLITE PROPULSION; Matthias Lau, Georg Herdrich, Stefanos Fasoulas, and Hans-Peter RÃ¶ser, Institute of Space Systems, University of Stuttgart, Stuttgart, 70569, Germany

2011-141: ENDURANCE TESTING OF HEMPT-BASED ION PROPULSION MODULES FOR SMALL GEO; A. Genovese, A. Lazurenko, N. Koch, S. Weis, M. Schirra, B. van Reijen, J. Haderspeck, and P. Holtmann, Thales Electron Devices GmbH, SÃ¶flinger Str. 100, Ulm 89077, Germany

2011-142: STUDY OF A HALL EFFECT THRUSTER WORKING WITH AMBIENT ATMOSPHERIC GAS AS PROPELLANT FOR LOW EARTH ORBIT MISSIONS; L. Garrigues, LAPLACE (Laboratoire Plasma et Conversion d’Energie), UniversitÃ© de Toulouse, UPS, INPT Toulouse, 118, route de Narbonne, F-31062 Toulouse, France

2011-143: CHARACTERIZATION OF AN ADJUSTABLE MAGNETIC FIELD, LOW-POWER HALL EFFECT THRUSTER; S. Oslyak and C. Ducci, Research Engineer, Alta S.p.A., Pisa, 56014 Italy; P. Rossetti, Project Manager, Alta S.p.A., Pisa, 56014, Italy; M. Andrenucci, Professor, Aerospace Engineering Dep. University of Pisa, CEO, Alta S.p.A., Pisa, 56014, Italy

2011-144: DEVELOPMENT OF A MICROTHRUSTER MODULE FOR NANOSATELLITE APPLICATIONS; A. Mingo PÃ©rez, University of Southampton, Southampton, SO171BJ, United Kingdom; M. Coletti, Mars Space Ltd, Southampton, SO16 3QD, United Kingdom; S. B. Gabriel, University of Southampton, Southampton, SO171BJ, United Kingdom

2011-145: TWO-DIMENSIONAL ANALYSIS OF CONICAL PULSED INDUCTIVE PLASMA THRUSTER PERFORMANCE; A. K. Hallock, Princeton University, Princeton, NJ, 08544; K. A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL 35812; G. D. Emsellem, The Elwing Company, Wilmington, DE, 19801

2011-146: OVERVIEW ON TESTING INFRASTRUCTURES AND DIAGNOSTIC TOOLS FOR HEMPT BASED ION PROPULSION SYSTEMS; A. Lazurenko, B. van Reijen, N. Koch, S. Weis, a. Genovese, J. Haderspeck, and M. Schirra, Thales Electron Devices GmbH, SÃ¶flinger Str. 100, Ulm 89077, Germany; S. Scaranzin, E. Bonelli, and F. Scortecci, AEROSPAZIO Tecnologie S.r.l., Raplolano Terme, Siena, 53040, Italy

2011-147: PERFORMANCE CHARACTERISTICS OF A MAGNESIUM HALL-EFFECT THRUSTER; Mark A. Hopkins and Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2011-148: DEVELOPMENT, QUALIFICATION AND DELIVERY STATUS OF TH HEMPT BASED ION PROPULSION SYSTEM FOR SMALLGEO; Norbert Koch, Stefan Weis, Martin Schirra, Alexey Lazurenko, Benjamin van Reigen, Jens Haderspeck, Angelo Genovese, and Peter Holtmann, Thales Electron Devices GmbH, SÃ¶flingerstr. 100, 89073 Ulm, Germany; Klaus Ruf and Norbert PÃ¼ttmann, German Space Agency DLR, Space Administration City, KÃ¶nigswinterer Str. 522-524, 53227 Bonn, Germany; Hendrik LÃ¼bberstedt, OHB Systems AG, UniversitÃ¤tsalle 27-29, 28349 Bremen, Germany

2011-149: EROSION MEASUREMENTS IN A DIVERGING CUSPED-FIELD THRUSTER; Stephen R. Gildea, Taylor S. Matlock, and Manuel MartÃnez-SÃ¡nchez, Massachusetts Institute of Technology, Cambridge, MA, 02139, USA; William A. Hargus, Jr., Air Force Research Laboratory, Edwards Air Force Base, CA 93524, USA

2011-150: IMPD SYSTEM STUDY AND HIGH VOLTAGE POWER SUPPLY SUBSYSTEM DEVELOPMENT AT IRS; Matthias Lau, Georg Herdrich, Stefanos Fasoulas, and Hans-Peter RÃ¶ser, Institute of Space Systems, University of Stuttgart, Stuttgart, 70569, Germany; Michael Koch and Thomas Hintze, ASP Equipment GmgH, Salem Neufrach, Baden-WÃ¼rttemberg, 88682, Germany

2011-151: HOLLOW CATHODE THRUSTER DESIGN AND DEVELOPMENT FOR SMALL SATELLITES; D. Lamprou, V. J. Lappas, and T. Schimizu, University of Surrey, Guildford, GU2 7XH, United Kingdom; D. Gibbon, Surrey Satellite Technology Ltd. Tycho House, 20 Stephenson Road, GU2 7YE, United Kingdom; M. Perren, EADS Astrium, 6 rue Laurent Pichat, 75216 Paris Cedex 16, France

2011-152: TWO-TEMPERATURE THERMODYNAMIC AND TRANSPORT PROPERTIES OF HYDROGEN PLASMAS; Shi-Qiang Chen and Hai-Xing Wang, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China; E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Prinecton, New Jersey, 08540, US

2011-153: NUMERICAL SIMULATION OF LOW AND MEDIUM POWER ARCJET THRUSTERS; Fu-Zhi Wei and Hai-Xing Wang, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China; E. Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, New Jersey, 08540, US

2011-154: VASIMR VX-200 OPERATION AT 200 KW AND PLUME MEASUREMENT: FUTURE PLANS AND AN ISS EP TEST PLATFORM; Jared P. Squire, Chris S. Olsen, Franklin R. Chang DÃaz, Leonard D. Cassady, Benjamin W. Longmeir, Maxwell G. Ballenger, Mark D. Carter, Tim W. Glover, and Greg E. McCaskill, Ad Astra Rocket Company, Webster, Texas, 77598, USA; Edgar A. Bering III, University of Houston, Houston, Texas, 77204, USA

2011-155: THE VX-CR EXPERIMENT: A THERMAL AND LIFETIME TESTBED FOR THE VASIMR ENGINE; Jaun I. Del Valle Gamboa, Sergio CortÃ©s Godoy, Luis Diego Fonseca Flores, Jorge Oguilve-Araya, Juan J. Valverde QuirÃ³s, Carlos MartÃnez Castillo, David Ixcamparij Rojas, Ronald Chang-DÃaz, Ad Astra Rockety Company, Liberia, Guanacaste, Costa Rica; Benjamin W. Longmier, Tim W. Glover, Jared P. Squire, Franklin R. Chang-DÃaz, Ad Astra Rocket Company, Webster, Texas, USA

2011-156: VASIMR VX-200 PERFORMANCE MEASUREMENTS AND HELICON THROTTLE TABLES USING ARGON AND KRYPTON; Benjamin W. Longmier, Jared P. Squire, Leonard D. Cassady, Maxwell G. Ballenger, Mark D. Carter, Chris Olsen, Andrew V. Ilin, Tim W. Glover, Greg E. McCaskill, Franklin R. and Chang DÃaz, Ad Astra Rocket Company, Webster, TX 77598, USA; Edgar A. Bering, III, University of Houston, Departments of Physics and ECE, Houston, TX 77204, USA; Juan Del Valle, Ad Astra Rocket Company, Liberia, Guanacaste, Costa Rica

2011-160: EFFECT OF AN ADDITIONAL, PARALLEL CAPACITOR ON PULSED INDUCTIVE PLASMA ACCELERATOR PERFORMANCE; Kurt A. Polzin, Amy D. Sivak, and Joseph V. Balla, NASA-Marshall Space Flight Center, Huntsville, AL 35812

2011-161: OVERVIEW OF NASA’S ELECTRIC PROPULSION DEVELOPMENT ACTIVITIES FOR ROBOTIC SCIENCE MISSIONS; Eric J. Pencil, Todd T. Peterson, and David J. Anderson, NASA Glenn Research Center, Cleveland, Ohio 44135, USA; John Dankanich, Gray Research, Cleveland, Ohio 44135, USA

2011-162: THE DESIGN AND DEVELOPMENT OF A 30-GHZ MICROWAVE ELECTROTHERMAL THRUSTER; Erica E. Capalungan, Michael M. Micci, and Sven G. BilÃ©n, The Pennsylvania State University, University Park, Pennsylvania 16802, USA

2011-164: DESIGN OF THE MINIATURE MICROWAVE-FREQUENCY ION THRUSTER; Daniel P. Lubey, Sven G. BilÃ©n, Michael M. Micci, and Pierre-Yves Taunay, The Pennsylvania State University, University Park, PA 16802, USA

2011-166: DIVERGENCE ANGLE OF IONS BEAMS EMANATING FROM AN IMMERSED RADIOFREQUENCY PLASMA SOURCE; Adam Shabshelowitz and Alec D. Gallimore, University of Michigan, Ann Arbor, Michigan, 48105, USA

2011-167: ELECTRIC PROPULSION THRUSTER ASSEMBLY FOR SMALL GEO-STATUS UPDATE; Olivier Duchemin, Vaitua Leroi, and Michael Oberg, Snecma, Safran Group, Space Engines Division, 27208 Vernon, France; Eric Bourguignon, Murielle Pardonge and Thierry Scalais, Thales Alenia Space ETCA, 6032 Mont-sur-Marchienne, Belgium; Alain Demaire and Staffan Persson, OHB-Sweden AB, SE-17122 SÃ¶lna, Sweden; Hendrik LÃ¼bberstedt, OHB-System AG, 28359 Bremen, Germany

2011-168: HIGH-SPEED DUAL LANGMUIR PROBE MEASUREMENTS OF THE PLASMA PROPERTIES AND EEDFS IN A HET PLUME; Robert B. Lobbia, Michael J. Sekerak, Raymond Liang, and Alec D. Gallimore, The University of Michigan, Ann Arbor, MI, 48109, USA

2011-169: OPTICAL DIAGNOSTICS OF A LOW TEMPERATURE ARGON THRUSER; K. Katsonis and Ch. Berenguer, Data Evaluation & Diagnostics Algorithms of Systems (DEDALOS EPE), Thessaloniki, Hellas; D. Pavarin, A. Lucca Fabris, F. Trezzolani, and M. Faenza, Center of Studies and Activities for Space (CISAS) “G. Colombo”, University of Padua, Padua, Italy; P. Tsekeris and S. Cohen, Physics Department, University of Ioannina, GR-45110 Ioannina, Greece; M. Cornille, LUTH, CNRS Observatoire de Paris, 92190 Meudon, France & Data Evaluation & Diagnostics Algorithms of Systems (DEDALOS EPE), Thesaloniki, Hellas

2011-170: THE RESONANT LINES VUV TRANSITIONS IN RARE GAS PLASMA THRUSTERS; Ch. Berenguer and K. Katsonis, Data Evaluation & Diagnostics Algorithms Of Systems (DEDALOS EPE), Thessaloniki, Hellas; D. Pavarin, Center of Studies and Activities for Space (CISAS) “G. Colombo”, University of Padua, Padua, Italy

2011-171: PROPULSION FOR NANOSATELLITES; C. Scharlemann and M. Tajmar, University of Applied Science Wiener Neustadt, Austria; I. Vasiljevich, N. Buldrini, D. Krejci, and B. Seifert, Fotec Forschungs-und Technologietransfer GmbH, Wr. Neustadt, Austria

2011-173: DIRECT MEASUREMENT OF SPOKE-INDUCED, CROSS-FIELD ELECTRON TRANSPORT IN A CYLINDRICAL HALL THRUSTER; C. Leland Ellison and Yevgeny Raitses and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton, NJ, 08543, USA

2011-174: THE USE OF ELECTRIC PROBE TECHNIQUES FOR ELECTRIC POTENTIAL MEASUREMENTS IN PLASMA THRUSTERS; J. P. Sheehan, Yevgeny Raitses, Noah Hershkowitz, Igor D. Kaganovich, and Nathaniel J. Fisch

2011-175: EFFECT OF MAGNETIC SHIELDING ON PLASMA PLUME OF THE CYLINDRICAL HALL THRUSTERS; Yevgeny Raitses, Jean Carlos Gayoso, and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 0854, USA

2011-176: MATHEMATICAL MODEL OF ACCELERATION STAGE OF MAGNETIC INDUCTIVE PULSED PLASMA THRUSTER; Hatef Dinparasti Saleh and Sergiy Yuriyovich Nesterenko, National Aerospace University (Kharkiv Aviation Institute), Kharkiv, 61070, Ukraine, Chkalova, 17

2011-178: CONTROLLING PLUME DIVERGENCE IN A CUSPED-FIELD THRUSTER; Taylor S. Matlock, Fuzhou Hu, and Manuel Martinez-Sanchez, Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA

2011-179: THE DEVELOPMENT OF 260W POWER PROCESSING UNITS FOR HALL EFFECT PROPULSION SYSTEM; Khalid Ibrahim Anochi, Assistance Research Engineer, Emirates Institute of Advance Science and Technology, Dubai, UAE; Mr. Choo and Won-Gyo, Electrical Power Team Principal Research Engineer, Satrec Initiative, Deajeon South Korea; Mr. Jeong and Yun-hwang, Manager, Satrec Initiative, Deajeon South Korea

2011-180: TWO-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF MAGNETIC SAILS; Yasumasa Ashida, Kyoto Univerity, Kyoto, 611-0011, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Kanagawa, 252-5210, Japan; Hiroshi Yamakawa, Kyoto University, Kyoto, 611-0011, Japan; Yoshihiro Kajimura, Japan Aerospace Exploration Agency, Kanagawa, 252-5210, Japan

2011-181: INCORPORATION OF AN ENERGY EQUATION INTO A PULSED INDUCTIVE THRUSTER PERFORMANCE MODEL; Kurt A. Polzin, NASA-Marshall Space Flight Center, Huntsville, AL 35812, USA; Jarred P. Reneau, Mississippi State University, Starkville, MS 39762, USA; Kameshwaran Sankaran, Whitworth University, Spokane, WA 99251, USA

2011-182: A NEW MAGNETIC FLUX DENSITY CONTROL METHOD TO IMPROVE POWER COMSUMPTION OF HALL THRUSTER; Mitsubishi Electric Corporation, Kamakura Works, Kamakura, Kanagawa, 247-8520, Japan; Fujio Kurokawa, Nagasaki University, Nagasaki, Nagasaki, 852-8521, Japan; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan; Taichiro Tamida, Mitsubishi Electric Corporation, Advanced Technology R&D Center, Amagasaki, Hyogo, 661-8661, Japan

2011-183: DEVELOPMENT STATUS OF HIGH VOLTAGE POWER SUPPLY FOR A 20MN CLASS ION THRUSTER; Hiroshi Nagano and Kenichi Kajiwara, Japan Aerospace Exploration Agency, Aerospace Research and Development Directorate, 2-1-1 Sengen, Tukuba, Ibaraki, 305-8505, Japan; Hiroyuki Osuga, Isao Terukina, Hirokazu Suzuki, and Kazuo Shuto, Mitsubishi Electric Corporation, Kamakura Works, Space System Department, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan

2011-186: EXPERIMENTAL INVESTIGATION OF MAGNETOPLASMA SAIL: MAGNETOSPHERE INFLATION BY EQUATORIAL RING CURRENT; Yuya Oshio, Graduate University for Advanced Studies, Sagamihara, Kanagawa, 252-5210, Japan, Kazuma Ueno and Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2011-189: ENHANCEMENT LAB6’S EMISSION PROPERTIES AFTER THE OXYGEN ION BOMBARDMENT; Anatoly Taran and Andriy Okhrimovskyy, National Aerospace University “Kharkiv Aviation Institute”, Kharkiv, 61079, Ukraine; Alexsadr Kovalev, Institute for Problems of Material Science of NASU, Kiev, 03680, Ukraine

2011-191: HT-100 HALL THRUSTER CHARACTERIZATION TESTS RESULTS; D. Dignani, C. Ducci, G. Cifali, P. Rossetti, and M. Andrenucci, Alta SpA, Pisa, 56121, Italy

2011-192: EXPERIMENTAL INVESTIGATION OF A LAYERED GRAPHITE/BN CHANNEL FOR HALL THRUSTERS; Serge Barral, Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland; StÃ©phan Zurbach, Snecma, Safran Group, 27208 Vernon, France; Michel Dudeck, UniversitÃ© Pierre et Marie Curie – Paris 6, 75252 Paris Cedex, France

2011-193: ACTIVE CONTROL OF A HALL THRUSTER DISCHARGE; Serge Barral, Jacek Kaczmarczyk, and Jacek Kurzyna, Institute of Plasma Physics and Laser Microgusion, 01-497 Warsaw, Poland; Michel Dudeck, UniversitÃ© Pierre et Marie Curie – Paris 6, 75252 Paris Cedex, France

2011-194: HIGH POWER PLASMA FLOW INTERACTION WITH MICRO- AND NANOPOWDERS; Michael N. Kazeev, Vladimir F. Kozlov, and Yuri S. Tolstov, National Research Centre Kurchatov Institute, pl. Kurchatova, 1, Moscow, 123182, Russia

2011-196: IONIZATION-INDUCED AZIMUTHAL OSCILLATION IN HALL EFFECT THRUSTERS; Diego Escobar and Eduardo Ahedo, Universidad PolitÃ©cnica de Madrid (UPM), Madrid, 28040, Spain

2011-197: RESULTS OF TESTS OF HIGH-CURRENT CATHODE FOR HIGH-POWER HALL THRUSTER; A. Loyan, N. Koshelev, and O. Ribalov, National Aerospace University, “KhAI”, 61070 Kharkiv, Ukraine; M. Dudeck, UPMC, France; S. Zurbach, Snecma, Safran Group, Space Propulsion Division, 27208 Vernon, France

2011-198: ELECTROSTATIC PROBE MEASUREMENTS IN A 4 J PULSED PLASMA THRUSTER; Zun Zhang, Haibin Tang, Yuan Yang, and Mingxin Li, Beijing University of Aeronautics and Astronautics, Beijing, Zip 100191, China

2011-199: THE COMPARISON OF RESULTS OF TESTS OF LOW-POWER HALL THRUSTERS: SPT AND TAL; Titov M., Loyan A., Rybalov O., and Maksymenko T., National Aerospace University “KhAI”, 61070 Kharkiv, Ukraine

2011-200: MEASUREMENT OF PLASMA PROPERTY IN AN ION THRUSTER USING LASER THOMSON SCATTERING TECHNIQUE, Naoji Yamamoto, Kensaku Sugita, Tomoaki Kurita, Kentaro Tomita, Kiichiro Uchino, and Hideki Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan

2011-201: NEXT GENERATION OF THRUSTER MODULE ASSEMBLY (TMA-NG); Anthony Lorand, Olivier Duchemin, and Nicolas Cornu, Snecma Division Moteurs Spatiaux, Vernon, 27200, France

2011-203: SGEO DEVELOPMENT STATUS AND OPPORTUNITIES FOR THE EP-BASED SMALL EUROPEAN TELECOMMUNICATION PLATFORM; Marco De Tata, Pierre-Etienne Frigot, Stefan Beekmans, Hendrik LÃ¼bberstedt, and Dieter Birreck, OHB System AG, Bremen, 28359, Germany; Alain DemairÃ© and Peter Rathsman, OHB Sweden AB, Solna, SE-171 04 Sweden

2011-204: NUMERICAL INVESTIGATION OF A DUAL STAGE VARIABLE ISP ION ENGINE; M. Coletti and Stephen B. Gabriel, Astronautics Research Group, University of Southampton, Southampton SO17 1DR, UK

2011-205: EFFECTS OF ELECTRON MODEL ON THREE-GRID ION ENGINE ANALYSES; Takeshi Miyasaka, Katsuo Asato, Fakhuradzi B. Baharudin, and Hitoshi Sugiyama, Gifu University, Gifu, 501-1193, Japan; Ikkoh Funaki, JAXA, Sagamihara, Kanagawa, 229-8510, Japan

2011-208: HALL THRUSTER SMALL SCALE PLASMA FLUCTUATIONS: QUALIFYIG 2D PIC SIMULATIONS AGAINST COLLECTIVE SCATTERING EXPERIMENTAL DATA; Cyrille HonorÃ©, Sedina Tsikata, and Dominique GrÃ©sillon, Laboratoire de Physique des Plasmas CNRS-UPMC, Ecole Polytechnique, Palaiseau France; Anne HÃ©ron, Centre de Physique ThÃ©orique, Ecole Polytechnique, Palaiseau, France; Jordan Cavalier and N. Lemoine, Institut Jean Lamour, UniversitÃ© Henri PoincarÃ©, Nancy, France

2011-209: THE EUROPEAN HIPER PROGRAMME: HIGH POWER ELECTRIC PROPULSION TECHNOLOGY FOR SPACE EXPLORATION; C. Casaregola, G. Cesaretti, and M. Andrenucci, Alta S.p.A., Pisa, 56127, Italy

2011-210: THE ROLE OF ELECTRIC PROPULSION IN A FLEXIBLE ARCHITECTURE FOR SPACE EXPLORATION; C. Casaregola, D. Dignani, P. Pergola, A. Ruggiero, and M. Andrenucci, Alta S.p.A., Pisa, 56121, Italy

2011-211: 30 KW-CLASS HALL THRUSTER: A KEY BUILDING BLOCK FOR PROPULSION NEEDS OF FUTURE SPACE TRANSPORATION AND EXPLORATION; P. Rossetti, C. Casaregola, and M. Andrenucci, Alta S.p.A., Pisa, 56121, Italy

2011-212: SIMULATIONS OF DIRECT ION ACCELERATION WITH BEATING ELECTROSTATIC WAVES; Bayard G. Gardineer, IV, Benjamin Jorns, and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ, 08540, USA

2011-213: A CARBON NANOTUBE FIELD EMISSION CATHODE FOR ELECTRODYNAMIC TETHER SYSTEMS; Yasushi Ohkawa, Shoji Kitamura, Satomi Kawamoto, Koji Matsumoto, and Seishiro Kibe, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; Takuya Matsumoto, Fumihiko Murata, Makoto Matsui, and Yoshiki Yamagiwa, Shizuoka University, Hamamatsu, Shizuoka, 432-8561, Japan

2011-216: MIXED METAL BASED HOLLOW CATHODE NEUTRALIZER TECHNOLOGY FOR HEMP BASED ION PROPULSION SYSTEMS; M. Schirra, N. Koch, S. Weis, A. Lazurenko, B. van Reijen, A. Genovese, J. Haderspeck, and P. Holtmann, Thales Electron Devices GmbH, SÃ¶fling StraÃŸe 100, 89077 Ulm

2011-217: RECIRCULATING LIQUID NITROGEN SYSTEM FOR OPERATION OF CRYOGENIC PUMPS; Alexander W. Kieckhafer and Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA 30332, USA

2011-219: TIME-RESOLVED MEASUREMENTS OF PLASMA PROPERTIES IN THE FAR-FIELD PLUME OF A LOW-POWER HALL EFFECT THRUSTER; K. Dnnenmayer and S. Mazouffre, Institut de Combustion, AÃ©rothermique, RÃ©activitÃ© et Environnement, CNRS, 1C avenue de la Recherche Scientifique, 45071 OrlÃ©ans, France; P. Kudrna and M. Tichy, Charels University, Faculty of Mathematics and Physics, Prague, Czech Republic

2011-220: SINGLE STAGE FARADAY ACCELERATOR WITH RADIO-FREQUENCY ASSISTED DISCHARGE (SS-FARAD); Matthew S. Feldman and Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08544, USA

2011-221: IPPLM HALL EFFECT THRUSTER – DESIGN GUIDELINES AND PRELIMINARY TESTS; Jacek Kurzyna and Dariusz Danitko, Institute of Plasma Physics and Laser Microfusion, Hery 23, 010-497 Warsaw, Poland

2011-222: SCALING OF ANODE SHEATH VOLTAGE FALL WITH THE OPERATIONAL PARAMETERS IN APPLIED-FIELD MPD THRUSTERS; Dan Lev and Edgar Y. Choueiri, Electric Propulsion and Plasma Dynamics Laboratory (EPPDYL), Princeton University, Princeton, NJ, 08544, USA

2011-223: ARCHITECTURE, FUNCTIONAL FEATURES AND OPERATIONAL CHARACTERISTICS OF THE HEMPT BASED ION PROPULSION SYSTEM FOR SMALLGEO; Stefan Weis, Norbert Koch, Martin Schirra, Alexey Lazurenko, Benjamin van Reien, Jens Haderspeck, Angelo Genovese, and Peter Holtmann, Thales Electron Devices GmbH, Soeflinger Str.,100, 89077 Ulm; Klaus Ruf and Norbert PÃ¼ttmann, Deutsches Zentrum fÃ¼r Luft- und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Koenigswinterer Strasse 522-524, 53227 Bonn, Germany; Hendrik Luebbersted, OHB System AG, Bremen, 28359, Germany

2011-224: EXPERIMENTAL CHARACTERIZATION OF HET AND RIT WITH ATMOSPHERIC PROPELLANTS; G. Cifali, T. Misuri, P. Rossetti, and M. Andrenucci, Alta SpA, Pisa, 56121, Italy; D. Valentian, Consultant for Snecma, Vernon, 27208, France; D. Feili and Benjamin Lotz, Giessen University, Giessen, D-35390, Germany

2011-225: OBSERVATION OF ION BEAM PROPERTIES IN THE HALL THRUSTER PLASMA USING AN AXIAL ELECTRON DENSITY FLUCTUATION MODE; Sedina Tsikata, Cyrille HonorÃ©, and Dominique GrÃ©sillon, Ecole Polytechnique, UMR 7648 CNRS, Palaiseau, France; Anne HÃ©ron, Ecole Polytechnique, UMR 7644 CNRS, Palaiseau, France; Nicolas Lemoine and Jordan Cavalier, UniversitÃ© Henri-PoincarÃ©, UMR 7198 CNRS, Nancy, France

2011-226: HARNESSING THE “ORBITAL BATTERY” FOR PROPULSION VIA ENERGY-HARVESTING ELECTRODYNAMIC TETHERS; Sven G. BilÃ©n and Jesse K. McTernan, The Pennsylvania State University, University Park, Pennsylvania 16802, USA; Brian E. Gilchrist and Iverson C. Bell, The University of Michigan, Ann Arbor, Michigan 48109, USA; Robert P. Hoyt and Nestor R. Voronka, Tethers Unlimited, Inc., Bothell, Washington 98011, USA

2011-227: ASSESSMENT OF DIFFERENTIAL CROSS-SECTIONS FOR HALL-THRUSTER PLUME SIMULATION; Tyler D. Huismann and Iain D. Boyd, University of Michigan, Ann Arbor, MI, 48109, USA

2011-228: NUMERICAL STUDY ON THE EFFECT OF ELECTRODE GEOMETRY IN MPD THRUSTERS; M. Mahendhran and Amit Kumar, Indian Institute of Technology Madras, Chennai-600 -036, India

2011-229: SIMILARITY PARAMETER EVOLUTION WITHIN A MAGNETIC NOZZLE WITH APPLICATIONS TO LABORATORY PLASMAS; Justin M. Little, Aaron S. Rubin, and Edgar Y. Choueiri, Princeton University, Princeton, New Jersey, 08540, USA

2011-231: RESEARCH TOWARD AN ELECTROSTATIC MICROPARTICLE THRUSTER BASED ON CONTACT CHARGING; Thomas Trottenberg, Viktor Schneider, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

2011-232: MEASUREMENT OF THE MOMENTUM FLUX IN AN ION BEAM; Alexander Spethmann, Thomas Trottenberg, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

2011-234: QUALIFICATION OF THE T6 ION THRUSTER FOR THE BEPICOLOMBO MISSION TO THE PLANET MERCURY; Dr. Angelo N. Grubisic, Flux Engineering Ltd., Farnborough, Hampshire, GU14 0LX, United Kingdom; Stephen Clark and Neil Wallace, QinetiQ Space Division, Farnborough, Hampshire, United Kingdom; Dr. C. Collingwood and Francesco Guarducci, University of Southampton/Mars Space, Southampton, Hampshire, SO17 1BJ, United Kingdom

2011-235: MODELING OF NANO-SCALE ELECTROKINETIC THRUSTERS; F. J. Diez, G. Hernaiz, and J. J. Miranda, Rutgers, The State University of New Jersey, Piscataway, NJ, 08854, USA; M. Sureda, ETSEIAT, Universitat PolitÃ©cnica Catalunya, Terrassa, Spain

2011-236: THE HEMPT CONCEPT – A SURVEY ON THEORETICAL CONSIDERATIONS AND EXPERIMENTAL EVIDENCES; N. Koch, M. Schirra, S. Weis, A. Lazurenko, B. van Reijen, J. Haderspeck, A. Genovese, and P. Holtmann, Thales Electron Devices GmbH, SÃ¶flinger StraÃŸe 100, 89077 Ulm; R. Schneider, K. Matyash, and O. Kalentyev, Ernst Mortiz Arndt UniversitÃ¤t Greifswald, Felix-Hausdorff-Stra ÃŸe 12, 17489 Greifswald

2011-238: STUDY OF PLASMA CONFINEMENT BY MAGNETIC FIELDS IN HALL THRUSTERS USING QUASI-NEUTRAL PIC MODELING; Jan Miedzik and Serge Barral, Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland, StÃ©phan Zurbach, Snecma, Safran Group, 27208 Vernon, France

2011-239: DESIGN AND TESTING OF A MICRO PULSED PLASMA THRUSTER FOR CUBESAT APPLICATION; F. Guarducci and M. Coletti, Mars Space Ltd, Southampton, S016 3QD, United Kingdom; S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, UK

2011-240: DEVELOPMENT OF PLASMA CODES FOR THE DESIGN OF MINI-HELICON THRUSTERS; D. Pavarin, F. Ferri, M. Manente, D. Curreli, D. Melazzi and D. Rondini, CISAS “G. Colombo”, Center of Studies and Activities for Space, University of Padova, 35151 Padova, Italy; A. Cardinali, ENEA, Frascati, Rome, Italy

2011-241: THRUSTER DEVELOPMENT SET-UP FOR THE HELICON PLASMA HYDRAZINE COMBINED MICRO RESEARCH PROJECT (HPH.COM); D. Pavarin, F. Ferri, M. Manente, A. Lucca Fabris, F. Trezzolani, M. Faenza, and L. Tasinato, Center of Studies and Activities for Space (CISAS) “G. Colombo”, University of Padova, Padova, Italy; O. Tudisco and R. Deangelis, Agenzia Nazionael per le Nuove Tecnologie l’Energia e lo Sviluppo Economico Sostenibile (ENEA), Frascati, Italy; A. Loyan, Y. Protsan and A. Tsaglov, National Aerospace University “Kharkiv Aviation Institute” (KhAI), Kharkiv, Ukraine; A. Selmo, Studio Progettazione e Realizzazione di Apparati Elettronici di Selmo Antonio (RESIA), Albaredo d’Adige, Italy; K. Katsonis and Ch. Berenguer, DEDALOS EPE, Thessaloniki, Greece; D. Packan, J. Jarrige, C. Blanchard, P. Q. Elias, and J. Bonnet, ONERA, Palaiseau, France

2011-242: PARAMETRIC INVESTIGATION OF THE ROTATING SPOKE INSTABILITY IN HALL THRUSTERS; Michael S. McDonald and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), University of Michigan, Ann Arbor, MI USA 48109

2011-243: ELECTRON TRAJECTORY SIMULATION IN EXPERIMENTAL HALL THRUSTER FIELDS; Michael S. McDonald and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), University of Michigan, Ann Arbor, MI USA

2011-244: NUMERICAL SIMULATIONS OF A 20-KW CLASS HALL THRUSTER USING THE MAGNETIC-FIELD-ALIGNED-MESH CODE HALL2DE; Ioannis G. Mikellides and Ira Katz, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109; Hani Kamhawi and Jonathan L. Vannoord, National Aeronautics and Space Administration Glenn Research Center, Cleveland, OH 44135, USA

2011-245: TIME-RESOLVED LANGMUIR PROBING OF A NEW LANTHANUM HEXABORIDE (LAB6) HOLLOW CATHODE; Kimberly R. Trent and Michael S. McDonald, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI, 48104, USA; Robert B. Lobbia, Air Force Research Laboratory, Edwards, CA, 93524, USA; Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, MI, 48104, USA

2011-246: DEVELOPMENT STATUS OF A 100-KW CLASS LABORATORY NESTED CHANNEL HALL THRUSTER; Roland Florenz and Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, US; Peter Y. Peterson, ElectroDynamics Applications Inc., Ann Arbor, MI, 48105 US

2011-247: CATHODE EFFECTS ON OPERATION AND PLASMA PLUME OF THE PERMANENT MAGNET CYLINDRICAL HALL THRUSTER; Jean C. Gayoso, Yevgeny Raitses, and Nathaniel J. Fisch, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543

2011-248: PLASMA SHEET VELOCITY MEASUREMENT TECHNIQUES FOR THE PULSED PLASMA THRUSTER SIMP-LEX; Anuscheh Nawaz and Matthias Lau, Institute of Space Systems, University Stuttgart, Germany

2011-251: THE VASIMR ENGINE: BENEFITS, DRAWBACKS, AND TECHNOLOGICAL CHALLENGES; Molina Cabrera Pedro Andres and Tolyarenko Nikolai, International Space University, Strasbourg, Alsace, 67400, France

2011-252: NUMERICAL STUDY ON ELECTRODE MODEL FOR PLASMA SIMULATION OF MPD THRUSTER; K. Kubota, Japan Aerospace Exploration Agency, Chofu, 182-8522, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan; Y. Okuno, Tokyo Institute of Technology, Yokohama, Kanagawa, 226-8502, Japan

2011-253: THERMAL STRESS ANALYSIS OF SEVERAL HUNDRED KW RADIATION COOLED ARCJET; Daisuke Nakata, Muroran Institute of Technology, 27-1, Mizumoto-cho, Muroran-shi, Hokkaido 050-8585, Japan; Kiyoshi Kinefuchi, Japan Aerospace Exploration Agency, 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan; Hitoshi Kuninaka, Japan Aerospace Exploration Agency, 3-1-1, Yoshinodai, Chuoku, Sagamihara-shi, Kanagawa 252-5210, Japan

2011-254: THE DESIGN AND CONTROL OF HALL THRUSTERS USING THE DIMENSION SCALING LAW OF THE OPERATING POINTS; Taichiro Tamida, Advanced Technology R&D Center, Mitsubishi Electric Corporation, 8-1-1 Tukaguchi-honmachi, Amagasaki, Hyogo, 661-8661, Japan; Hiroyuki Osuga, Space System Department, Kamakura Works, Mitsubishi Electric Corporation, 325 Kamimachiya, Kamakura, Kanagawa, 247-8520, Japan; Naoji Yamamoto, Kyushu University, 6-1 Kasuga-Kouen, Kasuga, Fukuoka, 816-8580, Japan; Matsushi Miura, Institute for Unmanned Space Experiment Free Flyer, 2-12 Kanda-Ogawamachi, Chiyoda-Ku, Tokyo, 101-0052, Japan

2011-255: STUDY OF STOCHASTIC EFFECTS IN A HALL EFFECT THRUSTER USING A TEST PARTICLES MONTE-CARLO MODEL; P. Coche and L. Garrigues, LAPLACE (Laboratoire Plasma et Conversion d’Energie), UniversitÃ© de Toulouse, UPS, INPT Toulouse, 118, route de Narbonne, F-31062 Toulouse cedex 9, France

2011-256: HELICON ELECTRON SOURCE FOR OPERATION WITH AGGRESSIVE PROPELLANT; A. V. Loyan and S. Roshanpour, Zhukovskiy National Aerospace University “KhAI”, Kharkiv, 61070, Ukraine

2011-257: A VERY LOW POWER ARCJET (VELARC) FOR SMALL SATELLITE MISSIONS; Birk L. Wollenhaupt, Alex hammer, Georg Herdrich, Stefanos Fasoulas, and Hans-Peter RÃ¶ser, Institute for Space Systems, University of Stuttgart, 70569, Germany

2011-258: MODELING AND NUMERICAL SIMULATION OF A TWO-DIMENSIONAL MPD THRUSTER USING A HYDROGEN PROPELLANT; H. Sato, The Graduate University for Advanced Studies, Sagamihara, Kanagawa, 252-5210, Japan; K. Kubota, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2011-260: JOINT TRAJECTORY AND ENERGY MANAGEMENT SIMULATION OF LOW THRUST MISSIONS; A. Ruggiero, P. Pergola, and S. Marcuccio, Alta, Pisa, 56121, Italy

2011-261: HIGH POWER SOLAR ELECTRIC PROPULSION FOR HUMAN SPACE EXPLORATION ARCHITECTURES; Roger Myers and Christian Carpenter, Aerojet, Redmond, WA 98072, USA

2011-262: MICROWAVE-EXCITED MICROPLASMA THRUSTER WITH APPLIED MAGNETIC FIELD; Tetsuo Kawanabe, Takeshi Takahashi, Yoshinori Takao, Koji Eriguchi, and Kouichi Ono, Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University, Yoshida-Honmachi, Sakyo-ku, Kyoto 606-8501, Japan

2011-264: CHARACTERIZATION OF A CYLINDRICAL HALL THRUSTER WITH PERMANENT MAGNETS; R. Spektor, K. D. Diamant, E. J. Beiting, K. A. Swenson, and D. T. Goddard, The Aerospace Corporation; Y. Raitses and N. J. Fisch, Princeton Plasma Physics Laboratory

2011-266: MICRO-CATHODE ARC THRUSTER DEVELOPMENT AND CHARACTERIZATION; Taisen Zhuang, Alexey Shashurin, Dereck Chiu, George Teel and Michael Keidar, The George Washington University, Department of Mechanical and Aerospace Engineering Washington, DC 20052

2011-268: PERFORMANCE OF POROUS TUNGSTEN NEEDLE LMIS FOR USE AS INDIUM FEEP EMITTERS; I. Vasiljevich, N. Buldrini, and F. Plesescu, Fotec Forschungs- und Technologietransfer GmbH, Wiener, Neustadt, Austria; C. Scharlemann, University of Applied Sciences Wiener Neustadt, Austria

2011-269: PERFORMANCE AND PLUME CHARACTERIZATION OF A HELICON HALL THRUSTER; Peter Y. Peterson and Dean R. Massey, ElectroDynamic Applications, Inc., Ann Arbor, MI, 48105, USA; Adam Shabshelowitz, Rohit Shastry, and Raymond Liang, The University of Michigan, Ann Arbor, MI, 48105, USA

2011-270: ENERGY DEPOSITION AT THE PROBE SURFACE UNDER PLASMA CONDITIONS TYPICAL FOR ION THRUSTER; A. Cenian, a. Chernukho, and H. Rachubinski, The Szewalski Institute of Fluid-Flow Machinery, PASci, 80-952 Gdansk, ul. Fiszera 14, Poland; M. Dudeck, University of Paris 6, 75252 Paris, France

2011-271: GRADIENT INSTABILITIES IN HALL THRUSTER PLASMAS; A. I. Smolyakov and W. Frias, Univerity of Saskatchewan, Saskatoon, SK S7N 5E2, Canada; Y Raitses and I. D. Kaganovich, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ 08543, USA

2011-274: HIGH ISP MECHANISM OF RECTANGULAR LASER-ELECTROMAGNETIC HYBRID ACCELEARTION THRUSTER; Hideyuki Horisawa, Yuki Mashima, and Osamu Yamada, Dept. Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, JAXA/ISAS, Sagamihara, Kanagawa, 252-5210, Japan

2011-275: TWO-DIMENSIONAL, APPLIED-FIELD MPD THRUSTER USING A HOLLOW CATHODE; Shigeru Yokota, Daisuke Ichihara, Masaki Yonemoto and Akihiro Sasoh, Nagoya University, Nagoya, Aichi, 464-8603, Japan

2011-277: FEASIBILITY OF CAPTURING AND RETURNING SMALL NEAR-EARTH ASTEROIDS; John R. Brophy, Robert Gershman, Damon Landau, James Polk, Chris Porter, and Don Yeomans, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; Carlton Allen and Williw Williams, NASA Johnson Space Center, Houston, Texas; Erik Asphaug, University of California at Santa Cruz, Santa Cruz, California

2011-279: EXPERIMENTAL INVESTIGATION OF PLASMA ACCELERATION BY ROTATING ELECTRIC FIELD FOR ELECTRODELESS PLASMA THRUSTER; Takahiro Nakamura, Kenji Yokoi, Hiroyuki Nishida, and Shunjirou Shinohara, Tokyo University of Agriculture and Technology, Koganei, Tokyo 184-8588, Japan; Ikkoh Funaki and Takeshi Matsuoka, Institute of Space and Astronautical Science, Sagamihara, Kanagawa 252-5210, Japan; Takao Tanikawa, Tokai University, Hiratsuka, Kanagawa 259-1292, Japan; Tohru Hada, Kyushu University, Kasuga, Fukuoka 816-8580, Japan; Konstantin P. Shamrai and Timofei S. Rudenko, Institute of Nuclear Research, Nauki, Kiev 03680, Ukraine

2011-280: VUV RADIATION IN A HALL EFFECT THRUSTER; PRELIMINARY RESULTS; M. Lino da Silva, Instituto de Plasmas e Fusao Nuclear, LaboratÃ³rio Associado, Instituto Superior TÃ©cnico, 1 Av. Rovisco Pais, 1049-001 Lisbon, Portugal; M. Dudeck, UniversitÃ© Pierre et Marie Curie, 4 Place Jussieu, 75005 Paris, France

2011-285: NUMERICAL SIMULATION FOR THE EFFECT OF CONDUCTIVE WALL NEAR THE EXIT OF A 1KW ATON-TYPE HALL THRUSTER CHANNEL ON ION FOCUSING ACCELERATION; Shaowei Qing, Daren Yu, and Hui Liu, Lab of Plasma Propulsioin, Mail Box 458, Harbin Institute of Technology, Harbin, Heilongjiang, 150001, China; Xiaogang Wang, State Key Lab of Nuclear Physics & Technology, School of Physics, Peking University, Beijing 100871, China; Ping Duan, School of Physics, Dalian Maritime University, Dalian, 116024, China

2011-286: STUDY ON IONIZATION CHARACTERISTICS OF LOW POWER HALL THRUSTER WITH VARIABLE CROSS-SECTION CHANNEL; Zhongxi Ning, Shiqiang Zhang, Hui Liu, and Daren Yu, Harbin Institute of Technology Plasma Propulsion Laboratory, Harbin, 150001, China

2011-287: AUTONOMOUS STATION KEEPING FOR LEO MISSIONS WITH A HYBRID CONTINUOUS/IMPULSIVE ELECTRIC PROPULSION SYSTEM; Andrea Garulli and Antonio Giannitrapani, UniversitÃ¡ degli Studi di Siena, Siena, 53100, Italy; Mirko Leomanni and Fabrizio Scortecci, Aerospazio Tecnologie s.r.l., Rapolano Terme, Siena, 53040, Italy

2011-288: INFLUENCE OF HYDROGEN ONTO WORK SURFACES OF DISCHARGE CHAMBER OF SPT MAG; Antonina I. Bugrova, Alexey V. Desyatskov, Vadim K. Kharcchevnikov, Marina V. Kozintseva, Pavel G. Smirnov and Vasiliy A. Terehov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, 119454, Russia; Stephan Zurbach, Snecma, Safran Group, Vernon, 27208, France; Helen V. Chubunova, National Research Nuclear University, “MEPHI”, Moscow, 115409, Russia; Vatslovas S. Kulikauskas, Lomonosov Moscow State University Skobeltsyn Institute of Nuclear Physics, Moscow, 119991, Russia

2011-289: THRUST PERFORMANCE OF A MICRO-MULTI-PLASMAJET-ARRAY THRUSTER; Ryosuke Hitomi, Naoto Kobayashi, Kazuki Asanuma, and Hideyuki Horisawa, Dept. Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, JAXA/ISAS, Kanagawa, 252-5210, Japan

2011-290: DESIGN OF HIGH-POWER HIGH-SPECIFIC IMPULSE RF-ION THRUSTER; H. W. Loeb and D. Feili, 1^st Institute of Physics, Giessen University, Heinrich-Buff-Ring 16, 35392 Giessen, Germany; G. A. Popov, V. A. Obukhov, V. V. Balashov, and A. I. Mogulkin, Research Institute of Applied Mechanics and Electrodynamics of MAI P/O Box 43, 125080 Moscow, Russia; V. M. Murashko and A. N. Nesterenko, EDB “Fakel”, 236001, 181 Moskovskiy av., Kaliningrad, Russia; S. Khartov, Moscow Aviation Institute, 4 Volokolamskoye shosse, 123993 Moscow, Russia

2011-291: A NEW FLEXIBLE MAGNETIC CIRCUIT FOR A HALL EFFECT THRUSTER; C. Henaux, R. Vilamot, and D. Harribey, LAPLACE (Laboratoire Plasma et Conversion d’Energie), CNRS; LAPLACE, F-31062 Toulouse, France; L. Garrigues, rue Charles Camichel, F-31071 Toulouse cedex 7, France, LAPLACE (Laboratoire Plasma et Conversion d’Energie), CNRS, LAPLACE; F-31062 Toulouse, France

2011-292: NUMERICAL ANALYSIS OF BEAM-SUPPORTED DETONATION PROPAGATING THROUGH AXISYMMETRIC TUBE; H. Shiraishi, Daido University, Nagoya, 457-8530, Japan

2011-293: FORECAST OF EROSION RATE OF SPT K-0 CHANNEL INSULATORS BY SPECTRAL MEASUREMENTS; Marina V. Kozintseva, Alexander S. Lipatov, Andrew M. Bishaev, Gleb e. Bugrov and Michael I. Shaposhnikov, Moscow Institute of Radio-engineering, Electronics and Automatics, Moscow, 119454, Russia; Yu Daren and Ning Zhongxi, Harbin Institute of Technology, Harbin, 150001, China

2011-294: DEVELOPMENT STATUE OF ATOMIC OXYGEN SIMULATOR FOR AIR BREATHING ION ENGINE; Yasuyoshi Hisamoto, Graduate University for Advanced Studies, Sagamihara, Kanagawa, 252-5210, Japan; Kazutaka Nishiyama, Japan Aerospace Exploration Agency/Institute of Space and Astronautical Science, Sagamihara, Kanagawa 252-5210, Japan; Hitoshi Kuninaka, Japan Aerospace Exploration Agency/Institute of Space and Astronautical Science, Sagamihara, Kanagawa 252-5210, Japan

2011-295: DEVELOPMENT OF A MICRO-MULTI-PLASMAJET-ARRAY THRUSTER; Naoto Kobayashi, Ryosuke Hitomi, Kazuki Asanuma and Hideyuki Horisawa, Dept. Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5120, Japan

2011-297: PERFROMANCE EVALUATION OF A MINIATURE ION THRUSTER Âµ1 WITH A UNIPOLAR AND BIPOLAR OPERATION; Hiroyuki Koizumi, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan; Hitoshi Kuninaka, Japan Aerospace Exploration Agency/Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 252-5210, Japan

2011-298: SHEATHINSTABILITY AND VELOCITY-SPACE DIFFUSION IN EXB DISCHARGES WITH STRONG SECONARY ELECTRON EMISSION; M. Campanell, A. Khrabrov, I. D. Kaganovich, and Y. Raitses, Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jersey 08543, USA; D. Sydorenko, Department of Physics, University of Alberta, Alberta, Canada; A. Smolyakov, Department of Physics and Engineering Physics, University of Saskatchewan S7N 5E2, Canada

2011-299: ION AND DROPLET MASS MEASUREMENTS OF AN ELECTROSPRAY EMITTER USING AN EXB FILTER; Kurt J. Terhune and Dr. Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2011-300: SIMULATION OF SELF-NEUTRALIZATION TECHNIQUES FOR CHARGED PARTICLE THRUSTERS; David C. Liaw, Brian E. Gilchrist, and Thomas M. Liu, University of Michigan, Ann Arbor, MI, 48109, USA

2011-301: MASS AND PLASMA CHARACTERISTICS IN THE CURRENT SHEET OF A PULSED PLASMA THRUSTER; Tony SchÃ¶nherr and Kimiya Komurasaki, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan; Sebastian Manna, Matthias Lau, Georg Herdrich, and Stefanos Fasoulas, UniversitÃ¤t Stuttgart, Stuttgart, Baden-WÃ¼rttemberg, 70569, Germany

2011-302: TWO-PHOTON SPECTROSCOPY ON NEUTRAL XENON IN THE PLUME OF THE RADIO-FREQUENCY ION THRUSTER RIT-10; Christoph Eichhorn, Stefan LÃ¶hle and Stefanos Fasoulas, Institut fÃ¼r Raumfahrtsysteme, IRS, UniversitÃ¤t Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany; Hans Leiter, EADS Astrium Space Transporation GmbH, Post Box 1119, D-74215 MÃ¶ckmÃ¼hl, Germany; Monika Auweter-Kurtz, German Aerospace Academy ASA, im Forum 1 am Konrad Zuse Platz 1, D-71034 BÃ¶blingen, Germany

2011-303: ELECTRIC PROPULSION POINTING MECHANISIM FOR BEPI COLOMBO; Christian Neugebauer and Paul Janu, RUAG Space GmbH, Stachegasse 16,1120 Vienna, Austria; Rudolf Schermann, RUAG Space GmbH, Stachegasse 16.1120 Vienna, Austria; Andreas Derntl, RUAG Space GmbH, Stachegasse 16, 1120 Vienna, Austria

2011-304: PLASMA MAGNETOSHELL FOR AEROBRAKING AND AEROCAPTURE; John Slough, David Kirtley, and Anthony Pancotti, MSNW LLC, Redmond, WA, 98052, USA

2011-305: PARAMETRIC STUDY ON SHAPE DEPENDENCE OF INDUCTIVELY COUPLED PLASMA CATHODE FOR PERFORMANCE IMPROVEMENT; Takuya Nakabayashi, Hiroki Watanabe, Satoshi Kasagami, Junichiro Aoyagi, and Haruki Takegahara, Department of Aerospace Engineering, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2011-306: EVALUATION OF PULSED PLASMA THRUSTER PERFORMANCE BY INCREASE OF ELECTRIC POWER; Daiki Mimura, Kyohei Umeda, Yohei Kitazono, Takahiro Shindo, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Department of Aerospace Engineering, 6-6 Asahigaoka hino, Tokyo, 191-0065, Japan

2011-307: ON THE KINETIC MODELING OF COLLISIONAL EFFECTS RELEVANT FOR NON-STATIONARY MAGNETOPLASMADYNAMIC THRUSTERS; Dejan Petkow, ESA-ESTEC, Noordwijk, 2200 AG, The Netherlands; Georg Herdich and Stefanos Fasoulas, Institute of Space Systems, UniversitÃ¤t Stuttgart, Stuttgart, 70569, Germany; Monika Auweter-Kurtz, German Aerospace Academy ASA, 71304, BÃ¶blingen, Germany

2011-308: MICRO-THRUSTER OPTIONS FOR THE JAPANESE SPACE GRAVITATIONAL WAVE OBSERVATORY MISSIONS; Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Minami, Kanagawa, 252-5210, Japan; Yoshinori Nakayama, National Defense Academy, Yokosuka, Kanagawa, 239-8686, Japan; Hideyuki Horisawa, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Masaki Ando, Kyoto University, Kitashirakawa, Sakyo, Kyoto 606-8502, Japan

2011-309: THE ION ENGINE SYSTEM FOR HAYABUSA2; Kazutaka Nishiyama, Satoshi Hosoda, Kazuma Ueno, and Hitoshi Kuninaka, Japa Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2011-311: ON THE KINETIC MODELING OF FUSION PROCESSES IN IEC DEVICES; Dejan Petkow, ESA-ESTEC, Noordwijk, 2200 AG, The Netherlands; Georg Herdrich, Constanze Syring, and Stefanos Fasoulas, Institute of Space Systems, Pfaffenwaldring 29, Stuttgart, 70569, Germany

2011-312: AN ADAPTABLE POWER CONTROL UNIT FOR ION THRUSTER MICRO-PROPULSION SUBSYSTEMS; Luca Ceruti and Aldo Polli, SELEX Galileo S.p.A., Viale Europa – 20014 Nerviano, Italy

2011-317: PRELIMINARY STUDY OF AN ARCJET PLASMA TORCH FOR GASIFICATION AND MATERIAL PROCESSING APPLICATIONS; Paolo Gessini, Augusto CÃ©sar de Mendonca Brasil, Rafael Moorgado Silva, Manuel Nascimento Dias Barcelos JÃºnior, University of Brasilia, Gama, DF, 72405-610, Brazil, JosÃ© Leonardo Ferreira and Ivan Soares Ferreira, University of Brasilia, Brasilia, DF, 70919-970, Brazil; Domenico Simone and Claudio Bruno, University of Rome “La Sapienza”, Rome, 00184, Italy

2011-318: NUMBER DENSITY MEASUREMENT OF XE I IN THE ECR ION THRUSTER Âµ10 USING OPTICAL FIBER PROBE; Ryudo Tsukizaki and Hiroyuki Koizumi, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan; Kazutaka Nishiyama and Hitoshi Kuninaka, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Chuo-ku, Sagamihara, Kanagawa, 229-8510, Japan

2011-319: Development and Performance of Permanent Magnet Hall Thruster; JosÃ© Leonardo Ferreira, Ivan S. Ferreira, Brunno S. Moraes, Gabriela C. Possa, Geovany Borges, and Alexandre M. Oliveira, Campus Darcy Ribeiro, Plano Piloto, Asa Norte, 70910-900 Brasilia-DF, Brazil; Paolo Gessini, Business of Academic Affiliation 2, City, Province, Zip Code, Country

2011-320: EXPERIMENTAL INVESTIGATION ON CW LASER MICROTHRUSTER; Hitoshi Yonnamine, Keiji Hagiwara, and Hideyuki Horisawa, Dept. Aeronautics and Astronautics, Tokai University, Hiratuka, Kanagawa, 259-1292, Japan; Yuya Oshio, Hiroki Sato, and Ikkoh Funaki, JAXA/ISAS, Sagamihara, Kanagawa, 252-5210, Japan

2011-322: CONTROL OF THRUST MEASUREMENT SYSTEM FOR CW LASER THRUSTERS; Keiji Hagiwara, Hitoshi Yonamine, and Hideyuki Horisawa, Dept. Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan; Yuya Oshio, Hiroki Sato, and Ikkoh Funaki, JAXA/ISAS, Sagamihara, Kanagawa, 252-5210, Japan

2011-323: SELF-CONSISTENT SIMULATION OF THE COUPLING BETWEEN PLASMA AND NEUTRAL GAS IN ÂµN-RIT; R. Henrich, D. Feili, and C. Heiliger; I. Physikalisches, Justus Liebig University, 35392, Germany

2011-325: RIT MICROPROPULSION SYSTEM ON LISA PATHFINDER; D. Di Cara, S. Strandmoe, J. A. Romera Perez, and L. Stagnaro, ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk ZH, The Netherlands; H. Leiter and R. Killinger, Astrium GmbH BL Equipement and Propulsion, P.O. 1119, 774215 MÃ¶ckmÃ¼hl, Germany; D. Feili and B. Lotz, I. Physics Institute of Justus Liebig University, Giessen, D-35392, Germany; A. Polli and L. Ceruti, SELEX Galileo S.p.A., Viale Europa, 20014 Nerviano, Italy

2011-326: THE DAWN OF VESTA SCIENCE; Charles E. Garner, Marc d. Rayman, John R. Brophy, and Steven C. Mikes, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2011-327: THE GOCE ION PROPULSION ASSEMBLY - LESSONS LEARNT FROM THE FIRST 22 MONTHS OF FLIGHT OPERATIONS; Neil Wallace, Peter Jameson, and Christopher Saunders, QinetiQ Ltd, Farnborough, UK; Michael Fehringer and Clive Edwards, ESA-ESTEC, Noordwijk, The Netherlands; Rune Floberghagen, ESA-ESOC, Darmstadt, Germany

2011-328: ROUND-TRIP DEEP SPACE MANEUVER OF MICROWAVE DISCHARGE ION ENGINES ONBOARD HAYABUSA EXPLORER; Hitoshi Kuninaka, JSPEC/JAXA, Yoshinodai, Chuo, Sagamihara, Kanagawa JAPAN

2011-329: ESA ELECTRIC PROPULSION ACTIVITIES; J. Gonzalez and G. Saccoccia, Business or Academic Affiliation 1

2011-330: AN OVERVIEW OF NASA’S ELECTRIC PROPULSION PROGRAMS, 2010-11; James E. Polk, Principal Engineer, Propulsion and Materials Engineering Section, Jet Propulsion Laboratory, California Institute of Technology M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; Hani Kamhawi, Senior Aerospace Engineer, Propulsion and Propellants Branch, Glenn Research Center, 21000 Brookpark Rd, Cleveland, OH; Kurt Polzin, Propulsion Research Engineer, Propulsion Research and Technology Applications Branch, Propulsion Systems Department, Marshall Space Flight Center, Huntsville, AL 35812; John Brophy, Principal Engineer, Propulsion and Materials Engineering Section, Jet Propulsion Laboratory, California Institute of Technology, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; John Ziemer, Senior Engineer, Propulsion and Materials Engineering Section, Jet Propulsion Laboratory, California Institute of Technology, M/S 125-109, 4800 Oak Grove Drive, Pasadena, CA 91109; Timothy D. Smith; Advanced In-Space Propulsion Project Manager, Glenn Research Center, 21000 Brookpark Rd, Cleveland, OH; Mike LaPointe, Deputy Manager, Science and Exploration Research Office, Marshall Space Flight Center, Huntsvile, AL 35812

2011-332: OVERVIEW OF JAXA’S ACTIVITIES ON ELECTRIC PROPULSION; Hitoshi Kuninaka, Lunar and Planetary Exploration Program Group, Japan Aerospace Exploration Agency, Yoshinodai, Chuo, Sagamihara, Kanagawa, 252-5210, Japan; Kenichi Kajiwara, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Sengen, Tsukuba, Ibaragi, 305-8686, Japan

2011-334: O-D PLASMA MODEL FOR ORIFICED HOLLOW CATHODES; Jorge Palacio Mizrahi, Vlad Vekselman, Yakov Krasik, and Victor Gurovich, Technion-Israel Institute of Technology, Kiryat ha Technion, Haifa, 32000, Israel

2011-335: ION SOURCES FOR NEUTRAL BEAM HEATING OF FUSION PLASMAS; Paul McNeely, Max-Planck- Institut fÃ¼r Plasmaphysik, Teilinstitut Greifswald, WendelsteinstraÃŸe 1, 17491 Greifswald

2011-337: ESTIMATION OF THE ELECTRON TEMPERATURE AND DENSITY IN THE PLASMA OF A HALL THRUSTER; J. Cavalier, N. Lemoine, and G. Bonhomme, Institut Jean Lamour, UHP, 54506, Vandoeuvre les Nancy, France; S. Tsikata, C. HonorÃ©, D. GrÃ©sillon, Laboratoire de Physique des Plasmas, Ecole Polytechnique, route de Saclay, 91128 Palaiseau, France

2011-338: KINETIC MODEL OF A PLASMA IN CONTACT WITH AN ION-EMITTING ANODE SURFACE; Edmond J. Meyer IV and Dr. Lyon B. King, Michigan Technological University, Houghton, MI, 49931, USA

2011-339: OVERVIEW OF HALL THRUSTER ACTIVITIES AT NASA GLENN RESEARCH CENTER; Hani Kamhawi, George Soulas, Luis Pinero, Daniel Herman, Jonathan VanNoord, Wensheng Huang, Rohit Shastry, Thomas Haag, and John Yim, National Aeronautics and Space Administration Glenn Research Center, Cleveland, Ohio, 44135; George Williams, Ohio Aerospace Institute, Cleveland, Ohio 44135

2011-340: PULSED PLASMA THRUSTERS: A WORLDWIDE REVIEW AND LONG YEARNED CLASSIFICATION; Molina-Cabrera P., Herdrich G., Lau M., Fausolas S., University of Stuttgart, Stuttgart, 70569, Germany; Schoenherr T. and Komurasaki K., University of Tokyo, Tokyo, 7-3-1, Hoongo, Bunkyo, Japan

2011-341: AN OVERVIEW OF ESSENTIAL PARAMETERS ON ABLATIVE PPT PERFORMANCE; Abdolrahim Rezaeiha, Sharif University of Technology, Tehran, Iran; Tony SchÃ¶nherr, The University of Tokyo, Tokyo, Japan

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2013 INDEX

2013-33: WEAR TEST OF A MAGNETICALLY SHIELDED HALL THRUSTER AT 3000 SECONDS SPECIFIC IMPULSE; Richard R. Hofer, Benjamin A. Jorns, James E. Polk, Ioannis G. Mikellides, and John Steven Snyder, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-37: EUROPEAN SPACE AGENCY ACTIVITIES IN ELECTRIC PROPULSION; Jose Gonzalez del Amo, European Space Agency, Noordwijk, 2200AG, The Netherlands

2013-44: PEAK POWER TRACKING AND MULTI-THRUSTER CONTROL IN DIRECT DRIVE SYSTEMS; John Steven Snyder and John R. Brophy, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-45: SOLAR ELECTRIC PROPULSION (SEP) BENEFITS FOR NEAR TERM SPACE EXPLORATION; Luke DeMaster-Smith, Scott Kimbrel, Christian Carpenter, Steve Overton, Roger Myers, and David King, Aerojet Rocketdyne, Inc., Redmond, WA 98052

2013-47: INITIAL FLIGHT TEST RESULTS OF THE LIPS-200 ELECTRIC PROPULSION SYSTEM ON SJ-9A SATELLITE; Zhang Tianping, Wang Xiaoyong, Jiang Haocheng, Wang Shaoning, Gao Jun, Xu Jinling, Cui Tieming, Yang Fuqan, Guo Ning, Tang Fujun, Chen Xuekang, Lanzhou Institute of Physics, Lanzhou, Gansun, 730000, China

2013-48: THE ELECTRIC PROPULSION DEVELOPMENT IN LIP; Zhang Tianping, Sun Mingming, Long Jianfei, and Zhou Haocheng, Lanzhou Institute of Physics, Lanzhou, Gansu Province, 730000, China

2013-51: INFLUENCE OF SPT MAGNETIC FIELD ON LIFE TIME CHARACTERISTICS OF THE THRUSTER; Olga A. Mitrofanova and Roman Yu. Gnizdor, EDB “Fakel”, Kaliningrad, Russia

2013-52: DEVELOPMENT AND RESEARCH OF THE PLASMA THRUSTER WITH A HOLLOW MAGNET ANODE PLAS-40; M. Yu. Potapenko, V. V. Gopanchuk, FSUE EDB Fakel, Kaliningrad, 236001, Russia

2013-53: NEAR FIELD MAPS OF XENON ION VELOCITY OF THE SPT-140 HALL THRUSTER BY LASER INDUCED FLUORESCENCE; Edward J. Beiting, Rostislav Spektor, and Kevin D. Diamant, The Aerospace Corporation, P.O. Box 929057 – M2/341, Los Angeles, CA 90009, USA; Ron Corey and Jorge Delgado, Space Systems/Loral, 3825 Fabian Way, Palo Alto, CA 94303, USA

2013-54: AUTONOMOUS TESTS OF THE CATHODE FOR USE IN THE DISCHARGE CHAMBER OF THE HIGH POWER ION THRUSTER; A. S. Lovtsov, P. M. Puchkov, and V. N. Shutov, SSC FSUE Keldysh Research Centre, Onezhskaya, 8, & Moscow, Russia, 125438

2013-55: DEVELOPMENT AND QUALIFICATION OF HALL THRUSTER KM-60 AND THE FLOW CONTROL UNIT; A. N. Kostin, A. S. Lovtsov, A. I. Vasin, and V. V. Vorontsov, SSC FSUE Keldysh Research Centre, Onezhskaya, 8, Moscow, Russia, 125438

2013-56: ON SCALING OF HALL EFFECT THRUSTERS; Andrey A. Shagayda, Keldysh Research Center, Moscow, 125438, Russia

2013-57: FARFIELD PLUME MEASUREMENT AND ANALYSIS ON THE NASA-300M AND NASA-300MS; Wensheng Huang, Rohit Shastry, George C. Soulas, and Hani Kamhawi, National Aeronautics and Space Administration Glenn Research Center, Cleveland, Ohio, 44135, USA

2013-58: EFFECT OF BACKGROUNG PRESSURE ON THE PERFORMANCE AND PLUME OF THE HIVHAC HALL THRUSTER; Wensheng Huang, Hani Kamhawi, and Thomas Haag, National Aeronautics and Space Administration Glenn Research Center, Cleveland, Ohio, 44135, USA

2013-60: HOLLOW CATHODE LIFE TEST FOR THE 80 MN HALL THRUSTER; Qiao Caixia, Kang Xiaolu, Yu Shuilin, Zhang Yan, Hang Guanrong, and Zhao Zhen, Shanghai Institute of Space Propulsion, Shanghai, 201112, China

2013-62: AN ELECTRIC PROPULSION SYSTEM BASED ON CONTROLLED FUSION AND ELECTROMECHANICAL ENERGY CONVERSION; P. J. Turchi, Santa Fe, New Mexico, USA

2013-63: EPS-500 DEVELOPMENT STATUS; F. Marchandise, V. Vial, M. Oberg and N. Cornu, Snecma Direction Moteurs Spatiaux, Vernon, 27200, France, D. Barbier, Sagem DÃ©fense SÃ©curitÃ©, Valence, 26000, France, N. Arcis, CNES, Toulouse, 31401, France

2013-64: A NEW ORBIT CONTROL ALGORITHM FOR THE 20 MN CLASS ION ENGINE SYSTEM; Hiroshi Nagano and Yukio Hayakawa, Japan Aerospace Exploration Agency, Chofu, 182-8522, Japan, Hiroyuki Osuga, Toshiyuki Ozaki, and Kazuo Shuto, Mitsubishi Electric Corporation, Kamakura, 247-8520, Japan

2013-65: ACTIVITIES OF VNIIEM IN EPT FIELD HISTORY, OUR DAYS AND PROSPECTS; Vladimir P. Khodnenko, VNIIEM ‘Corporation’ JSD, Address: POB 496, Glavpochtamt, Moscow, 101000, Russia

2013-66: IONOSFERE SATELLITE WITH APPT BASED EPS; Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia, Michael N. Kazeev, National Research Centre Kurchatov Institute, I, Kurchatov sq., Moscow, 123182, Russia, Vladimir P. Khodnenko, VNIIEM Corporation’ JSC, 101000, P. O. Box 496, Moscow, Russia

2013-67: NON-EQUIDISTANT PARTICLE-IN-CELL FOR ION THRUSTER PLUMES; K. F. Luskow, J. Duras, O. Kalentev, K. Matyash, J. Geiser, and R. Schneider, Ernst-Moritz-Arndt Universitat Greifswald, Felix-Hausdorff-Strabe 12, 17489 Greifswald, Germany, D. Tskhakaya, Institute of Applied Physics, Vienna University of Technology, Wiedner Hauptstrasse 8-10/E134, A-1040 Vienna, Austria

2013-68: ABLATIVE PULSED PLASMA THRUSTERS R&D IN RUSSIA SINCE THE BEGINNING OF THE 90S; Nickolay N. Antropov and Garry A. Popov, Research Institute of Applied Mechanics and Electrodynamics, 4, Volokolamskoye shosse, Moscow, 125810, Russia, Michael N. Kazeev, National Research Centre Kurchatov Institute, pl. Kurchatove, I. Moscow, 123182, Russia

2013-70: PRECISE ATTITUDE CONTROL OF ALL-ELECTRIC GEO SPACECRAFT USING XENON MICROTHRUSTERS; Mirko Leomanni, Andrea Garulli, and Antonio Giannitrapani, UniversitÃ¡ di Siena, Siena, 53100, Italy, Fabrizio Scortecci, Aerospazio Tecnologie s.r.l., Rapolano Terme, Siena, 53040, Italy

2013-71: ION BEAM INSTABILITY IN HALL THRUSTERS; A. Kapulkin and E. Behar, Asher Space Research Institute, Technion-Israel Institute of Technology, Haifa, 32000, Israel, Y. Raitses, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2013-72: GENERATION OF MICROWAVE RANGE ELECTROMAGNETIC RADIATION IN THE HALL THRUSTER PLASMA; Sergey A. Oghienko, National Aerospace University “Kharkiv Aviation Institute”, Kharkiv, 61070, Ukraine

2013-73: SELF-CONSISTENT SIMULATIONS OF INTERACTIONS BETWEEN SPACECRAFT AND PLUMES OF ELECTRIC THRUSTERS; Carlos Ardura, Sogeti High Tech of Astrium Satellites, Toulouse, 31000 France, and Fred Gengembre, ESAESTEC, Noordwijk 2201, The Netherlands

2013-76: HIGH CURRENT HOLLOW CATHODE PLASMA PLUME MEASUREMENTS; Robert e. Thomas and Hani Kamhawi, NASA Glenn Research Center, Cleveland, OH, 44135, USA, George J. Williams, Jr., Ohio Aerospace Institute, Cleveland, OH, 44135, USA

2013-77: WALL-INDUCED CROSS-FIELD ELECTRON TRANSPORT WITH OBLIQUE MAGNETIC FIELD LINES; Jan Miedzik and Serge Barral, Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland, Stephan Zurbach, Snecma, Safran Group, 27208 Vernon, France

2013-079: SPATIALLY RESOLVED MOMENTUM FLUX MEASUREMENTS FOR THRUSTER PLUME DIAGNOSTICS; Alexander Spethmann, Thomas Trottenberg, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

2013-80: AZIMUTHAL OSCILLATIONS AND DYNAMICS OF ELECTRONS INTO CHANNEL OF STATIONARY PLASMA THRUSTER; A. N. Veselovzorov, A. A. Pogorelov, E. B. Svirsky, V. A. Smirnov, National Research Centre ‘Kurchatov Institute’ Moscow, Russia

2013-82: NEAR-EARTH ASTEROID RETRIEVAL MISSION (ARM) STUDY; John R. Brophy and Brian Muirhead, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

2013-83: EXPERIMENTAL RESEARCH OF DEFLECTION OF SPT THRUST VECTOR; Marina V. Kozintseva, Andrew M. Bishaev, Antonina I. Bugrova, Gleb E. Bugrov, Alexey V. Desyatskov, Alexander S. Lipatov, Vadim K. Kharchevnikov, and Pavel G. Smirnov, Moscow State Technical University of Radioengineering, Electronics and Automation, Moscow, 119454, Russia

2013-85: NUMERICAL DETERMINIATION OF INDUCED ELECTRIC EDDY FIELDS INSIDE ARBITRARILY SHAPED INDUCTION COILS; Chris Volkmar, Jens Simon, and Ubbo Ricklefs, Technische Hochschule Mittelhessen University of Applied Sciences, 35390 Giessen, Germany

2013-86: TRAVELING MAGNETIC FIELD PLASMA ACCELERATOR; Andrea Lucca Fabris, University of Padova, Padova, 35131, Italy; Mark A. Cappelli, Stanford University, Stanford, CA 94305, USA

2013-88: ENTROPY CLOSURE MODEL FOR TRANSPORT IN HALL THRUSTER SIMULATIONS; M. A. Cappelli and E. Cha, Stanford University, Stanford, CA 94305, USA, and E. Fernandez, Eckerd College, St. Petersburg, FL 33711

2013-89: LOW AND HIGH FREQUENCY OSCILLATIONS OF THE ACCELERATING ELECTRIC FIELD IN A HALL THRUSTER; J. Vaudolon, B. Khiar, and S. Mazouffre, CNRS – ICARE (Institut de Combustion, Aerothermique, Reactivite et Environnement), 1C, Avenue de la Recherche Scientifique, 45071 Orleans Cedex 2, France

2013-90: EXPERIMENTAL VALIDATION OF RIT MICRO-PROPULSION SUBSYSTEM PERFORMANCE AT EPL; D. Di Cara, A. Bulit, J. Gonzalez del Amo, and J. A. Romera, ESA/ESTEC, 2201AZ Noordwijk, The Netherlands, H. Leiter, D. Lauer, C. Altmann, and R. Kukies, Astrium GmbH BL Equipement and Propulsion, 74215 Mockmuhl, Germany, A. Polli, L. Ceruti, and A. Antimiani, SELEX ES, 20014 Nerviano, Italy, D. Feili and B. Lotz, I. Physics Institute of Justus Liebig University, Giessen, 35392, Germany, L. Serafini, Astrium SrL, 00196, Rome, Italy

2013-93: ALL EP PLATFORM: MISSION DESIGN CHALLENGES AND SUBSYSTEM DESIGN OPPORTUNITIES; E. Rezugina and A. DemairÃ©, OHB Sweden AB, Solna, SE-17122, Sweden; A. Edfors, B. Andersson, P. Rathsman, E. Lamoureux and F. SjÃ¶berg, OHB Sweden AB, Solna, SE-17122, Sweden; M. De Tata, OHB System AG, Bremen, 28359, Germany

2013-94: PERFORMANCE CHARACTERISTICS OF STEADY-STATE MPD THRUSTERS WITH PERMANENT MAGNETS AND MULTI HOLLOW CATHODES FOR IN-SPACE PROPULSION; Norihide Koyama, Tomoya Suzuki, Taisuke Kubota, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan

2013-95: PERFORMANCE CHARACTERISTICS OF LOW-POWER ARCJET THRUSTERS USING LOW TOXICITY PROPELLANT HAN DECOMPASED GAS; Kazuma Matsumoto, Akira Iwakai, Fumihiro Inoue, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan, Taiichi Nagata and Ideo Masuda, Japan Aerospace Exploration Agency, 2-1-1, Sengen, Tsukuba, Ibaraki 305-8505, Japan

2013-96: PERFORMANCE CHARACTERISTICS OF HIGH-POWER, HIGH SPECIFIC-IMPULSE HALL THRUSTERS FOR JAPANESE IN-SPACE PROPULSION; Yohei Mito, Masato Nishida, Taisuke Kagota, Tsuyoshi Kawamura, Tomoyuki Ikeda, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-ku, Osaka 535-8585, Japan

2013-97: RESEARCH AND DEVELOPMENT OF ELECTROTHERMAL PULSED PLASMA THRUSTER SYSTEMS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITES; Shuya Kisaki, Rikio Muraoka, Chen Huanjun, Masato Tanaka, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan, Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-98: THREE-DIMENSIONAL HYBRID-PIC SIMULATION OF MICROWAVE NEUTRALIZER; K. Kubota, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan; H. Watanabe and I. Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan; N. Yamamoto and H. Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan; and T. Miyasaka, Gifu University, Gifu, Gifu, 501-1193, Japan

2013-99: FLOWFIELD SIMULATION AND PERFORMANCE MEASUREMENT OF ELECTROTHERMAL PULSED PLASMA THRUSTERS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES; Masato Tanaka, Rikio Muraoka, Shuya Kisaki, Chen Huanjun, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535*8585, Japan, Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-100: R&D, LAUNCH AND INITIAL OPERATION OF THE OSAKA INSTITUTE OF TECHNOLOGY 1^ST PROITERES NANO-SATELLITE WITH ELECTROTHERMAL PULSED PLASMA THRUSTERS AND DEVELOPMENT OF THE 2^ND SATELLITE; Naoki Egami, Takaaki Matsuoka, Masaaki Sakamoto, Yoichi Inoue, Tomoyuki Ikeda, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan

2013-101: RESEARCH AND DEVELOPMENT OF HALL THRUSTER SERIES AT OSAKA INSTITUTE OF TECHNOLOGY; Masato Nishida, Yohei Mito, Taisuke Kagota, Tsuyoshi Kawamura, Tomoyuki Ikeda, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan

2013-102: PERFORMANCE PREDICTION OF ELECTROTHERMAL PULSED PLASMA THRUST SYSTEMS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES; Chen Huanjun, Rikio Muraoka, Shuya Kisaki, Masato Tanaka, and Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan, Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-103: RESEARCH AND DEVELOPMENT OF OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES WITH ELECTRIC ROCKET ENGINES; Rikio Muraoka, Shuya Kisaki, Chen Huanjun, Masato Tanaka, and hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya, Asahi-Ku, Osaka 535-8585, Japan; Takashi Wakizono, High Serve, 780-7, Tomehara, Akiruno, Tokyo 190-0152, Japan

2013-104: THE ISS SPACE PLASMA LABORATORY: A PROPOSED ELECTRIC PROPULSION ON-ORBIT WORKBENCH; Edgar A. Bering, III, and Gregg Edeen, University of Houston, Houston, Texas, 77204-5005; Spiro K. Antiochos, C. Richard DeVore, and Barbara J. Thompson, NASA/Goddard Space Flight Center, Greenbelt, Maryland, 20771; Mark Carter, Matthew Giambusso, Chris Olsen, and Jared Squire, Ad Astra Rocket Company, Webster, Texas, 77598; Davin Larson and James P. McFadden, University of California Berkeley, California, 94720; Benjamin Longmier, University of Michigan, Ann Arbor, Michigan, 48109; and David M. Smith, University of California, Santa Cruz, California, 95064

2013-105: FULL KINETIC ANALYSIS OF SMALL-SCALE MAGNETO PLASMA SAIL IN MAGNETIZED SOLAR WIND; Yasumasa Ashida, Kyoto University, Kyoto, 611-0011, Japan, Ikkoh Funaki, Japan Aerospace Exploration Agency, Kanagawa, 252-5210, Japan, Hiroshi Yamakawa, Kyoto University, Kyoto, 611-0011, Japan, Yoshihiro Kajimura, Akashi National College of Technology, Hyogo, 674-8501, Japan

2013-106: NEUTRAL PRESSURE MEASUREMENT IN AN ION THRUSTER DISCHARGE CHAMBER; Yoshinori Nakayama and Keninchi Narisawa, Department of Aerospace Engineering, National Defense Academy of Japan, 1-10-20, Hashirimizu, Tokosuka, Kanagawa 239-8686, Japan

2013-107: EXPERIMENTAL VISUALIZATION OF ION THRUSTER NEUTRALIZATION PHENOMENA; Futoshi Tanaka and Yoshinori Nakayama, National Defense Academy of Japan, Yokosuka, Kanagawa, 239-8686, Japan

2013-108: FLIGHT DEMONSTRATION AND APPLICATION OF ELECTRIC PROPULSION AT CAST; Chen Jian, Shen Yan, Hu Yanlin, Gao Jun, Beijing Institute of Control Engineering, Beijing, 100190, China

2013-109: DEVELOPMENT OF LOW-POWER CYLINDRICAL TYPE HALL THRUSTERS FOR NANO SATELLITE; Tomoyuki Ikeda, Yohei Mito, Masato Nishida, Taisuke Kagota, Tsuyoshi kawamura, and Hirokazu Tahara, Osaka Institute of Technology, Asahi-ku, Osaka, 535-858, Japan

2013-110: INVESTIGATION OF SIDE BY SIDE HALL THRUSTER SYSTEM; Takeshi Miyasaka and Katsuo Asato, Ryosuke Muraki, Daiki Furuta, and Kei Kubota, Gifu University, Gifu, 501-1193, Japan

2013-111: THEORETICAL MODEL OF A LANTHANUM HEXABORIDE HOLLOW CATHODE; Daniela Pedrini, University of Pisa, Pisa, 56126, Itlay, Riccardo Albertoni, Alta SpA, Ospedaletto, Pisa, 56121, Italy, Fabrizio Paganucci, University of Pisa, Pisa, 56126, Italy, and Mariano Andrenucci, Alta SpA, Ospedaletto, Pisa, 56121, Italy

2013-112: EXPERIMENTAL STUDY ON ELECTRODELESS ELECTROMAGNETIC ACCELERATION IN HELICON PLASMA THRUSTER; D. Kuwahara, S. Waseda, H. Ishii, N. Teshigahara, H. Fujitsuka, T. Ishii, S. Otsuka, T. Nakagawa, and S. Shinohara, Tokyo University of Agriculture and Technology, Koganei, Tokyo, 184-8588, Japan

2013-114: DEVELOPMENT AND QUALIFICATION STATUS OF THE ELECTRIC PROPULSION SYSTEM FOR THE BEPICOLOMBO MISSION; H. L. Gray, Astrium Ltd, Portsmouth, Hants, PO3 5PU, UK, O. Sutherland, European Space Agency, Noordwijk, 2200AG, The Netherlands

2013-115: GEOMETRIC EFFECTS ON THE ACCELERATION MECHANISMA IN APPLIED-FIELD MAGNETOPLASMADYNAMIC THRUSTERS; Meng-Di Kong and Hai-Bin Tang, Beihang University, Beijing, 100191, China

2013-119: REAL-TIME BORON NITRIDE EROSION MEASUREMENTS OF THE HIVHAC THRUSTER VIA CAVITY RING-DOWN SPECTROSCOPY; Brian C. Lee and Azer P. Yalin, Colorado State University, Fort Collins, CO, 80523, USA, Alec Gallimore, University of Michigan, Ann Arbor, MI, 48109, USA, Wensheng Huang and Hani Kamhawi, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-120: EMI TESTS OF THE HEMP THRUSTER PROPULSION SYSTEM; Edward J. Beiting, William A. Cox, Kevin D. Diamant, Jason A. Young, and Rostislav Spektor, The Aerospace Corporation, Los Angeles, CA 90009, USA, Stefan Weis and Benjamin van Reijen, Thales Electronic Systems GmbH, 89077 Ulm, Germany, Klaus Ruf, Deutsches Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR), D-53227 Bonn, Germany

2013-121: STATUS OF NASA’S EVOLUTIONARY XENON THRUSTER (NEXT) LONG-DURATION TEST AS OF 50,000 H AND 900 KG THROUGHOUT; Rohit Shastry, Daniel A. Herman, George C. Soulas, and Michael J. Patterson, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-122: LANGMUIR PROBE MEASUREMENTS WITHIN THE DISCHARGE CHANNEL OF THE 20-KW NASA-300M AND NASA-300MS HALL THRUSTERS; Rohit Shastry, Wensheng Huang, Thomas W. Haag, and Hani Kamhawi, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-123: AN EXPERIMENTAL STUDY OF PLASMA DETACHMENT FROM A MAGNETIC NOZZLE IN THE PLUME OF THE VASIMR ENGINE; Christopher S. Olsen, Maxwell G. Ballenger, Mark D. Carter, Franklin R. Chang DÃaz, Matthew Giambusso, Timothy W. Glover, Andrew V. Ilin, and Jared P. Squire, Ad Astra Rocket Company, Webster, TX, 77598, USA; Benjamin W. Longmier, University of Michigan, Department of Aerospace Engineering, Ann Arbor, Michigan, 48109, USA; Edgar A. Bering III, University of Houston, Department of Physics and ECE, Houston, Texas, 77204, USA; and Paul A. Cloutier, Rice University, Department of Physics and Astronomy, Houston, Texas, 77005, USA

2013-124: SOLAR ELECTRIC PROPULSION FOR DISCOVERY CLASS MISSIONS; David Y. Oh, John Steven Snyder, Dan M. Goebel, Richard R. Hofer, Damon F. Landau, and Thomas M. Randolph, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109, USA

2013-125: PLASMA TRANSPORT IN A CONVERGING MAGNETIC FIELD WITH APPLICATIONS TO HELICON PLASMA THRUSTERS; Justin M. Little and Edgar Y. Choueiri, Princeton University, Princeton, New Jersey, 08450, USA

2013-126: STRATEGY OF MULTISCALE MODELLING FOR COMBINED THRUSTER-PLUME MODELS; O. Kalentev, J. Duras, K. F. LÃ¼skow, K. Matyash, and R. Schneider, Ernst-Moritz-Arndt, UniversitÃ¤t Greifswald, D-17489, Germany

2013-127: DESIGN AND FABRICATION OF THE THRUSTER HEADS FOR THE MICROTHRUST MEMS ELECTROSPRAY PROPULSION SYSTEM; Simon Dandavino, Caglar Ataman, Subha Chakraborty, and Herbert Shea, Ecole Polytechnique Federale de Lausanne (EPEL), Neuchatel, 2000, Switzerland, Charles Ryan and John Stark, Queen Mary University London, London, E1 4NS, United Kingdom

2013-128: CONCEPTS FOR MICRO-THRUSTERS BASED ON SOLID STATE ION CONDUCTORS; Niklas Wolf and Stefan Kolling, THM University of Applied Sciences, Wiesenstrasse 14, DE-35390 Giessen, Germany; JÃ¼rgen Janek, Institute of Physical Chemistry, Justus Liebig University, Heinrich-Buff-Ring 58, DE-35392 Giessen, Germany

2013-129: THRUST MEASUREMENTS ON THE T6 HOLLOW CATHODE THRUSTER USING DIRECT THRUST BALANCES; D. Frollani, University of Southampton, Southampton, SO17 1BJ, UK, M. Coletti, Mars Space Ltd, Southampton, SO14 5FE, UK, and S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, UK

2013-130: EXB PROBE INVESTIGATION OF THE PEGASES THRUSTER ION BEAM IN XE AND SF6; D. Gerst, D. Renaud, and S. Mazouffre, ICARE – CNRS, 45071 Orleans, France, P. Chabert and A. Aanesland, LPP, Ecole Polytechnique, Palaiseau, France

2013-133: BEPICOLOMBO ELECTRIC PROPULSION THRUSTER AND HIGH POWER ELECTRONICS COUPLING TEST PERFORMANCES; Stephen D. Clark and Mark S. Hutchins, QinetiQ, Cody Technology Park, Farnborough, GU14 0LX, UK, Ismat Rudwan and Neil C. Wallace, Mars-Space Ltd, Southampton, Hampshire, SO14 5FE, UK, Javier Palencia, EADS Astrium CRISA, C/. Tores Quevedo, 9(P.T.M.), 28760 Tres Cantos, Madrid, Spain, Howard Gray, Astrium, Anchorage Road, Portsmouth, Hampshire P03 5PU, UK

2013-137: PRELIMINARY CHARACTERIZATION OF A LAB6 HOLLOW CATHODE FOR LOW-POWER HALL EFFECT THRUSTERS; R. Albertoni and M. Andrenucci, Alta SpA, Ospedaletto, Pisa, 56121, Italy; D. Pedrini and F. Paganucci, University of Pisa, Pisa, 56126, Italy

2013-139: 2D FLUID MODEL OF A MAGNETIZED PLASMA IN A CLOSED CHAMBER; P.-Q. Elias, ONERA – the French Aerospace Lab, Palaiseau, 91123, France

2013-140: HT100D PERFORMANCE EVALUATION AND ENDURANCE TEST RESULTS; Ducci C., Oslyak S., Dignani D., Albertoni R., and Andrenucci M., Alta SpA, Pisa 56121, Italy

2013-141: INVESTIGATION OF THE EMISSION BEHAVIOR OF MINIATURIZED SU-8 BASED COLLOID EMITTERS; K. Huhn, M. Piechotka, T. Henning, and P. J. Klar, Institute of Experimental Physics I, Justus Liebig University, DE-35392 Giessen, Germany

2013-142: NUMERICAL SIMULATIONS OF THE PARTIALLY-IONIZED GAS IN A 100-A LAB6 HOLLOW CATHODE; Ioannis G. Mikellides, Dan M. Goebel, Benjamin A. Jorns, James E. Polk, and Pablo Guerrero, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 91109

2013-143: AZIMUTHAL SPOKE PROPAGATION IN HALL EFFECT THRUSTERS; Michael J. Sekerak, Benjamin W. Longmier, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, Daniel L. Brown, U.S. Air Force Research Laboratory, Edwards Air Force Base, California 93524, Richard R. Hofer and James E. Polk, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-144: SGEO ELECTRIC PROPULSION SUBSYSTEM DEVELOPMENT STATUS AND FUTURE OPPORTUNITIES; Marco De Tata, Pierre-Etienne Frigot, Stefan Beekmans, Hendrik Lubberstedt, and Dieter Birrecl, OHB System AG, Bremen, 28359, Germany, Alain Demaire, Peter Rathsman, and Ekaterina Rezugina, OHB Sweden AB, Solna, SE-171 04, Sweden, Niccola Kutufa, ESA-ESTEC, Noordwijk, The Netherlands

2013-145: MAGNETOHYDRODYNAMICS AND PARTICLE-IN-CELL CODES SIMULATION OF PLASMA PROCESSES IN MICRO HEMP-THRUSTERS; Tim Brandt, Frank Jensen, Rodion Groll, and Claus Braxmaier, DLR, Institute of Space Systems, Robert-Hooke Str. 7, 28359 Bremen, Germany, ZARM, University of Bremen, Am Fallturm, 28359 Bremen Germany, Ulrich Johann and Andreas Keller, Astrium GmbH, Claude-Dornierstrabe 1, 88090 Immenstaad, Germany, Justus-Liebig-University Gieben, I. Physikalisches Institut

2013-146: EXPERIMENTAL PROGRESS TOWARDS THE MICROTHRUST EMEMS ELECTROSPRAY ELECTRIC PROPULSION SYSTEM; C. Ryan, A Daykin-Iliopoulos, and J. Stark, Queen Mary University of London, London, E1 4NS, United Kingdom; A. Z. Salaverri, E. Vargas and P. Rangsten, SSC NanoSpace, Uppsala Science Park, SE-751 83, Uppsala, Sweden; S. Dandavino, C. Ataman, S. Chakraborty, D. Courtney, and H. Shea, Ecole Polytechnique FÃ©rÃ©rale de Lausanne (EPFL), Neuchatel, 2000, Switzerland

2013-147: INVESTIGATIONS ON THE FLOWING PULSED PLASMA OF A 20J PULSED PLASMA THRUSTER; Zun Zhang and Haibin Tang, Beihang University, Beijing, 100191, China

2013-148: PHYSICS OF HALL-EFFECT DISCHARGE BY PARTICLE; F. Taccogna, P. Minelli, and N. Oudini, Istituto di Metodologie Inorganiche e di Plasmi – CNR, via Amendola 122/D, 70126 Bari, Italy

2013-149: VASIMR SPACEFLIGHT ENGINE SYSTEM MASS STUDY AND SCALING WITH POWER; Jared P. Squire, Mark D. Carter, Franklin R. Chang Diaz, Matthew Giambusso, Timothy W. Glover, Andrew V. Ilin, Jorge Oguilve-Araya, and Christopher S. Olsen, Ad Astra Rocket Company, Webster, Texas 77598, USA, Edgar A. Bering III, University of Houston, Houston, Texas 77204, USA, and Benjamin W. Longmier, University of Michigan, Ann Arbor, MI 48109, USA

2013-150: MODELING MAGNETIC NOZZLE EFFECTS IN DIFFERENT PLASMA RADII WITH AN AXISYMMETRIC PARTICLE-IN-CELL METHOD; Min Li and Hai-bin Tang, Beihang University, Beijing, 100191, China

2013-153: LOW POWER RADIO-FREQUENCY PLASMA THRUSTER DEVELOPMENT AND TESTING; F. Trezzolani, A. Lucca Fabris, and D. Pavarin, University of Padova, Italy, A. Selmo, RESIA, Albaredo d’Adige, Italy, A. I. Tsaglov, A. V. Loyan, and O. P. Rubalov, National Aerospace University ‘Kharkiv Aviation Institute (KhAI)’, Ukraine, M. Manente, HIT09 s.r.l., Padova, Italy

2013-155: THRUST BALANCE CHARACTERIZATION OF A 200W QUAD CONFINEMENT THRUSTER FOR HIGH THRUST REGIMES; Aaron Knoll, Dimitrios Lamprou, and Vaios Lappas, University of Surrey, Guildford, Surrey, GU2 7XH, United Kingdom; Mark Pollard, Surrey Satellite Technology Ltd., Stephenson Road, Surrey Research Park, Guildford, GU2 7YE, United Kingdom; Paolo Bianco, Astrium Ltd., Anchorage Road, Portsmough, Hampshire, PO3 5PU, United Kingdom

2013-157: THE IMPACT OF BACK-SPUTTERED CARBON ON THE ACCELERATOR GRID WEAR RATES OF THE NEXT AND NSTAR ION THRUSTERS; George C. Soulas, NASA Glenn Research Center, Cleveland, OH, 44135, USA

2013-158: CHARACTERIZATION OF ERODED BORON ATOMS IN THE PLUME OF A HALL THRUSTER; Horatiu C. Dragnea and Iain D. Boyd, University of Michigan, Ann Arbor, MI, 48109, USA, Brian C. Lee and Azer P. Yalin, Colorado State University, For Collins, CO, 80523, USA

2013-159: PLASMA ADIABATICITY IN A DIVERGING MAGNETIC NOZZLE; J. P. Sheehan and Benjamin W. Longmier, University of Michigan, Ann Arbor, MI, 48103, USA; Edgar A. Bering, University of Houston, Houston, TX, 77204, USA; Christopher S. Olsen, Jared P. Squire, Mark D. Carter, Franklin R. Chang DÃaz, Timothy W. Glover, and Andrew V. Ilin, Ad Astra Rocket Company, Webster, TX, 77598, USA; Leonard D. Cassady, Jacobs Engineering, Bingham Farms, MI, 48025, USA

2013-160: EXPERIMENTAL INVESTIGATION OF THRUST CHARACTERISTICS OF MAGNETOPLASMA SAIL; Yuya Oshio, Kazuma Ueno, and Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, kanagawa, 252-5210, Japan

2013-161: THE RELIABILITY EVALUATION OF LHC-5 HOLLOW CATHODE HEATER; Jia Yanhui, Guo Ning, Chen Juanjuan, Zhang Tianping, Yang Wei, Liang Kai, Sun Yunkui, Geng Hai, and Tian Huabing, Lanzhou Institute of Physics, Lanzhou, GanSu,730000, China

2013-162: PIC/MCC SIMULATION COMPUTATIONAL MODELING OF A ION THRUSTER DISCHARGE CHAMBER; Chen Juanjuan, Zhang Tianping, Liu Mingzheng, and Jia Yanhui, Lanzhou Institute of Physics, Lanzhou 73000, China

2013-163: HELICON PLASMA THRUSTER EXPERIMENT CONTROLLING CROSS-FIELD DIFFUSION WITHIN A MAGNETIC NOZZLE; K. Takahashi, Department of Electrical Engineering, Tohoku University, Sendai, 980-8579, Japan, C. Charles and R. W. Bowell, Space Plasma Power and Propulsion Laboratory, Research School of Physics and Engineering, The Australian National University, Canberra ACT 0200, Australia, A. Ando, Department of Electrical Engineering, Tohoku University, Sendai, 980-8579, Japan

2013-164: PPTCUP LIFETIME TEST RESULTS; S. Ciaralli, University of Southampton, Southampton, UK, SO17 1BJ, M. Coletti and F. Guarducci, Mars Space Ltd. Southampton, UK, SO14 5FE, and S. B. Gabriel, University of Southampton, Southampton, UK, SO17 1BJ

2013-165: Âµ-PPTS DIAGNOSTICS: A HIGH ACCURACY IMPULSIVE THRUST BALANCE; S. Ciaralli, University of Southampton, Southampton, UK, SO17 1BJ, M. Coletti, Mars Space Ltd, Southampton, UK, SO14 5FE, and S. B. Gabriel, University of Southampton, Southampton, UK, SO17 1BJ

2013-166: STUDY ON THE INFECTIONS OF MAGNETIC FIELD IN LHT-100 THRUSTER; Jianfei Long, Tianping Zhang, and Mingming Sun, Lanzhou Institute of Physics, Lanzhou, GanSu, 730000, China

2013-167: NUMERICAL INVESTIGATION OF THE INFLUENCE OF AMBIPOLAR ELECTRIC FIELD ON MAGNETIC NOZZLE DETACHMENT; Yujie Xu and Haibin Tang, School of Astronautics, Beihang Unversity, Beijing 100191, China

2013-171: PARTICLE-IN-CELL SIMULATIONS FOR A VARIABLE MAGNET LENGTH CUSPED-FIELD THRUSTER; Yinjian Zhao, Hui Liu, Daren Yu, and Chengyu Ma, Institute of Advanced Power, Harbin Institute of Technology, Harbin, Heilongjiang Province, 150001, China

2013-172: LIFETIME ASSESSMENT OF HALL THRUSTER; Hu Yanlin, Chen Jian, Mao Wei, Shen Yan, and Chen Jun, Beijing Institute of Control Engineering, Beijing, 100190, China

2013-175: GRADIENT DRIFT INSTABILITY IN HALL PLASMA DEVICES; W. Frias and A.I. Smolyakov, University of Saskatchewan, Saskatoon, SK, S7N 5E2, Canada; Y. Raitses and I. D. Kaganovich, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2013-176: DRIVING LOW FREQUENCY AZIMUTHAL MODE IN CYLINDRICAL HALL THRUSTER WITH A SEGMENTED ANODE; Yuan Shi, Scott Keller, Yevgeny Raitses, and Ahmed Diallo, Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543, USA

2013-177: INFLUENCE OF CATHODE SHAPE ON VACUUM ARC THRUSTER PERFORMANCE AND OPERATION; Jonathan Lun, University of the Witwatersrand, Johannesburg, Gauteng, 2000, South Africa, South African National Space Agency: Space Science, Hermanus, Western Cape, 7200, South Africa, Craig Law, University of Witwatersrand, Johannesburg, Gauteng, 2000, South Africa

2013-178: DEVELOPMENT OF A HALL THRUSTER FULLY KINETIC SIMULATION MODEL USING ARTIFICAL ELECTRON MASS; Shinatora Cho, Japan Aerospace Exploration Agency, Tokyo, 182-8522, Japan, Kimmiya Komurasaki and Yoshihiro Arakawa, The University of Tokyo, Tokyo, 113-8656, Japan

2013-179: 6-DOF FLIGHT DYNAMICS OF LASER-BOOSTED VEHICLE DRIVEN BY BLAST WAVE; Masayuki Takahashi and Naofumi Ohnishu, Tohoku University, Sendai, Miyagi, 980-8579, Japan

2013-181: IMPULSE VECTOR CHARACTERISTICS OF A LASER ABLATION PROPULSION SYSTEM; Takumi Oyama, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan, Hideyuki Horisawa, Yuji Oigawa, and Keiji Hagiwara

2013-182: NUMERICAL STUDY ON THE OPERATIN LIMITS OF MPD THRUSTERS; Arsad Quraishi and M. Mahendhran, Indian Institute of Technology Madras, Chennai-600036, India, Amit Kumar, Indian Institute of Technology Madras, Chennaii-600036, India

2013-186: THREE-DIMENSIONAL PARTICLE-IN-CELL SIMULATION OF A MINIATURE MICROWAVE DISCHARGE ION THRUSTER Âµ1; Yoshinori Takao, Koji Eriguchi, and Kouichi Ono, Kyoto University, Kyoto, 615-8540, Japan, Yuto Sugita, Shizuoka University, Shizuoka, 422-8529, Japan, Hiroyuki Koizumi and Kimiya Komurasaki, The University of Tokyo, Tokyo, 113-8636, Japan

2013-187: LANGMUIR PROBE MEASUREMENTS OF A MAGNETOPLASMADYNAMIC THRUSTER; Yang Li, Hai-Bin Tang, Zun Zhang, and Yuan Yang, Beihang University, Beijing, 100191, China

2013-188: MEASUREMENT OF THE DIELECTRIC WALL EROSION IN HELICON PLASMA THRUSTERS: AN APPLICATION TO THE VASIMR VX-CR EXPERIMENT; Juan Del Valle, Jose A. Castro, Norberto Arce, Erick Chinchilla, Estaban EcheverrÃa, Daniel Lexama, Carlos MartÃnez, Jorge Oguilve, Allan Rivera, Max RodrÃguez, Juan Valverde, and RÃ³nold Chang DÃaz, Ad Astra Rocket Company, Liberia, Guanacaste, Costa Rica, Christopher S. Olsen, Andrew V. Ilin, Matthew Giambusso, Mark D. Carter, Jared P. Squire, and Franklin R. Chang DÃaz, Ad Astra Rocket Company, Webster, Texas, USA

2013-190: A SIMPLE COLLISIONAL-RADIATIVE MODEL APPLICABLE TO ARGON ARCJET; Su-Rong Sun and Hai-Xing Wang, School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China

2013-191: EMITTANCE MEASUREMENT SETUP FACILITATING PLASMA DIAGNOSTIC OF ION THRUSTERS; K. Holste, S. Schippers, and A. MÃ¼ller, Justus-Liebig UniversitÃ¤t GieÃŸen, 35392, Germany, P. SpÃ¤dtke, GSI Darmstadt, PlanckstraÃŸe 1, 64291 Darmstadt, Germany, M. Smirnova, Justus-Liebig UniversitÃ¤t GieÃŸen, I. Physikalisches Institut, Heinrich-Buff-Ring 16, 35392 GieÃŸen, Germany, D. Feili, Astronautics Research Group, Southampton S017 1BJ, United Kingdom

2013-192: CREW WASTE WATER ELECTRIC PROPULSION SYSTEM DEVELOPMENT AND SMALL SATELLITE DEPLOYMENT FROM ISS WITH ITS ARCJET THRUSTER; Yuichiro Nogawa, Earth-Track Corporation, Tokyo, Japan; Hirokazu Tahara, Osaka Institute of Technology, Osaka, Japan, and Akira Tsuchida, Earth-Track Corporation, Tokyo, Japan

2013-193: CHARACTERISTICS OF HIGH-REPETITION RATE OPERATION OF A LASER-ASSISTED PULSED PLASMA THRUSTER; Mizuki Karima, Hideyuki Horisawa, and Yuki Oigawa, Dept. Aeronautics and Astronautics, Tokai University, Hiratsuka, Kanagawa, 259-1292, Japan

2013-194: NUMERICAL SIMULATIONS OF A MINIATURE MICROWAVE ION THRUSTER; Pierre-Yves C. R. Taunay, Sven G. BilÃ©n, and Michael M. Micci, The Pennsylvania State University University Park, PA 16802, USA

2013-196: EXAMINATION OF THE EXTERNAL MAGNETIC FIELD GENERATED BY A RADIO-FREQUENCY ION THRUSTER (RIT); Timo Baruth and Rainer Thueringer, Technische Hochschule Mittelhessen University of Applied Sciences, Giessen, 35390, Germany

2013-198: PPT DEVELOPMENT FOR NANOSATELLITES APPLICATIONS: EXPERIMENTAL RESULTS; M. Coletti, Mars Space Ltd, Southampton, SO14 5FE, UK, S. Ciaralli and S. B. Gabriel, University of Southampton, Southampton, SO17 1BJ, UK

2013-199: A PLAN TO STUDY THE RADIATED EMISSIONS FROM A VASIMR ENGINE EXHAUST PLUME; Matthew Giambusso, Edgar A. Bering, III, Gregg A. Edeen, University of Houston, Houston, Texas, 77294, USA, Mark D. Carter, Christopher S. Olsen, and Jared P. Squire, Ad Astra Rocket Company, Webster, Texas, 77598, USA

2013-201: MAGNETICALLY SHIELDED MINIATURE HALL THRUSTER: DEVELOPMENT AND INITIAL TESTING; Ryan W. Conversano, University of California Los Angeles, Los Angeles, CA, 90095, USA, Dan M. Goebel and Richard R. Hofer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, 991109, Taylor S. Matlock and Richard E. Wirz, University of California Los Angeles, Los Angeles, CA, 90095, USA

2013-202: VASIMR VX-CR EXPERIMENT: STATUS, DIAGNOSTICS AND PLASMA PLUME CHARACTERIZATION; Jose A. Castro Nieto, Juan Del Valle, Carlos MartÃnez, Allan Rivera, and Jorge Oguilve, Ad Astra Rocket Company, Liberia, Guanacaste, Costa Rica, Christopher S. Olsen, Matthew Giambusso, Mark d. Carter, Jared P. Squire, and Franklin R. Chang DÃaz, Ad Astra Rocket Company, Webster, Texas, USA

2013-205: RESONANT MODE TRANSITION IN THE RF-CONTROLLED HOLLOW CATHODE; Matthew L. Plasek, Christopher J. Wordingham, Edgar Y. Choueiri, Princeton University, Princeton, NJ, 08544, USA

2013-209: EXPERIMENT RESEARCH ON A VARIABLE MAGNET LENGTH CUSPED FIELD THRUSTER; Chengyu Ma, Hui Liu, Daren Yu, Yinjian Zhao, Pengbo Chen, and Guoshun Sun, Institute of Advanced Power, Harbin Institute of Technology, Harbin, Heilongjiang Province, 150001, China

2013-210: NUMERICAL STUDY OF LISSAJOUS ACCELERATION FOR ELECTRODELSS PLASMA THRUSTER; Ryosuke Nomura and Naofumi Ohnishi, Tohoku University, Sendai, Miyagi, 980-8579, Japan; Takahiro Nakamura and Hiroyuki Nishida, Tokyo University of Agriculture and Technology, Koganei, Tokyo, 184-8588, Japan

2013-211: THE 250MN THRUST BALANCE FOR THE DLR GOETTINGEN EP TEST FACILITY; Andreas Neumann and Julian Sinske, German Aerospace Center DLR, Goettingen, Germany and Hans-Peter Harmann, AST Advanced Space Technologies GmbH, Stuhr, Germany

2013-212: TWO-DIMENSIONAL SIMULATIONS OF COHERENT FLUCTUATION-DRIVEN TRANSPORT IN A HALL THRUSTER; Cheryl M. Lam and Mark A. Cappelli, Stanfod Plasma Physics Laboratory, Stanford University, Stanford, CA 94305, USA; Eduardo Fernandez, Department of Mathematics and Physics, Eckerd College, St. Petersburg, FL, 33711, USA

2013-213: POWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA); Eric Bourguignon, StÃ©phane Fraselle, and Thierry Scalais, Thales Alenia Space Belgium (ETCA), B-6032 Charleroi, Belgium

2013-214: TIME-AVERAGED AND TIME-VARYING PLASMA POTENTIAL IN THE NEAR-FIELD PLUME OF A HALL THRUSTER; A. Petin and S. Mazouffre, ICARE, CNRS, 1c Avenue de la recherchÃ© scientifique, 45071 Orleans, France, K. Dannenmayer, ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, Netherlands, P. Kudrna and M. Tichyu, Charles University, Faculty of Mathematics and Phuysics, Prague, Czech Repulic

2013-216: IMPLEMENTATION OF AN ENTROPY CLOSURE MODEL FOR TWO-DIMENSIONAL HYBRID HALL THRUSTER SIMULATIONS; Eunsun Cha and Mark A. Cappelli, Stanford University, Stanford, CA, 94305, USA, and Eduardo Fernandez, Eckerd College, St. Petersburg, FL, 33711, USA

2013-217: SMALL ELECTRIC PROPULSION PLATFORM FOR ACTIVE SPACE DEBRIS REMOVAL; A. Ruggiero, P. Pergola, and M. Andrenucci, Alta, Pisa, 56100, Italy

2013-219: DEVELOPMENT AND TEST OF XR-150, A NEW HIGH-THRUST 100 W RESISTOJET; A. Passaro, Alta S.p.A., Pisa, 56121, Italy, A. Bulit, ESA-ESTEC, Noordwijk, 2201 AZ, The Netherlands

2013-222: ELECTRIC PROPULSION THRUSTER ASSEMBLY FOR SMALL GEO: END-TO-END TESTING AND FINAL DELIVERY; Olivier Duchemin, Vaitua Leroi, Michael Oberg, and David Le Mehaute, Snecma, Safran Group, Space Engines Division, 27208 Vernon, France, Ramon Perez Vara, IberEspacio, Magallanes 3, 4a Planta, 28015 Madrid, Spain, Alain Demaire, Mikael Bjorklund and Staffan Persson, OHB-Sweden AB, SE-17122 Solna, Sweden, Marco De Tata and Stefan Beekmans, OHB-System AG, 28359 Bremen, Germany, Niccola Kutufa, ESA/ESTEC, Keplerlaan 1, Postbus 299, 2200 AG Noordwijk, The Netherlands

2013-223: MICROWAVE-PLASMA INTERACTION IN A MINIATURE PLASMA ION THRUSTER; Indranuh Dey, Yuji Toyoda, Naoji Yamamoto, and Hideki Nakashima, Department of Advanced Energy Engineering Science, Kyushu University, Kasuga, 816-8580, Japan

2013-224: COMPUTATIONAL MODELING OF A HIGH POWER PLASMA SOURCE FOR MATERIAL INTERACTION EXPERIMENTS; Christopher A. Dodson, Richard E. Wirz, and Taylor S. Matlock, University of California, Los Angeles, CA, 90095

2013-227: ÂµFCU – A MINIATURIZED FLOW CONTROL UNIT FOR XENON; H. –P. Harmann, S. Rothaus, and G. Wanot, AST Advanced Space Technologies GmbH, D-28816 Stuhr, Germany

2013-228: ÂµFCU – RESULTS OF A PREQUALIFICATION TEST CAMPAIGN; S. Rothaus, H. –P. Harmann, and T. Kopp, AST Advanced Space Technologies GmbH, D-28816 Stuhr, Germany

2013-234: EXPERIMENTAL STUDY OF A 1-MW-CLASS QUASI-STEADY-STATE SELF-FIELD MAGNETOPLASMADYNAMIC THRUSTER; Kenji Miyazaki and Syunm Takenaka, Tokai University, Hiratsuka, Kanagawa 259-1292, Japan, Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, kanagawa 252-5210, Japan, Hideyuki Horisawa, Tokai University, Hiratsuka, Kanagawa 259-1292, Japan

2013-235: EXPERIMENTAL INVESTIGATIONS OF COMPONENT DETERMINING CAMILA HALL THRUSTER PERFORMANCE; M. Rubanovich, V. Balabanov, A. Kapulkin, and e. Behar, Asher Space Research Institute, Technion-Israel Institute of Technology, Haifa, 32000, Israel

2013-238: DEVELOPMENT OF A 1 KW CLASS THERMAL ARCJET THRUSTER TALOS; Q. H. Le and G. Herdrich, Institute of Space Systems, University of Stuttgart, Stuttgart, 70569, Germany

2013-239: TIME-DEPENDENT ION VELOCITY DISTRIBUTION: A NOVEL HETERODYNE LASER-INDUCED FLUORESCENCE WITH COUPLED WAVE EXCITATION; A Diallo, Y. Shi, S. Keller, and Y. Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08536, USA, S. Mazouffre, ICARE, CNRS, OrlÃ©ans, France

2013-241: MECHANICAL PROBE AND MODELING EFFORTS FOR EVALUATION OF PLASMA CREATION AND ACCELERATION IN PPT; Tony SchÃ¶nherr, W. Alexander Zach, and Kimiya Komurasaki, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan, Sebastian HÃ¶rner and Yoshihiro Arakawa, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan, Georg Herdrich, University of Stuttgart, Stuttgart, Baden-WÃ¼rttemberg, 70569, Germany

2013-242: DESIGN AND PERFORMANCE EVALUATION OF THRUSTER WITH ANODE LAYER UT-58 FOR HIGH-POWER APPLICATION; Tony SchÃ¶nherr, Rei Kawashima, Hiroyuki Koizumi, and Kimiya Komurasaki, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan, Daiki Fujita and Yuki Ito, The University of Tokyo, Kashiwa, Chiba, 277-8561, Japan

2013-243: APPLICATION OF THE HOLLOW CATHODE TO DC ARCJET; Masahiro Kinoshita, The University of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan, Daisuke Nakata, Muroran Institute of Technology, Hokkaido, 050-8585, Japan, Kiyoshi Kinefuchi, Japan Aerospace Exploration Agency, Tsukuba, Ibaragi, 305-8505, Japan, Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2013-244: DEVELOPMENTS OF ROBUST ANODE-LAYER INTELLILGENT THRUSTER FOR JAPAN IN-SPACE PROPULSION SYSTEM; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan, Takeshi Miyasaka, Gifu University, Gifu, Gifu, 501-1193, Japan, Kimiya Komurasaki, Hiroyuki Koizumi, and Tony Schonherr, The University of Tokyo, Tokyo, Tokyo, 113-8656, Japan, Hirokazu Tahara, Osaka Institute of Technology, Osaka, Japan, Haruki Takegahara and Junichiro Aoyagi, Tokyo Metropolitan University, Tokyo, Japan, Masakatsu Nakano, Tokyo Metropolitan College of Industrial Technology, Tokyo, Japan, Ikkoh Funaki, Hiroki Watanabe, and Yasushi Ohkawa, Japan Aerospace Exploration Agency, Japan, Akirai Kakami, University of Miyazaki, Miyazaki, Japan, Yoshiyuki Takao, Nishinippon Institute of Technology, Fukuoka, Japan, Shigeru Yokota, Nagoya University, Nagoya, Japan, Toshiyuki Ozaki and Hiroyuki Osuga, Mitsubishi Electric Corporation, Kamakura, Japan

2013-245: PLASMA DIAGNOSTICS IN A MINIATURE MICROWAVE DISCHARGE ION THRUSTER; Yuto Sugita, Shizuoka University, Shizuoka, 432-8561, Japan, Hiroyuki Koizumi, The University of Tokyo, Tokyo, 113-8656, Japan, Ryudo Tsukizaki and Hitoshi Kuninaka, The Institute of Space and Astronautical Science, Sagamihara, 252-5210, Japan, Yoshinori Takao, Kyoto University, Kyoto, 615-8540, Japan, Yoshiki Yamagiwa and Makoto Matsui, Shizuoka University, ,Shizuoka, 432-8561, Japan

2013-246: STEADY-STATE, APPLIED-FIELD, RECTANGULAR MPD THRUSTERS; Shigeru Yokota, Daisuke Ichihara, Hisashi Kataoka, Shota Harada, and Akihiro Sasoh, Nagoya University, Nagoya, Aichi, 464-8603, Japan

2013-247: INFLUENCE OF ELECTRON AND ION THERMODYNAMICS ON THE MAGNETIC NOZZLE PLASMA ESPANSION; Mario Merino and Eduardo Ahedo, Universidad Carlos III de Mardrid, Avda. de la Universidad 30, 28911 LeganÃ©s (Madrid). Spain

2013-248: DEVELOPMENT OF A NOVEL PROCESSING UNIT FOR HALL THRUSTERS; Naoji Yamamoto, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan; Haruki Takegahara, Junichiro Aoyagi, and Kyoichi Kuriki, Tokyo Metropolitan University, 191-0065, Tokyo, Japan; Taichiro Tamida, Mitsubishi Electric Corporation, Hyogo, 661-8661, Japan; and Hiroyuki Osuga, Mitsubishi Electric Corporation, Kamakura, 247-8520, Japan

2013-249: TWO-DIMENSIONAL PARTICLE-IN-CELL MODEL OF THE EXTRACTION REGION OF THE PEGASES ION-ION PLASMA SOURCE; L. Garrigues, G. J. M. Hagelaar, D. Levko, LAPLACE (Laboratoire Plasma et Conversion d’Energie), Universite de Toulouse, UPS, INPT Toulouse, 118, route de Narbonne, F-31062 Toulouse, France, CNRS; LAPLACE; F-31062 Toulouse, France, A. Aanesland, Laboratoire de Physique des Plasmas, CNRS, Ecole Polytechnique, 91128 Palaiseau cedex France

2013-250: DESIGN AND FIRST TEST CAMPAIGN RESULTS WITH A NEW FLEXIBLE MAGNETIC CIRCUIT FOR A HALL THRUSTER; L. Garrigues, LAPLACE (Laboratoire Plasma et Conversion d’Energie), UniversitÃ© de Toulouse, UPS, INPT Toulouse, S. Mazouffre, G. Bourgeois, and J. Vaudolon, ICARE (Institut de Combustion AÃ©rothermique RÃ©activitÃ© et Environnement), C. HÃ©naux, R. Vilamot, A. Rossi, and D. Harribey, CNRS; LAPLACE; F-31062 Toulouse, France, S. Zurbach, Snecma, Safran Group; 27200 Vernon, France

2013-251: EXPERIMENTAL TEST CAMPAIGN OF GAS-FED STEADY STATE APPLIED-FIELD MAGNETOPLASMADYNAMIC THRUSTER SX3; Adam Boxberger and Georg Herdrich, University of Stuttgart, Institute of Space Systems (IRS), 70569 Stuttgart, Pfaffenwaldring 29, Germany

2013-252: A TWO-DIMENSIONAL (AZIMUTHAL-AXIAL) PARTICLE-IN-CELL OF A HALL THRUSTER; L. Garrigues, LAPLACE (Laboratoire Plasma et Conversion d’Energie). UniversitÃ© de Toulouse, UPS, INPT Toulouse, 118 route de Narbonne, F-31062 Toulouse cedex 9, France; P. Coche LAPLACE (Laboratoire Plasma et Conversion d’Energie). UniversitÃ© de Toulouse, UPS, INPT Toulouse, 118 route de Narbonne, F-31062 Toulouse cedex 9, France, CNRS; LAPLACE, F-31062 Toulouse, France

2013-253: THRUST CHARACTERISTICS OF HELICON PLASMA THRUSTERS; S. Tonooka, The Graduate University for Advanced Studies, Sagamihara, Kanagawa, 252-5210, Japan, S. Iwabuchi, T. Nakamura, S. Shinohara, and H. Nishida, Tokyo University of Agriculture and Technology, Koganei, Tokyo, 184-8588, Japan

2013-254: EFFECTS OF ELECTRIC CHARGE IN CAPACITORS ON PULSED PLASMA THRUSTER PERFORMANCE WITH EXTERNAL MAGNETIC FIELD, Shinya Mori, Takahiro Shindo, Keisuke Tajiri, Yuya Tamugi, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2013-255: PULSED PLASMA THRUSTER ENDURANCE OPERATION STRESS TESTING IN IRS; M. Lau and G. Herdrich, University of Stuttgart, Institute of Space Systems, Stuttgert, Baden-WÃ¼rttemberg. 70659, USA

2013-257: ELECTRIC PROPULSION IN GERMANY: SYSTEM ACTIVITIES TODAY, INSTITUTIONS INVOLVED, CHALLENGES COMING UP; Norbert PÃ¼ttmann and Klaus Ruf, German Aerospace center (DLR) – Space Administration, Koenigswinterer Str. 522-524, D-53227 Bonn, Germany

2013-258: MINIATURIZED HV POWER SUPPLLY; Richard Visee, Martin de Jong, and Jan Timmerman, SystematIC design b.v., Delft, 2623CR, the Netherlands

2013-259: THE PEGASES GRIDDED ION-ION THRUSTER PERFORMANCE AND PREDICTIONS; A. Aanesland, D. Rafalskyi, J. Bredin, P. Grondein, N. Oudini, and P. Chabert, Laboratoire de Physique des Plasmas (LPP), CNRS-Ecole Polytechnique, 91128 Palaiseau Cedex, France, L. Garrigues and G. Hagelaar, LAboratoire PLAsma et Conversion d’Energie-LAPLACE, 31062 Toulouse Cedex 9, France

2013-260: CHARACTERISTICS OF A LASER-ELECTROSTATIC HYBRID PROPULSION SYSTEM; Tatsuro Sakai, Akihiro Osamura, and Hideyuki Horisawa, Tokai University, hiratuka, Kanagawa, 259-1292, Japan

2013-261: THE SMALL-SCALE HIGH-FREQUENCY EXB INSTABILITY AND ITS LINKS TO OBSERVED FEATURES OF THE HALL THRUSTER DISCHARGE; ICARE, Electric Propulsion Team, UPR 3021, CNRS, OrlÃ©ans, France, Cyrille Honore and Dominique GrÃ©sillon, LPP, Ecole Polytechnique, UMR 7648 CNRS, Palaiseau, France, Anne HÃ©ron, CPHT, Ecole Polytechnique, UMR 7644 CNRS, Palaiseau, France, Nicolas Lemoine and Jordan Cavalier, IJL UMR 7198 CNRS, Nancy, France

2013-262: MHD AND THERMAL SIMULATIONS OF A RADIATION COOLED SELF-FIELD MPD THRUSTER; Akira Kawasaki, Tokyo Institute of Technology, Yokohama, Kanagawa, 252-8502, Japan, Kenichi Kubota, Japan Aerospace Exploration Agency, Chofu, Tokyo, 182-8522, Japan, Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan, Yoshihiro Okuno, Tokyo Institute of Technology, Tokohama, Kanagawa, 226-8502, Japan

2013-263: CONCEPTUAL DESIGN OF HIGH EFFICIENCY BREECH-FED ABLATIVE PPT IN TOKYO METROPOLITAN UNIVERSITY; Takahiro Shindo, Shinya Mori, Keisuke Tajiri, Yuya Tamugi, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metropolitan University, Hino, Tokyo, 191-0065, Japan

2013-264: DEVELOPMENT OF VACUUM ARC THRUSTER FOR NANO SATELLITE; Shingo Fuchikami, Masayoshi Nakamoto, Kazuhiro Toyoda, and Mengu Cho, Kyushu Institute of Technology, Kitakyushu, Fukuoka, Japan

2013-265: IMPROVEMENT OF LASER ELECTROMAGNETIC HYBRID THRUSTER; Yuji Oigawa and Hideyuki Horisawa, Tokai University, Kitakaname, Hiratsuka City, Kanagawa, 259-1292, Ikkoh Funaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan

2013-266: LOW FREQUENCY OSCILLATION ANALYSIS OF A HALL THRUSTER USING A ONE-DIMENSIONAL HYBRID-DIRECT KINETIC SIMULATION; Kentaro Hara and Iain D. Boyd, University of Michigan, Ann Arbor, MI 48109-2140

2013-268: SENSITIVITY ANALYSIS ON ION ACCELERATION GRID EROSION IN ION THRUSTERS; Hiroki Watanabe, Ikkoh Funaki, and Ryoji Takaki, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan, Masakatsu Nakano, Tokyo Metropolitan College of Industrial Technology, Arakawa-ku, Tokyo, 116-0003, Japan, Yoshihiro Kajimura, Akashi National College of Technology, Akashi, Hyogo, 674-8501, Japan

2013-269: PARAMETRIC STUDY OF HEMP-THRUSTER DOWNSCALING TO ÂµN THRUST LEVELS; Andreas Keller, Franz Georg Hey, Dennis, Weise, and Ulrich Johann, Astrium GmbH – Satellites, Friedrichshafen, Germany, Justus-Liebig-University Gieben, I. Physikalisches Institut, Germany, Peter Kohler, Justus-Liebig-University Gieben, I. Physikalisches Institut, Germany, Marcel Berger, Astrium GmbH – Space Transportation, Bremen, Germany, Claus Braxmaier, Unviersity of Bremen, ZARM Center for Applied Space Technology and Microgravity, DLR German Aerospance Center, Institute of Space Systsems, Bremen, Davar Feilli, University of Southampton, Faculty of Engineering and the Environment, United Kingdom

2013-270: PLASMA DIANOSTICS OF THE Âµ10 ECR ION THRUSTER USING OPTICAL FIBER PROBES; Ryudo Tsukizaki, Japan Aerospace Exploration Agency, Sagmihara, Kanagawa, 252-5210, Japan, Toshiyuki Ise and Hiroyuki Koizumi, The Universrity of Tokyo, Bunkyo-ku, Tokyo, 113-8656, Japan, Hiroyoshi Togo, Nippon Telegraph and Telephone Corporation, Atsugi, Kanagawa, 243-0198, Japan, and Kazutaka Nishiyama and Hitoshi Kuninaka, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 252-5210, Japan

2013-272: ELECTRON TEMPERATURE AND PLASMA POTENTIAL MEASUREMENTS IN A RADIAL PLASMA SOURCE; Gennady Makrinich, D. Zoler, and A. Fructhtman, H.I.T. – Holon Institute of Technology, Holon, 58102, Israel

2013-273: SPACE MISSIONS POTENTIALLY BENEFIT OR ENABLED BY THE PROSPECTIVE USE OF HELICON PLASMA THRUSTERS; M. Ruiz, I. urdampilleta, and J. M. del Cura, SENER IngenierÃa y Sistemas, Tres Cantos, Madrid, Spain, E. Ahedo, Universidad Carlos III de Madrid, Madrid, Spain, J. Navarro-CavallÃ©, Universidad PolitÃ©cnica de Madrid, Madrid, Spain

2013-274: PROGRESS IN TESTING OF QM AND FM HEMP THRUSTER MODULES; A. Lazurenko, A. Genovese, B. van Reijen, J. Haderspeck, S. Weis, and P. Holtmann, Thales Electronic Systems GmbH, Ulm, 89077, Germany, M. Schirra, Kempten University of Applied Sciences, K. Ruf and N. PÃ¼ttmann, Deutsches Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR) – Raumfahrtmanagement, Bonn, 53227, Germany

2013-275 a: ESA PROPULSION LABORATORY; A Bulit and J. Gonzalez Del Amo, ESA/ESTEC, Keplerlaan1, 2200 AG Noordwijk ZH, The Netherlands

2013-276: CONDUCTIN WALL HALL THRUSTERS; Dan M. Goebel, Richard R. Hofer, Ioannis G. Mikellides, Ira Katz, James E. Polk, and Brandon Dotson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109

2013-275 b: DEVELOPMENT OF A HIGHLY PRECISE MICRO-NEWTON THRUST BALANCE; Franz Georg Hey, Astrium GmgH – Satellites, Friedrichshafen, Germany, Technische UniversitÃ¤t Dresden, Germany, Andreas Keller, Astrium GmbH – Satellites, Friedrichshafen, Germany, Justus-Liebig, University GieÃŸen, I. Physikalisches Institut, Germany, Dirk Papendorf, Astrium GmbH – Satellites, Friedrichshafen, Germany, Claus Braxmaier, University of Bremen, ZARM Center of Applied Space Technology and Microgravity, DLR German Aerospace Center, Institute of Space Systems, Bremen, Martin Tajmar, Technische UniversitÃ¤t Dresden, Germany, Ulirch Johann and Dennis Weise, Astrium GmbH – Satellites, Friedrichshafen, Germany

2013-278: A DIRECT DRIVE SYSTEM APPLICATION FOR HALL EFFECT THRUSTERS; Alessio Pampaloni and Mirko Trisolini, University of Pisa, Pisa, 56122, Italy; Tommaso Misuri, Alta S.p.A., Ospedaletto, Pisa, 56121, Italy; Mariano Andrenucci, Alta S.p.A., Ospedaletto, Pisa, 56121, Italy

2013-279: HT5K HALL THRUSTER TO IMPROVE SMALL LAUNCHER CAPABILITIES; Tommaso Misuri Pierpaolo Pergola, Alta S.p.A. Ospedaletto, Pisa, 56121, Italy, Mariano Andrenucci, Alta S.p.A. Ospedaletto, Pisa, 56121, Italy

2013-280: VERIFICATION OF A FLOW CONTROL UNIT WITH GAS PURIFIER AND INTEGRATION INTO THE HEMP THRUSTER MODULE; J. Haderspeck, S. Weis, B. van Reijen, A. Lazurenko, A. Genovese, and P. Holtmann, Thales Electronic Systems GmbH, Ulm, 89077, Germany, K. Ruf and N. PÃ¼ttmann, Deutsches Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany, M. schirra, Hochschule fÃ¼r angewandte Wissenschaften, Kempten, 87435, Germany, J. Kuiper, MOOG Bradford heerle, 4726 TG, The Netherlands

2013-281: HIGH SPECIFIC IMPULSE SOLUTIONS FOR ORBIT RAISING, ORBIT TOPPING AND STATION KEEPING WITH THE HEMP-T ELECTRIC PROPULSION SYSTEM; B. van Reijen, S. Weis, J. Haderspeck, A. Lazurenko, A. Genovese, and P. Holtmann, Thales Air Systems & Electron Devices GmbH, Ulm, 89077, Germany, M. Schirra, Kempten University of Applied Sciences, K. Ruf and N. PÃ¼ttmann, Deutsches Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany

2013-282: ENVIRONMENTAL AND OPERATIONAL QUALIFICATION OF THE THALES MIXED METAL HOLLOW CATHODE NEUTRALIZER FOR THE HEMP-T BASED ION PROPULSION SYSTEM; B. van Reijen, A. Genovese, A. Lazurenko, S. Weis, J. Haderspeck, and P. Holtmann, Thales Electronic Systems GmbH, Ulm, 89077, Germany, M. Schirra, Hochschule fÃ¼r angewandte Wissenschaften, Kempten, 87435, Germany, K. Ruf and N. PÃ¼ttmann, Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany

2013-283: PERFORMANCE MEASUREMENTS OF A HIGH POWERED QUAD CONFINEMENT THRUSTER; Thomas Harle, Aaron Knoll, and Vaios J. Lappas, Unversity of Surrey, Guildford, GU2 7XH, United Kingdom; Paolo Bianco, Astrium Ltd, Anchorage Road, Portsmouth, PO3 5PU, United Kingdom

2013-284: HIGH PRECISION THRUST VECTOR DETERMINATION THROUGH FULL HEMISPHERICAL RPA MEASUREMENTS ASSISTED BY ANGULAR MAPPING OF ION ENERGY CHARGE STATE DISTRIBUTION; B. van Reijen, S. Weis, A. Lazurenko, J. Haderspeck, A. Genovese, and P. Holtmann, Thales Electronic Sytstems GmbH, Ulm, 89077, Germany; K. Ruf and N. PÃ¼ttmann, Deutsches Zentrum fÃ¼r Luft-und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, Bonn, 53227, Germany

2013-286: QUASINEUTRAL PIC ELECTRON GUIDING CENTER MODELING IN THE PRESENCE OF SLOW CROSS-FIELD ELECTRON TRANSPORT IN A HALL THRUSTER; Dariusz Danitko and Serge Barral, Institute of Plasma Physics and Laser Microfusion, Hery 23, 01-497 Warsaw, Poland, StÃ©phan Zurback, Snecma, Safran Group, 27208 Vernon, France

2013-289: EXPERIMENTAL DISCHARGE CHARACTERIZATION AND SCALING OF IEC PLASMA DEVICES; Constanze Syring and Greg Herdrich, University of Stuttgart, Stuttgart, 70567, Germany

2013-291: DEVELOPMENT STATUS OF AN OPEN CAPILLARY PULSED PLASMA THRUSTER WITH NON-VOLATILE LIQUID PROPELLANT; S. Barral and J. Kurzyna, Institute of Plasma Physics and Laser Microfusion, 01497 Warsaw, Poland, E. RemÃrez and R. Martin, JMP Ingenieros, 26371 SotÃ©s (la Rioja), Spain, S. Bottinelli and Y. Mabillard, Mecartex, 6933 Muzzano, Switzerland, A. ZaldÃvar and P. Rangsten, NanoSpace AB, Uppsala Science Park, SE-751 83 Uppsala, Sweden, and C. R. Koppel, KopooS Consulting Ind., 75008 Paris, France

2013-292: DEVELOPMENT OF LONG-LIFE LIGHTWEIGHT ARCJETS; Daisuke Nakata, Muroran Institute of Technology, 27-1, Mizumoto-cho, Muroran-shi, Hokkaido 050-8585, Japan, Kiyoshi Kinefuchi, Japan Aerospace Exploration Agency, 2-1-1, Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan, Masahiro Kinoshita, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan, Satoshi Hosoda, Aerospace Exploration Agency, 3-1-1, Yoshinodai, Chuoku, Sagamihara-shi, Kanagawa 252-5210, Japan, Hirokazu Tahara, Osaka Institute of Technology, 5-16-1, Omiya Asahi-Ku, Osaka 535-8585, Japan, Hitoshi Kuninaka, Aerospace Exploration Agency, 3-1-1, Yoshinodai, Chuoku, Sagamihara-shi, Kanagawa 252-5210, Japan

2013-294: 2D AXISYMMETRIC FLUID AND ELECTROMAGNETIC MODELS FOR INDUCTIVELY COUPLED PLASMA (ICP) NI RF ION THRUSTERS; Emre Turkoz and Murat Celik, Bogazici University, Istanbul, Turkey

2013-295: PLASMADIAGNOSTICS IN THE PLUME OF A RADIOFREQUENCY ION THRUSTER; Christoph Eichhorn, Frank Scholze, Carsten Bundesmann, and Horst Neumann, Leibniz-Institute of Surface Modification (IOM), Permoserstrasse 15, D-04318 Leipzig, Germany

2013-296: DIRECT FUSION DRIVE ROCKET FOR ASTEROID DEFLECTION; Joseph B. Mueller, Yosef S. Razin, Michael A. Paluszek, Amanda J. Knutson, and Gary Pajer, Princeton Satellite Systems, 6 Market St., Suite 926, Plainsboro, NJ, 08536, USA; Samuel A. Cohen, Plasma Physics Laboratory, 100 Stellarator Road, Princeton, NJ, 08540; and Allen H. Glasser, University of Washington, Department of Aeronautics and Astronautics, Guggenheim Hall, Seattle, WA 98195

20123-297: BEAM DIAGNOSTICS FOR MINI ION ENGINES; Peter E. KÃ¶hler and Bruno K. Meyer, University of Giessen, 1. Physikalisches Insitut, 35392 Griessen, Germany

2013-298: 3D THERMAL SIMULATION OF A ÂµN-RIT; Waldemar GÃ¤rtner, Benjamin Lotz, and Bruno K. Meyer, Justus-Liebig-University Giessen, I. Physikalisches Institut, Giessen, hessen, 35392, Germany

2013-299: OVERVIEW, QUALIFICATION AND DELIVERY STATUS OF THE HEMPT BASED ION PROPULSION SYSTEM FOR SMALLGEO; Stefan Weis, Alexey Lazurenko, Benjamin van Reijen, Jens Haderspeck, Angelo Genovese, and Peter Holtmann, Thales Electronic Systems GmbH, Soeflinger Str. 100, D-89077 Ulm, Germany; Klaus Ruf and Norbert PÃ¼ttmann, Deutsches Zentrum FÃ¼r Luft- und Raumfahrt e. V. (DLR) – Raumfahrt-Agentur, KÃ¶nigswinterer Strasse 522-524, 53227 Bonn; Martin Schirra, Hochschule fÃ¼r angewandte Wissenschaften Kempten, BahnhofstraÃŸe 61, 87435 Kempten, Germany

2013-300: ELECTROSTATIC ANALYZERS WITH APPLICATION TO ELECTRIC PROPULSION TESTING; Casey C. Farnell and Cody C. Farnell, Colorado State University, Fort Collins, CO 80523, USA, Shawn C. Farnell, Kenyon College, Gambier, OH 43022, USA, Plasma Controls, LLC, Fort Collins, CO 80526, USA, and John D. Williams, Colorado State University, Fort Collins, CO 80523, USA, Plasma Controls, LLC, Fort Collins, CO 80526, USA

2013-301: THREE DIMENSIONAL SIMULATION OF MICRO NEWTON RITS; Robert Henrich and Christian Heiliger, Justus-Liebig-University, Giessen, 35392, Germany

2013-304: GLOBAL STABILITY ANALYSIS OF AZIMUTHAL OSCILLATIONS IN HALL THRUSTERS; Diego Escobar, Universidad Politecnica de Madrid (UPM), Madrid, 28040, Spain, Eduardo Ahedo, Universidad Carlos III de Madris (UC3M), Leganes, 28911, Spain

2013-305: INSTANT START ELECTRIDE HOLLOW CATHODE; Lauren P. Rand and John D. Williams, Colorado State University, Fort Collins, CO, 80523, USA

2013-306: INNOVATIVE VACUUM ARC THRUSTER FOR CUBESAT CONSTELLATIONS; Mathias Pietzka, Marina Kuhn-Kauffeldt, and Jochen Schein, University of the Federal Armed Forces Munchen, Werner-Heisenberg-Weg 39, 85577 Neubiberg, Germany, Igal Kronhaus and Klaus Schilling, Justus-Maximilians-Universitat Wurzburg, Am Hubland, 97074, Wurzburg, Germany, Toni Mai and Anton Lebeda, Apcon AeroSpace & Defense GmbH, Prof.-Messerschmidt-Str. 4, 85577 Neubiberg, Germany

2013-307: 3D SIMULATION OF THE ROTATING SPOKE IN A HALL THRUSTER; K. Matyash and R. Schneider, Greifswald University, Greifswald, D-17487, Germanhy, S. Mazouffre and S. Tsikata, ICARE, Centre National de la Recherche Scientifique, 45071 Orleans, France, Y. Raitses and A. Diallo, Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543, USA

2013-311: IODINE PROPELLANT SPACE PROPULSION; James Szabo, Mike Robin, Surjeet Paintal, Bruce Pote, Vlad Hruby, Chas Freeman, Busek Co. Inc. Natick, MA, 01760, USA

2013-313: ACCURATELY DETERMINING THE PLASMA POTENTIAL USING EMISSIVE PROBES; J. P. Sheehan, University of Michigan, Ann Arbor, MI, 48103, USA, Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08543, USA, Noah Hershkowitz, University of Wisconsin – Madison, Madison, WI, 53706, USA

2013-315: INSIGHT INTO PERFORMANCE IMPROVEMENT OF ECR NEUTRALIZER; W. Ohmichi, The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan, H. Kuninaka, The Institute of Space and Astronautical Science, Sagamihara, Kanagawa, 252-5210, Japan

2013-317: EIGHT KILOWATT HALL THRUSTER SYSTEM CHARACTERIZATION; James Szabo, Bruce Pote, Lawrence Byrne, Surjeet Paintal, Vlad Hruby, Rachel Tedrake, George Kolencik, and Chas Freeman, Busek Co. Inc, Natick, MA, 01760, USA; Nikolaos Gatsonis, Worchester Polytechnic Institute, Worcester, MA 01609, USA

2013-318: PROGRESS ON THE DEVELOPMENT OF A PULSED PLASMA THRUSTER FOR THE ASTER MISSION; Fin Paula and Intini Marques, R., INPE – The Brazilian National Institute for Space Research, LCP – Combustion and Propulsion Laboratory – Cachoeira Paulista – Sao Paulo State, Brazil

2013-319: IONIC LIQUID FERROFLUID ELECTROSPRAY WITH EMIM-NTf2 AND FERROFLUID MODE STUDIES WITH FERROTEC-EFH-1 IN A NON-UNIFORM MAGNETIC FIELD; Edmond J. Meyer IV and Lyon B. King, Michigan Technological University, Houghton, MI 49931, USA; Nirmesh Jain and Brian s. Hawkett, University of Sydney, NSW, 2006, Australia

2013-320: APPLICATION OF AUGER SPECTROSCOPY FOR MEASUREMENT OF SECONDARY ELECTRON EMISSION FROM CONDUCTING MATERIAL FOR ELECTRIC PROPULSIOIN DEVICES; Marlene I. Patino, University of California, Los Angeles, CA, 90095, USA, Yevgeny Raitses, Princeton Plasma Physics Laboratory, Princeton, NJ, 08540, USA, and Richard E. Wirz, University of California, Los Angeles, CA 90095, USA

2013-321: OVERVIEW OF MISSION DESIGN FOR NASA ASTEROID REDIRECT ROBOTIC MISSION CONCEPT; Nathan Strange, Damon Landau, Timothy McElrath, Gregory Lantoine and Try Lam, Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Dr., Pasadena, CA, 91109; Melissa McGuire, Laura Burke, and Michael Martini, NASA Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH, 44135; and John Dankanich, NASA Marshall Space Flight Center, Huntsville, AL, 35812

2013-324: MODELING OF A DC-RF PLASMATHRUSTER WITH THE NAVIER-STOKES CODE SINA; U. Bauder and G. Herdrich and S. Fasoulas, Institute of Space Systems (IRS), University of Stuttgart, 70569 Stuttgart, Germany; M. Auweter-Kurtz, German Aerospace Academy ASA, 71304 BÃ¶blingen, Germany

2013-325: IS THERE A FUTURE FOR FISSION NUCLEAR ELECTRIC PROPULSION; Richard Blott, Director, Space Enterprise Partnerships Ltd, Eastergate, West Sussex, PO20 3SJ, UK, Christophe Koppel, KopooS Consulting Ind, Paris, 75008, France, Dr. Dominique Valentian, ITG, Paris, 75008, France, Dr. Frank Jansen, DLR, Bremen, 28359, Germany, Prof. Claudio Ferrari, ISIS R&D, Rome, 00146, Italy, Prof. Claudio Bruno, c/o ISIS R&D, Rome, 00146, Italy, Priv. Doz. Dr., Adj. Assoc, Prof/Baylor Georg Herdrich, IRS Stuttgart, Stuttgart, Stuttgart 70714, Germany, Dipl.-Ing. Roland Gabrielli, IRS Stuttgart, Stuttgart 70714, Germany

2013-327: NEAR ANODE PLASMA IN THE PLASMA INTERACTION FACILITY AT UCLA; Taylor S. Matlock, Dan M. Goebel, and Richard E. Wirz, University of California Los Angeles, Los Angeles, CA, 90095, USA

2013-329: EXPERIMENTAL INVESTIGATION OF MOMENTUM TRANSFER TO SOLID SURFACES BY THE IMPACT OF ENERGETIC IONS AND ATOMS; Thomas Trottenberg, Jakob Rutscher, and Holger Kersten, Institute of Experimental and Applied Physics, University of Kiel, 24098 Kiel, Germany

2013-331: ELECTRON LOSS AT A MAGNETIC CUSP FOR A RANGE OF UPSTREAM MAGNETIC FIELD CONDITIONS; Dankongkakul B. and Wirz R. E., University of California, Los Angeles, CA, 90024, USA

2013-332: ELECTRIC PROPULSION FOR COMMERICAL APPLICATIOS; IN-FLIGHT AND PERSPECITVE AT EUTELSAT; C. Casaregola, Eutelsat SA, Paris, 75015, France

2013-334: PRELIMINARY MAGNETOHYDRODYNAMIC SIMULATIONS OF MAGNETIC NOZZLES; Frans H. Ebersohn, Benjamin W. Longmier, and J.P. Sheehan, University of Michigan, Ann Arbor, MI 48109, USA; John V. Shebalin, NASA JSC, ARES, Houston, TX, 77058, USA; Sharath S. Girimaji, Texas A&M University, College Station, TX, 77843, USA

2013-336: VASIMR SOLAR POWERED MISSIONS FOR NEWA RETRIEVAL AND NEA DEFLECTION; Andrew V. Ilin, Daniel A. Gilman, Mark D. Carter, Franklin R. Chang Diaz, Jared P. Squire and Joseph E. Farrias, Ad Astra Rocket Company, Webster, Texas, 77598, USA

2013-338: ENHANCEMENT OF THRUST PERFORMANCE OF A MPD THRUSTER WITH MAGNETIC NOZZLE; Akira Ando, Kazunori Takahashi, Yuuki Izawa, Kiyotaka Suzuki, and Yusuke Hoshino, Department of Electrical Engineering, Tohoku University, Sendai, 980-8579, Japan

2013-339: ACTIVE CONTROL AND EXCITATION OF BREATHING OSCILLATIONS IN A HALL THRUSTER WITH A FAST DIGITAL SIGNAL PROCESSOR; S. Barral, J. Kaczmarczyk, and J. Kurzyna, Institute of Plasma Physics and Laser Microfusion, 01-497 Warsaw, Poland, and M. Dudeck, UniversitÃ© Pierre et Marie Curie-Paris 6, 75252 Paris Cedex, France

2013-344: LOW POWER ABLATIVE PULSED PLASMA THRUSTERS; Paolo Gessini, Lui T. C. Habl, Manuel N. D. Barcelos Jr., and Jose L. Ferreira, University of Brasilia, Brasilia, DF, 72444-240, Brazil, Rodrigo I. Marques, National Institute for Space Research (INPE), Cachoeira Paulista, SP, 126300-000, Brazil, Michele Coletti, Mars Space Ltd., Southampton, Hampshire, SO14 5FE, United Kingdom

2013-346: EFFECT OF ION-NEUTRAL COLLISIONS ON SHEATH POTENTIAL PROFILE; Samuel Langendorf and Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA 30332, USA; Laura Rose and Michael Keidar, George Washington University, Washington, DC 20052, USA; Lubos Brieda, Particle in Cell Consulting LLC, Falls Church, VA 22046

2013-347: A 205 HOUR KRYPTON PROPELLANT LIFE TEST OF THE SPT-100 OPERATING AT 2 KW; Michael R. Nakles, ERC, Inc., Edwards Air Force Base, CA, 93524, Jorge J. Delgado and Ronald L. Corey, Space Systems/Loral, Palo Alto, CA 94303

2013-348: OPERATION OF SPINDT-TYPE, CARBON NANOTUBE COLD CATHODES IN A HALL EFFECT THRUSTER ENVIRONMENT; Lake A. Singh and Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA 30332, USA, Graham P. Sanborn, Stephan P. Turano, and W. Jub Ready, Georgia Tech Research Institute, Atlanta, GA 30332, USA

2013-349: PARTICLE SIMULATION OF NEAR-SURFACE CUSP CONFINEMENT OF WEAKLY IONIZED PLASMA; Samuel J. Araki and Richard E. Wirz, University of California, Los Angeles, CA, 90095, USA

2013-351: TOWARDS A CAVITY ENHANCED THOMSON SCATTERING DIAGNOSTIC FOR ELECTRIC PROPULSION RESEARCH; Adam Friss, Brian Lee, Isaiah Franka, and Azer Yalin, Colorado State University, Fort Collins, CO, 80523, USA

2013-352: PRACTICAL APPLICATION OF WIDE BANDWIDTH FLOATING EMISSIVE PROBES AND WAVELET ANALYSIS TO THE X2 NESTED HALL THRUSTER; Michael S. McDonald, Raymond Liang, and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), University of Michigan, Ann Arbor, MI, USA 48109

2013-353: COMPARISON OF BREATHING AND SPOKE MODE STRENGTH IN THE H6 HALL THRUSTER USING HIGH SPEED IMAGING; Michael S. McDonald and Alec D. Gallimore, Plasmadynamics and Electric Propulsion Laboratory (PEPL), University of Michigan, Ann Arbor, MI USA 48109

2013-354: TESTING AND COMPREHENSIVE MODELING OF A GIE UTILIZING ATMOSPHERIC PROPELLANTS; D. Feili, Astronautics Research Group, University of Southampton, SO17 1BJ, U.K., B. Lotz, B. Meyer, and H. Loeb, I. Physics Institute of Justus Liebig University, Giessen, D-35392, Germany, C. Collingwood, TransMIT GmbH, D-35390 Giessen, Germany, M. Smimova and S. Khartov, Moscow Aviation Institute (National Research Center), Volokolamskoe Shosse 4, 125993 Moscow, Russia, D. Di Cara and A. Bulit, ESA/ESTEC, Keplerlaanl, 2200 AG Noordwijk ZH, The Netherlands

2013-356: DEVELOPMENT AND VALIDATION OF A NOVEL TIME-RESOLVED LASER-INDUCED FLUORESCENCE TECHNIQUE; Christopher J. Durot, Alec D. Gallimore, and Timothy B. Smith, University of Michigan, Ann Arbor, MI, 48105, USA

2013-358: RECOMMENDED PRACTICE FOR PRESSURE MEASUREMENTS AND CALCULATION OF EFFECTIVE PUMPING SPEEDS DURING ELECTRIC PROPULSION TESTING; John W. Dankanich, Marshall Space Flight Center, MSFC, AL, 35812, USA, Mitchell Walker, Georgia Institute of Technology, Atlanta, GA, 30332, USA, Michael W. Swiatek and John T. Yim, NASA Glenn Research Center, Cleveland, OH, 44132

2013-359: CUBESAT MICROWAVE ELECTROTHERMAL THRUSTER (CÂµMET), Mikhail D. Abaimov, Swarna Sinha, Sven G. Bilen, and Michael M. Micci, The Pennsylvania State University, University Park, PA 16802, USA

2013-361: DEVELOPMENT OF A STEADY OPERATING PULSED POWER SYSTEM FOR FRC AND INDUCTIVE THRUSTERS; David Kirtley, Jim Pihl, and Chris Pihl, MSNW LLC, Redmond, WA 98052, USA

2013-362: ARGON AND XENON PLASMA ENERGY ANALYSIS IN A PULSED INDUCTIVE TEST ARTICLE; Ryan A. Pahl and Joshua L. Rovey, Missouri University of Science and Technology, Rolla, MO, 65401, USA

2013-364: OBSERVATION AND ANALYSIS OF GRAPHITE HOLLOW CATHODE AFTER 45,000-HOUR LIFE TEST; Yasushi Ohkawa, Toshiharu Higuchi, Yukio Hayakawa, Katsuhiro Miyazaki, and Hiroshi Nagano, Propulsion Group, Japan Aerospace Exploration Agency, 7-44-1 Jindaiji-higashi-machi, Chofu, Tokyo 182-8522, Japan

2013-365: LOW-THRUST ORBITAL MANEUVER ANALYSIS FOR CUBESAT SPACECRAFT WITH A MICRO-CATHODE ARC THRUSTER SUBSYSTEM; Samudra E. Haque, Michael Keidar, and Taeyoung Lee, The George Washington University, Washington, DC 20052, USA

2013-366: LOW-THRUST ATTITUDE CONTROL FOR NANO-SATELLITE WITH MICRO-CATHODE THRUSTERS; Tse-Huai Wu, Taeyoung Lee and Michael Keidar, The George Washington University, Washington DC, 20052, USA

2013-367: LASER-COLLISIONAL INDUCED FLUORESCENCE STUDY OF ELECTRON DISTRIBUTIONS IN A MAGNETIC CUSP; Aimee A. Hubble and John E. Foster, University of Michigan, Ann Arbor, MI, 48109, USA, Edward V. Barnat and Brandon R. Weatherford, Sandia National Laboratories, Albuquerque, NM, 87123, USA

2013-368: ADVANCED FLOW CONTROL DEVICES BASED ON MEMS TECHNOLOGY FOR ELECTRIC PROPULSION; J. Bejhed, K. Jonsson, T-A. Gronland and P. Rangsten, NanoSpace AB, Uppsala, SE-751 83, Sweden

2013-369: DEMIXING IN THE LOW POWER ARGON/HELIUM ARCJET; Jinyue Geng, Xuan Chen, and Hai-Xing Wang, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China, Michael Keidar, George Washington University, Washington DC 20052, USA

2013-372: ELECTOMAGNETICALLY DRIVEN FUSION PROPULSION; John Slough, University of Washington, Plasma Dynamics Laboratory, Redmond, WA, 98052, USA, Anthony Pancotti, David Kirtley, and George Votroubek, MSNW LLC, Redmond, WA, 98052

2013-373: INVESTIGATING THE POTENTIAL OF MINIATURIZED ELECTRODYNAMIC TETHERS TO ENHANCE CHIPSATS; Iverson C. Bell III, Brian E. Gilchrist, David Liaw, Vritika Singh, and Kyle A. Hagen, The University of Michigan, Ann Arbor, MI 48109, USA. Sven G. BilÃ©n and Jesse K. McTernan, The Pennsylvania State University, University Park, PA 16802, USA

2013-374: MOMENTUM MODELING OF A HALL THRUSTER PLUME; Mark W. Crofton, The Aerospace Corporation, El Segundo, California 90245, USA; Iain D. Boyd, University of Michigan, Ann Arbor, Michigan 48109, USA

2013-376: ELECTORMAGNETIC OPTIMIZATION OF FRC-BASED PULSED PLASMA THRSUTERS; Jamie Waldock, University of Washington, Seattle, WA, 98105, United States, Dr. David Kirtley and Dr. John Slough, MSNW LLC., Redmond, WA, 98052, United States

2013-377: TRANSIENT AND STEADY STATE THERMAL MODELING OF PULSED INDUCTIVE FRC-BASED THRUSTERS; Michael Pfaff, University of Washington, Seattle, WA, 98105, United States, Dr. David Kirtley and Dr. John Slough, MSNW LLC, Redmond, WA, 98052, United States, Jim Pihl, Raven Technologies LLC, Woodinville, Washington, 98072

2013-378: ARGON AND XENON PULSED THETA-PINCH PLASMA VIA OPTICAL EMISSION SPECTROSCOPY; Warner C. Meeks and Joshua L. Rovey, Missouri University of Science and Technology, Rolla, MO, 65409, USA

2013-379: INFLUENCE OF TAILORED APPLIED MAGNETIC FIELDS ON HIGH-POWER MPD THRUSTER CURRENT TRANSPORT AND ONSET-RELATED PHENOMENA; Robert C. Moeller and James E. Polk, Jet Propulsion Laboratory (JPL), California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109, USA

2013-380: A COMPARATIVE STUDY OF HEATERLESS HOLLOW CATHODE: 2D PIC MODELING VS. EXPERIMENT; V. Vekselman, Department of Material Science and Engineering, Clemson University, Clemson, SC, 29634, USA, D. Levko, LAPLACE (Laboratoire Plasma et Conversion d’Energier), Universite de Toulouse, UPS, INPT Toulouse, 118 route de Narbonne, F-31062, France, Ya E. Krasik, Department of Physics, Technion, Haifa, 32000, Israel, and I. Haber, University of Maryland, College Park, Maryland 20742-3511, USA

2013-381: INVESTIGATIONS OF DISCHARGE CHAMBER MATERIAL INFLUENCE ON SMALL HALL THRUSTER PARAMETERS; Andriy V. Loyan and Taras A. Maksymenko, National Aerospace University, Kharkiv, 61070, Ukraine

2013-382: QUALIFICATION OF AN ADVANCED XENON FLOW CONTROL MODULE; Joseph M. Cardin, William Cook, and Rajesh Bhandari, VACCO Industries, Inc., south El Monte, California, 91733, USA

2013-384: HIGH-SPEED IMAGING OF THE FIRST KINK MODE INSTABILITY IN A SELF-FIELD MAGNETOPLASMADYNAMIC THRUSTER; Jonathan A. Walker, Samuel Langendorf, and Mitchell Walker, Georgia Institute of Technology, Atlanta, GA, 30332, USA, Kurt Polzin and Adam Kimberlin, Marshall Space Flight Center, Huntsville, AL, 35812, USA

2013-385: TEMPORAL FLUCTUATIONS IN A 100-A LAB6 HOLLOW CATHODE; Benjamin A. Jorns and Ioannis G. Mikellides, and Dan M. Goebel, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA

2013-388: HIGH INPUT VOLTAGE DISCHARGE SUPPLY FOR HIGH POWER HALL THRUSTERS USING SILICON CARBIDE DEVICES; Luis R. PiÃ±ero, Robert J. Scheidegger and Michael V. Aulisio, NASA Glenn Research Center, Cleveland, OH, 44135, USA, Arthur g. Birchenough, Vantage Partners LLC, Cleveland, OH, 44135, USA

2013-389: COMPARATIVE ANALYSIS OF MICRO-CATHODE ARC THRUSTER PERFORMANCE; Alexey Shashurin and Michael Keidar, The George Washington University, Washington, DC 20052, USA; Taisen Zhuang, US Medical Innovations, LLC, Takoma Park, MD 20912, USA; The George Washington University, Washington, DC 20052, USA

2013-390: ELECTRON EMISSION FROM NANO AND MICRO ENGINEERED MATERIALS RELEVANT TO ELECTRIC PROPULSION; Y. Raitses and I. D. Kaganovich, Princeton Plasma Physics Laboratory, Princeton, NJ 08543, USA, A. V. Sumant, Center for Nanoscale Materials, Argonne National Laboratory, Argonne, IL 6043, USA

2013-391: PHYSICS OF A VACUUM ARC FOR A PLASMA THRUSTER APPLICATION; Isak I. Beilis, Electrical Discharge and Plasma Laboratory, Department of Electrical Engineering – Physical Electronics, Faculty of Engineering, Tel Aviv University, P.O.B. 39040, Tel Aviv 69978, Israel

2013-392: STANDARD PRACTICES FOR USAGE OF INDUCTIVE MAGNETIC FIELD PROBES WITH APPLICATION TO ELECTRIC PROPULSION TESTING; Kurt A. Polzin, NASA Marshall Space Flight Center, Huntsville, AL 35812, Carrie S. Hill, ERC Inc., Air Force Research Laboratory, Edwards Air Force Base, CA 93524, Peter J. Turchi, Los Alamos, NM 87545, Rodney L. Burton, University of Illinois at Urbana-Champaign, Urbana, IL 61801, Sarah Messer, HyperV Technologies Corp., Chantilly, VA 20151, Ralph H. Lovberg, University of California – San Diego, La Jolla, CA 92093, Ashley K. Hallock, Yetispace, Inc., Huntsville, AL 35811

2013-394: FIRST FIRING OF A 100-KW NESTED-CHANNEL HALL THRUSTER; Roland E. Florenz, Scott J. Hall, and Alec D. Gallimore, University of Michigan, Ann Arbor, MI, 48109, U.S.A., Hani Kamhawi and Christopher M. Griffiths, NASA Glenn Research Center, Cleveland, OH, 44135, U.S.A., Daniel L. Brown, Air Force Research Laboratory, Edwards AFB, CA, 93523, U.S.A., Richard R. Hofer and James E. Polk, NASA Jet Propulsion Laboratory, Pasadena, CA, 91109, U.S.A.

2013-396: FLUID SIMULATION OF A MICROWAVE PLASMA CATHODE; L. Liard, Y. Zhu, G. J. M. Hagelaar and J. P. Boeuf, UniversitÃ© de Toulouse, UPS, INPT, LAPLACE (Laboratoire Plasma et Conversion d’Energie), 118 route de Narbonne, F-31062 Toulouse cedex 9, France; CNRS, LAPLACE, F-31062 Toulouse, France

2013-398: TOWARDS UNDERSTANDING THE EEDF VARIATIONS IN A HALL THRUSTER CHANNEL DUE TO SECONDARY ELECTRON EMISSION IN A HIGHLY CONTROLLED CROSSED FIELD EXPERIMENT; Kapil U. Sawlani and John E. Foster, University of Michigan, Ann Arbor, MI, 48109, USA

2013-399: NEUTRAL XENON DENSITY IN THE SPT-140 NEAR-FIELD PLUME; M. W. Crofton, A. G. Hsu Schouten, J. A. Young, E. J. Beiting, and K. D. Diamant, The Aerospce Corporation, el Segundo, California 90245, USA; R. L. Corey and J. J. Delgado, Space Systems/Loral, Palo Alto, CA 94303, USA

2013-400: COUPLED FLUCTUATIONS OF BULK PLASMA AND THE SHEATH IN PLASMAS WITH E0 X B0 DRIFT; W. Frias and A. I. Smolyakov, University of Saskatchewan, Saskatoon, SK, S7N 5E2, Canada; Y. Raitses and I. D. Kaganovich, Princeton Plasma Physics Laboratory, Princeton University, Princeton, NJ, 08543, USA

2013-403: THE ELECTRIC PROPULSION LIBRARY OF ESPSS FOR SYSTEM SIMULATIONS; Christophe R. Koppel, KopooS Consulting Ind., 57 rue d’Amsterdam 75008 Paris, France, Fernando Rodriquez Lucas, Empresarios Agrupados, c/Magallanes 3, 28015 Madrid, Spain, Dr. Francesco Di Matteo and Dr. Johan Steelant, ESA-ESTEC, Keplerlaan 1, 2201AZ Noordwijk, The Netherlands

2013-405: 30-KW SEP SPACECRAFT AS SECONDARY PAYLOADS FOR LOW-COST DEEP SPACE SCIENCE MISSIONS; John R. Brophy and Tim Larson, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

2013-406: NUMERICAL SIMULATION OF NONEQUILIBRIUM FLOW IN A LOW-POWER HYDROGEN ARCJET; Wei-Ping Sun, Fu-Zhi Wei, and Hai-Xing Wang, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China

2013-408: COMPARISON OF PLASMA DIAGNOSTICS OF A HELICON THRUSTER USING ARGON AND WATER VAPOR WITH HELIUM; Adriane J. Faust and Raymond J. Sedwick, University of Maryland, College Park, MD, 20742, USA

2013-409: MICRO CATHODE ARC THRUSTER PHONESAT EXPERIMENT FOR SMALL SATELLITES; Samudra E. Haque, George Teel, and Michael Keidar, The George Washington University, Washington, DC 20052, United States, Elwood F. Agasid, Oriol Tintore Gazulla, Andres Dono Perez, Greenfield T. Trinh, and Eddie A. Uribe, NASA Ames Research Center, Moffett Field, California, 94305, United States

2013-410: MIDDLE POWER HALL EFFECT THRUSTERS WITH CENTRALLY LOCATED CATHODE; A. Loyan, M. Titov, O. Rybalov, and T. Maksymenko, National Aerospace University “KhAI”, 61070 Kharkiv, Ukraine

2013-411: EFFECT OF ELECTRONS NON-MIRROR REFLECTION FROM POTENTIAL SHIELD ON PLASMA BORDERS INSIDE HELICON AND HALL EFFECT THRUSTERS; Nesterenko S. Yu, Roshanpour S., Le Quang Quyen, Ngo Dai Phong, Zhukovskiy National Aerospace University “KhAI”, Kharkov, 61070, Ukraine

2013-412: DEVELOPMENT OF A MINIATURE MICROWAVE DISCHARGE NEUTRALIZER FOR MINIATURE ION ENGINES; Naoji Yamamoto, Yoshiaki Hiraoka, and Hideki Nakashima, Kyushu University, Kasuga, Fukuoka, 816-8580, Japan

2013-413: DEVELOPMENT OF A TOF SETUP WITH AN ION-GUIDE FOR CHARACTERIZATION OF ELECTROSPRAY MICROTHRUSTERS; Subha Chakraborty, Simon Dandavino, Caglar Ataman, Daniel G. Courtney, and Herbert Shea, Ecole Polytechnique FÃ©dÃ©rale de Lausanne (EPFL), Neuchatel, 2002, Switzerland

2013-414: LAGRANGIAN COHERENT STRUCTURES IN THE ELLIPTIC RESTRICTED THREE-BODY PROBLEM AND SPACE MISSION DESIGN; Lorenzo Provinciali and Michele Mastropietro, UniversitÃ¡ de Pisa, Pisa, 56100, Italy, Pierpaolo Pergola and mariano Andrenucci, Alta S.p.A., Pisa, 56100, Italy

2013-416: KINETIC MODELING OF THE JET EXGTRACTION MECHANISM IN SPHERICAL IEC DEVICES; Georg Herdrich, Constanze Syring, and Marcel Pfeiffer, Institute of Space Systems (IRS), Stuttgart, 70569, Germany, Dejan Petkow, ESA-ESTEC Advanced Concepts Team, Keplerlaan 1, Noordwijk, 2201, The Netherlands

2013-418: MICRONEWTON BALANCE MEASUREMENTS AT ONERA AND APPLICATION TO THE GAIA MISSION; D. Packan, J. Jarrige, P. thobois, C. Blanchard, and P. –Q. Elias, ONERA – The French Aerospace Lab, Palaiseau, 91761, France, L. Fallerini and G. Noci, SELEX ES, Campi Bisenzio, 50013, Italy

2013-420: PERFORMANCE COMPARISON OF AN ECR PLASMA THRUSTER USING ARGON AND XENON AS PROPELLANT GAS; Julien Jarrige, Paul-Quentin Elias, FÃ©lix Cannat, and Denis Packan, ONERA – The French Aerospace Lab, Palaiseau, France

2013-421: ANALYSIS OF ATMOSPHERE-BREATHING ELECTRIC PROPULSION; Tony Schonherr and Kimiya Komurasaki, The University of Tokyo, Bunkyo Tokyo, 113-8656, Japan, Georg Herdrich, University of Stuttgart, Stuttgart, Baden-Wurttemberg, 70569, Germany

2013-422: CATHODE SPOT MOVEMENT IN VACUUM ARC USING SILICON CATHODE; Joel D. Slotten, George Teel, Dereck Chui, and Michael Keidar, The George Washington University, Washington, DC, 20052, USA

2013-424: THE APPLICABILITY OF PULSED PLASMA THRUSTERS TO RENDEZVOUS AND DOCKING OF CUBESATS; Stephen Gabriel and Eric Rogers, University of Southampton, England; Mirko Leomanni, University of Siena, Italy

2013-425: FLOW CONTROL AND MEASUREMENT IN ELECTRIC PROPULSION SYSTEMS: TOWARDS AN AIAA REFERENCE STANDARD; John Steven Snyder, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, Jeff Baldwin, SSL, Palo Alto, CA 94303, Jason D. Frieman and Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA 30332, Nathan S. Hicks, The Boeing Company, Seattle, WA 98108, Kurt A Polzin, NASA Marshall Space Flight Center, Huntsville, AL 35812, James T. Singleton, Air Force Research Laboratory, Aerospace Systems Directorate, Edwards AFB, CA 93524

2013-428: PLASMA DIAGNOSTICS SYSTEM DEVELOPMENT FOR PERMANENT MAGNET HALL THRUSTERS; JosÃ© Leonardo Ferreira, Ivan Soares Ferreira, Jean Carlo Santos, Rodrigo Miranda, Paolo Gessini, Gabriela Possa and Lui T. C. Habl, University of Brasilia, Brasilia, DF, 70910-900, Brazil

2013-431: INVESTIGATION OF MAGNETIC NOZZLE PLASMA DETACHMENT USING SCALED DOWN PULSED MICRO-THRUSTER; T.E.R. Smith, T. Zhuang, and M. Keidar, George Washington University, Washington, DC, 20052

2013-435: EFFECT ON ELECTRON EMISSION OF INDUCTIVELY COUPLED PLASMA CATHODE’S LENGTH; Jun Sato, Natsumi Torii, Satoshi Kasagami, Chisato Ota, Junichiro Aoyagi, and Haruki Takegahara, Tokyo Metorpolitan University1, Hino, Tokyo, 191-0065, Japan

2013-437: PRELIMINARY CHARACTERIZATION OF ION ENERGY SPECTRA ACQUIRED FROM HIGH CURRENT HOLLOW CATHODES; Bradley S. Sommers and John E. Foster, University of Michigan, Ann Arbor, MI, 48109, USA, Chris N. Davis and Eric Viges, ElectroDynamic Applications, Inc., Ann Arbor, MI, 48109, USA

2013-439: 30 YEARS OF ELECTRIC PROPULSION FLIGHT EXPERIENCE AT AEROJET ROCKETDYNE; W. Andrew Hoskins and R. Joseph Cassady, Aerojet Rocketdyne, Arlington, VA, 22209, USA; Olwen Morgan, Roger M. Myers, and Fred Wilson, David Q. King, and Kristi deGrys, Aerojet Rocketdyne, Redmond, WA, 98052, USA

2013-440: RECOMMENDED PRACTICES IN THRUST MEASUREMENTS; James E. Polk, Anthony Pancotti, Thomas Haag, Scott King, Mitchell Walker, Joseph Blakely, and John Ziemer

2013-451: DEMONSTRATION OF THE XR-12 HALL CURRENT THRUSTER; Benjamin Welander, Jeff Monheiser, Nicole Meckel, Kristi de Grys, and Peter Peterson, Aerojet Rocketdyne, Redmond, WA 98052, Vadim Khayms, Lockheed Martin Space Systems Company, Sunnyvale, CA, 94089

2013-452: INFRARED THERMOGRAPHIC DIAGNOSTIC FOR IMAGING HALL THRUSTERS; Rostislav Spektor and Edward J. Beiting, The Aerospace Corporation, Los Angeles, CA 90009, USA, Marcus Byeman, David King, and Alex Mathers, Aerojet Rocketdyne, Redmond, WA, 98052, USA, Mark I. Luttrell and Arash Firooznam, Lockheed Martin Space Systems Company, Sunnyvale, CA, 94089, USA, Jonathan Paisley, Lockheed Martin Space System Company, Littleton, CO, 80125, USA

2013-453: COUPLED MOLECULAR DYNAMICS – THREE DIMENSIONAL POISSON SIMULATIONS OF IONIC LIQUID ELECTROSPRAY THRUSTERS; Arnaud Borner and Deborah A. Levin, Pennsylvania State University, University Park, PA 16802

2013-455: ASTEROID RETRIEVAL PROPULSION AND FLIGHT DYNAMICS CONCEPTS; Eric H. Cardiff and Jacob A. Englander, NASA Goddard Space Flight Center, Greenbelt, MD 20771

2013-456: SOLAR ELECTRIC PROPULSION DEMONSTRATION MISSION TRAJECTORY TRADES; William D. Deininger, Scott Mitchell, and Bryce Unruh, Ball Aerospace, Boulder, CO, 80301, USA; and John Dankanich, NASA Marshall Space Flight Center, Huntsville, AL, USA

2013-457: SOLAR ELECTRIC PROPULSION DEMONSTRATION MISSION BASELINE CONCEPT DESCRIPTION; William D. Deininger, Scott Enmger, Joe Hackel, J. C. Soto, and Bryce Unruh, Ball Aerospace, Boulder, CO, 80301, USA, Dave Murphy, ATK Aerospace Systems, Goleta, CA, 93117, USA, Kristi DeGrys, Aerojet Rocketdyne, Redmond, WA, 98052, USA

2013-458: ION VELOCIMETRY MEASUREMENTS AND PARTICLE-IN-CELL SIMULATION OF A CYLINDRICAL CUSPED PLASMA ACCELERATOR; A. Lucca Fabris, M. Manente, and D. Pavarin, University of Padova, Padova, 35131, Italy; C. V. Young and M. A. Cappelli, Stanford University, Stanford, CA 94305, USA

2013-459: MEASUREMENT OF THE SHEATH PROTENTIAL WITH SECONDARY ELECTRON EMISSION: PROGRESS TOWARD A LASER-INDUCED FLUORESCENCE TECHNIQUE FOR LOW-DENSITY XENON PLASMAS; Alexander C. Englesbe, Kapil U. Sawlani, and John E. Foster, University of Michigan, Ann Arbor, Michigan, 48109, USA

2013-A: DEVELOPMENT STATUS AND FUTURE OF THE EUPROPEAN ELECTRIC PROPULSION PLUME DATA ASE; A. Reissner and S. Hummel, FOTEC Forschungs- und Technologietransfer, GmbH, Wr. Neustadt, Austria; E. Gengembre, ESA-ESTEC, Noordwijk, The Netherlands

2013-B: INTEGRATION OF ELECTRIC PROPULSION SYSTEM WITH SPACECRAFT – AN OVERVIEW; Thomas M. Liu and Mitchell L. R. Walker, Georgia Institute of Technology, Atlanta, GA 30332

2013-C: MICRO-PROPULSION CONCEPTS UTILIZING MICROPLASMA GENERATORS; Kunning G. Xu, University of Alabama in Huntsville, Huntsville, AL, 35899, USA

2013-D: COMPUTATION OF TOTAL AND DIFFERENTIAL SPUTTER YIELDS OF BORON NITRIDE USING MOLECULAR DYNAMICS; Brandon D. Smith and Iain D. Boyd, Nonequilibrium Gas and Plasma Dynamics Laboratory, University of Michigan, Ann Arbor, Michigan, 48109, USA

2013-E: INTERACTIONS BETWEEN ION THRUSTER PLUMES AND VESSEL WALLS; J. Duras, O. Kalentev, K. Matyash, and R. Schneider, Ernst-Moritz-Arndt UniverstÃ¤t Greifswald, Felix-Hausdorff-StraÃŸe 12, 17489 Greisfswald, Germany; S. Kemnitz, University of Rostock, Albert-Einstein-StraÃŸe 22, 18059 Rostock, Germany; and A. Mutzke, Max-Planck-Institute for Plasma Physics, Wendelstein. Str. 1, 17491 Greifswald, Germany

2013-F: BACKGROUND PRESSURE EFFECTS ON KRYPTON HALL EFFECT THRUSTER INTERNAL ACCELERATION; William A. Hargus Jr., Landon J. Tango, and Michael R. Nakles, Air Force Research Laboratory, Edwards Air Force Base, CA 93524

2013-G: MN-FEEP THRUSTER MODULE DESIGN AND PRELIMINARY PERFORMANCE TESTING; A. Reissner, N. Buldrini, B. Seifert, and F. Plesescu, FOTEC Forschungs-und Technologietransfer GmbH, Wr. Neustadt, Austria, C. Scharlemann, University of Applied Sciences Wr. Neustadt, Austria, J. Gonzales del Amo, ESA-ESTEC, Noordwijk, The Netherlands

2013-H: EP TEST STANDARDS: FABRICATION, CALIBRATION, USAGE OF MAGNETIC FLUX PROBES WITH APPLICATION TO ELECTRIC PROPULSION TESTING; David Kirtley and George Votroubek, MSNW LLC, Redmond, WA 98052, USA, Hani Kamhawi, NASA Glenn Research Center Cleveland, OH 44135, and Thomas Weber, Los Alamos National Laboratory, Los Alamos, NM 87544

2013-I: PLASMA-WALL INTERACTION IN PRESENCE OF INTENSE ELECTRON EMISSION FROM WALLS; I. D. Kaganovich, A. V. Khrabrov, M. D. Campanell, H. Wang, and Y. Raites, Princeton Plasma Physics Laboratory, Princeton University, Princeton, New Jersey, USA, D. Sydorenko, Department of Physics, University of Alberta, Alberta, Canada

2013-J: TEST OF A NOVEL FEEP EMITTER WITH LISA PF HARDWARE; C. Scharlemann, University of Applied Science, Wiener Neustadt, Austria, N. Buldrini, FOTEC GmbH, Wiener Neustadt, Austria, R. Killinger, Astrium GmbH, D-74239 Lampoldshausen, Germany, D. DiCara, European Space Agency, ESTEC, Noordwijk, 2201 AZ, The Netherlands

2013-K: DEVELOPMENT AND PRIMARY IN-FLIGHT EXPERIENCE OF ELECTRIC PROPULSION SYSTEM ON SATELLITE SJ-9A; Dr. Shen Yan, Dr. Gao Jun, Ms. Wu Conglong, and Prof. Wei Yanming, Beijing Institute of Control Engineering, China, Prof. Zhao Zhiming and Prof. Liu Yiwei, China Spacesat C o., Ltd

2013-L: EFFECTS OF ASYMMETRIC SECONDARY EMISSION ON PLASMA PROPERTIES IN HALL THRUSTER ACCELERATION CHANNEL; H. Wang, M. D. Campanell, I. D. Kaganovich, A. V. Khrabrov, and Y. Raitses, Princeton Plasma Physics Laboratory, Princeton University, New Jersey, USA, D. Sydorenko, Department of Physics, University of Alberta, Alberta, Canada

2013-M: MULTISCALE MODELING OF HALL THRUSTERS; Lubos Brieda and Michael Keidar, The George Washington University, Washington, D.C. 20052

2013-N: DEVELOPMENT AND VERIFICATION OF A ÂµN THRUST BALANCE FOR HIGH VOLTAGE ELECTRIC PROPULSION SYSTEMS; B. Seifert, A. Reissner, N. Buldrini, and F. Plesescu, FOTEC Forschungs-und Technologietransfer GmbH, Wr. Neustadt, Austria, C. Scharlemann, University of Applied Sciences Wr. Neustadt, Austria

2013 FILE DIRECTORY

IEPC-2013-N

2015 INDEX

2015-01: OVERVIEW OF ELECTRIC PROPULSION RESEARCH ACTIVITIES IN JAPAN, Haruki Takegahara, Hitoshi Kuninaka, Ikkoh Funaki, Akira Ando, Kimiya Komurasaki, Hiroyuki Koizumi, Tony SchÃ¶nherr, Shunjiro Shinohara, Takao Tanikawa, Masakatsu Nakano, Yoshinori Nakayama, Akihiro Sasoh, Takeshi Miyasaka, Hirokazu Tahara, Naoji Yamamoto, Akira Kakami, Tokyo Metropolitan University, Japan

2015-02: EUROPEAN SPACE AGENCY (ESA) ELECTRIC PROPULSION ACTIVITIES, Jose Antonio Gonzalez Del Amo, ESA, the Netherlands

2015-03: EXPERIENCE OF MOSCOW AVIATION INSTITUTE IN THE FIELD OF ELECTRIC PROPULSION: HISTORY AND STATE OF THE ART, Sergey Khartov, Andrey Nadiradze, Igor Nazarenko, Stanislav Sevruk, Maria Smirnova, Moscow Aviation Institute, Russia

2015-04: SPACE SYSTEMS LORAL ELECTRIC PROPULSION SUBSYSTEM: 10 YEARS OF ON-ORBIT OPERATION, Jorge Javier Delgado, Jeff Baldwin, Ronald L. Corey, SSL, USA

2015-05: AN OVERVIEW OF ELECTRIC PROPULSION ACTIVITIES AT CNES, Claude Boniface, Nicolas Arcis, CNES, France

2015-06: DEMOCRITOS DEMONSTRATORS FOR REALIZATION OF NUCLEAR ELECTRIC PROPULSION OF THE EUROPEAN ROADMAPS MEGAHIT & DIPOP, Frank Jansen, Waldemar Bauer, Frederic Masson, Jean-Marc Ruault, Jean-Claude Worms, Emmanouil Detsis, Francois Lassoudiere, Richard Granjon, Enrico Gaia, Maria Cristina Tosi, Anatoly S. Koroteev, Alexander Semenkin, Tim Tinsley, Zara Hodgson, Christoph Koppel, Lamartine Guimaraes, DLR Institute of Space Systems, Germany

2015-07: PERFORMANCE AND FACILITY BACKGROUND PRESSURE CHARACTERIZATION TESTS OF NASA'S 12.5-KW HALL EFFECT ROCKET WITH MAGNETIC SHIELDING THRUSTER, Hani Kamhawi, Wensheng Huang, Thomas Haag, Rohit Shastry, Robert Thomas, John Yim, Daniel Herman, George Williams, James Myers, Richard Hofer, Ioannis Mikellides, Michael Sekerak, James Polk, NASA Glenn Research Center, USA

2015-08: THE ION PROPULSION SYSTEM FOR THE SOLAR ELECTRIC PROPULSION TECHNOLOGY DEMONSTRATION MISSION, Daniel Andrew Herman, Walter Santiago, Hani Kamhawi, James Polk, John Snyder, Richard Hofer, Morgan Parker, NASA Glenn Research Center, USA

2015-09: PROPULSION SYSTEM DEVELOPMENT FOR THE IODINE SATELLITE (ISAT) DEMONSTRATION MISSION, Kurt Alexander Polzin, Stephen Peeples, Joao Seixal, Stephanie Mauro, Brandon Lewis, Gregory Jerman, Derek Calvert, John Dankanich, Hani Kamhawi, Tyler Hickman, James Szabo, Bruce Pote, Lauren Lee, NASA Marshall Space Flight Center, USA

2015-10: PERFORMANCE OF PLUME CHARACTERIZATION OF THE SPT100-B THRUSTER, Damiano Pagano, Giovanni Coduti, Simone Scaranzin, Gianfranco Meniconi, Fabrizio Scortecci, Niccola Kutufa, AEROSPAZIO Tecnologie s.r.l., Italy

2015-12: ASSESSMENT OF THE AZIMUTHAL HOMOGENEITY OF THE NEUTRAL GAS IN A HALL EFFECT THRUSTER USING ELECTRON BEAM FLUORESCENCE, Julien Jarrige, Denis Packan, Olivier Duchemin, Lahib Balika, ONERA, France

2015-14: HOLLOW CATHODE MODELING: A FIRST APPROACH ON SCALING LAWS, Gaetan Sary, Laurent Garrigues, Jean-Pierre Boeuf, University of Toulouse, France

2015-15: HYBRID-PIC SIMULATION ON PLASMA FLOW OF HOLLOW CATHODE, Kenichi Kubota, Yuya Oshio, Hiroki Watanabe, Shinatora Cho, Yasushi Ohkawa, Ikkoh Funaki, JAXA, Japan

2015-16: NUMERICAL SIMULATION OF KEEPER EROSION IN A 6-KW LABORATORY HALL THRUSTER, Maria Choi, Iain D. Boyd, University of Michigan, USA

2015-17: STUDY ON HOLLOW CATHODE MODEL AND INNER PRESSURE, Bingjian An, Zhongxi Ning, Daren Yu, Harbin Institute of Technology, China

2015-18: SSC ZOND WITH APPT-95 BASED EPS, Nikolay Antropov, Michael Kazeev, Vladimir Khodnenko, Research Institute of Applied Mechanics and Electrodynamics, Russia

2015-20: REVIEW OF THERMAL PULSED PLASMA THRUSTER - DESIGN, CHARACTERIZATION, AND APPLICATION, Yung-An Chan, Christoph Montag, Georg Herdrich, Tony SchÃ¶nherr, University of Stuttgart, Germany

2015-21: PULSED PLASMA THRUSTER - SUBSYSTEM ENGINEERING AT IRS, Matthias Lau, Georg Herdrich, University of Stuttgart, Germany

2015-22: RESEARCH AND DEVELOPMENT OF HIGH-POWER ELECTROTHERMAL PULSED PLASMA THRUSTER SYSTEMS FOR OSAKA INSTITUTE OF TECHNOLOGY 2ND PROITERES NANO-SATELLITE, Keita Kanaoka, Ryota Fujita, Rikio Muraoka, Hirokazu Tahara, Takashi Wakizono, Osaka Institute of Technology, Japan

2015-23: SYSTEM ORIENTED DEVELOPMENT OF FUSION PROPULSION CONCEPTS, Roland Antonius Gabrielli, Adam Pagan, Eloi Ferrer-Gil, Georg Herdrich, Institute of Space Systems (IRS), Germany

2015-24: RESEARCH ON SPECIFIC MASS OF HIGH POWER NUCLEAR ELECTRIC PROPULSION SYSTEM WITH HIGH TEMPERATURE GAS-COOLED REACTOR, Cheng Zhou, Yong Li, Lei Wang, Wang Ge, Jun Gao, Daren Zou, Beijing Institute of Control Engineering, China

2015-28: R&D ACTIVITIES OF ELECTRIC PROPULSION IN JAPAN, Yasuhiro Satio, Kiyoshi Kinefuchi, Naoki Nagao, Koichi Okita, Hitoshi Kuninaka, JAXA, Japan

2015-29: ELECTRIC PROPULSION ACTIVITIES AT ONERA, Denis Packan, Paul-Quentin Elias, Julien Jarrige, Felix Cannat, Clement Zaepffel, Julien Labaune, Trevor Lafleur, ONERA, France

2015-30: ELECTRIC PROPULSION DEVELOPMENTS AT RAFAEL, Jacob Herscovitz, Zvi Zuckerman, Dan Lev, RAFAEL - Advanced Defense Systems, Israel

2015-33: WATER ELECTRICAL PROPULSION SYSTEM COMBINED WITH MANNED SPACE MISSION, Yuichiro Nogawa, Hirokazu Tahara, Splije LLC (Space Propulsion Limitless In Japan Engineering), Japan

2015-34: ELECTRICAL PROPULSION SYSTEM IN THE CONTROL OF EARTH OBSERVING SPACECRAFT, Vladimir Khodnenko, VNIIEM Corporation, JSC, Russia

2015-35: ELECTRIC PROPULSION SUBSYSTEM OPTIMIZATION FOR "ION BEAM SHEPHERD" MISSIONS, Filippo Cichocki, Mario Merino, Eduardo Ahedo, Davar Feili, Mercedes Ruiz, Universidad Carlos III de Madrid, Spain

2015-36: QUAD CONFINEMENT THRUSTER - INDUSTRIALISATION & FLIGHT INTEGRATION, Oliver A.I. Lane, Aaron Knoll, Surrey Satellite Technology Ltd, UK

2015-37: THRUSTER SUBSYSTEM FOR THE UNITED STATES NAVAL ACADEMY’S (USNA) BALLISTICALLY REINFORCED COMMUNICATION SATELLITE (BRICSAT-P), Samantha Audrey Hurley, George Teel, Joseph Lukas, Samudra Haque, Michael Keidar, Christopher Dinelli, Jin Kang, The George Washington University, USA

2015-40: PARAMETRIC OPTIMIZATION OF A HALL EFFECT THRUSTER MAGNETIC CIRCUIT, Alberto Rossi, Frederic Messine, Carole Henaux, Satafa Sanogo, Laplace laboratory, France

2015-41: EEDF CONTROL OF A HALL THRUSTER PLASMA USING A DOWNSTREAM REVERSE ORIENTATION CATHODE, Kimberly Renee Trent, Alec D. Gallimore, University of Michigan, USA

2015-43: LANTHANUM HEXABORIDE HOLLOW CATHODE FOR THE ASTEROID REDIRECT ROBOTIC MISSION 12.5 KW HALL THRUSTER, Dan M. Goebel, James E. Polk, California Institute of Technology, USA

2015-44: THERMAL CHARACTERISTICS OF A LANTHANUM HEXABORIDE HOLLOW CATHODE, James Polk, Dan Goebel, Pablo Guerrero, California Institute of Technology, USA

2015-46: FLEXIBLE LaB₆ HOLLOW CATHODE FOR LAB TESTS, Daniele Frollani, Michele Coletti, Stephen B. Gabriel, Mars Space Ltd, UK

2015-47: DEVELOPMENT OF A LaB₆ CATHODE FOR HIGH-POWER HALL THRUSTERS, Daniela Pedrini, Riccardo Albertoni, Fabrizio Paganucci, Mariano Andrenucci, University of Pisa, Italy

2015-49: NON-PHASE-DIFFERENCE ROGOWSKI COIL FOR MEASURING PULSED PLASMA THRUSTER DISCHARGE CURRENT, Zhe Zhang, Haibin Tang, Zun Zhang, Qi Liu, Shuai Cao, Beihang University, China

2015-50: DESIGN AND TESTING OF A SMALL INDUCTIVE PULSED PLASMA THRUSTER, Adam K. Martin, Alexandra Dominguez, Richard H. Eskridge, Kurt A. Polzin, Daniel P. Riley, Kevin A. Perdue, NASA Marshall Space Flight Center, USA

2015-51: DEVELOPMENT OF AN ENGINEERING OPTIMIZATION TOOL FOR MINIATURE PULSED PLASMA THRUSTERS, Igor O. Golosnoy, Stephen B. Gabriel, Simone Ciaralli, Michele Coletti, University of Southampton, UK

2015-53: ANALYSIS OF IGNITION OF THE MICRO CATHODE ARC THRUSTER, George Lewis Teel, Joseph Lukas, Alexey Shashurin, Michael Keidar, The George Washington University, USA

2015-54: EXPERIMENTAL INVESTIGATION OF AN ALUMINIUM FUELLED VACUUM ARC THRUSTER, Jonathan Kolbeck, D. Lines, Aaron Knoll, Surrey Space Centre, United Kingdom

2015-56: ANALYSIS OF VACUUM ARC USING SOLAR ARRAY MATERIALS, Joel D. Slotten, George Teel, Joseph Lukas, Michael Keidar, The George Washington University, USA

2015-57: NUMERICAL STUDIES OF MICRO-CATHODE ARC THRUSTER PLUME EXPANSION, Lubos Brieda, Michael Keidar, Particle In Cell Consulting LLC, USA

2015-58: HIGH SPECIFIC IMPULSE VACUUM ARC THRUSTERS WITH NOVEL ELECTRODE DESIGNS AND ARC OPERATION, Jonathan Lun, Craig Law, University of the Witwatersrand, South Africa

2015-59: DLR’S ELECTRIC PROPULSION TEST FACILITY – THE FIRST THREE YEARS OF THRUSTER OPERATION, Andreas Neumann, Christopher Geile, Stefan Staemm, Klaus Hannemann, DLR, Germany

2015-60: ESA PROPULSION LABORATORY AT ESTEC, Eduard Bosch Borras, Jose Gonzalez Del Amo, Alexandra Bulit, ESA, the Netherlands

2015-62: MEASUREMENT OF PLASMA PARAMETERS IN THE PLUME OF ELECTRIC PROPULSION DEVICES – RECENT WORKS PERFORMED AT THE ESA PROPULSION LABORATORY, Kaethe Dannenmayer, Alexandra Bulit, Jose Gonzalez Del Amo, ESA, the Netherlands

2015-63: A REVIEW OF PLASMA THRUSTER WORK AT THE AUSTRALIAN NATIONAL UNIVERSITY, Rod Boswell, Christine Charles, Australian National University, Australia

2015-64: ADVANCED SOLAR ELECTRIC PROPULSION FOR PLANETARY DEFENSE, John R Brophy, California Institute of Technology, USA

2015-65: ELECTRIC PROPULSION FOR DEEP SPACE: A STUDY CASE Â« JUPITER ICY MOON Â» WITH EP, Frederic R. Marchandise, Christophe R. Koppel, Snecma, Safran Group, France

2015-66: MODELING OF FORCE IMPACT ON LARGE-SIZED OBJECT OF SPACE DEBRIS BY ION INJECTION, Andrey B. Nadiradze, Vladimir A. Obukhov, Garri A. Popov, Victoria V. Svotina, Moscow Aviation Institute, Russia

2015-67: ELECTRODELESS LORENTZ FORCE (ELF) THRUSTER FOR ISRU AND SAMPLE RETURN MISSION, Anthony Pancotti, Justin Little, Jordan Neuhoff, Barry Cornella, David Kirtley, John Slough, MSNW LLC, USA

2015-68: MARS MISSION TRADE STUDIES AND TECHNOLOGY DEVELOPMENT OF A 36 MW FUSION ROCKET, Anthony Pancotti, John Slough, Akihisa Shimazu, MSNW LLC, USA

2015-69: PERFORMANCE AND PLUME CHARACTERIZATION OF THE BHT-1500 HALL THRUSTER, Kevin David Diamant, Thomas J. Curtiss, Rostislav Spektor, Edward J. Beiting, Vlad Hruby, Bruce Pote, Juraj Kolencik, Surjeet Paintal, The Aerospace Corporation, USA

2015-70: CHARACTERISTICS OF SIDE BY SIDE OPERATION OF HALL THRUSTER, Takeshi Miyasaka, Katsuo Asato, Daiki Furuta, Yudai Uyama, Ryota Goto, Daichi Shimizu, Mikoto Yoshida, Masahiro Sakoda, Yoshimi Miyake, Gifu University, Japan

2015-71: PLUME MODELING OF A TWO CAMILA HALL THRUSTER CLUSTER FOR THRUST VECTORING, Matteo Laterza, Moshe Guelman, Technion - Israel Institute of Technology, Israel

2015-73: PLUME STRUCTURE STUDY OF HOLLOW CATHODE IN BIAS VOLTAGE CONDITIONS, Qimeng Xia, Kan Xie, Xiangyang Liu, Zhiwen Wu, Ningfei Wang, Beijing Institute of Technology, China

2015-75: ATOMIC OXYGEN EFFECT TO PERFORMANCE OF THE HOLLOW CATHODE OF 20 MN ION THRUSTER, Inanaga Yasutaka, Oinuma Gaku, Ozaki Toshiyuki, Shuto Kazuo, Hayakawa Yukio, Nagano Hiroshi, MELCO, Japan

2015-77: INFLUENCE OF BACKGROUND MAGNETIC FIELD ON HOLLOW CATHODE DISCHARGE CHARACTERISTICS, Tianhang Meng, Zhongxi Ning, Daren Yu, Harbin Institute of Technology, China

2015-78: ABLATION AND IONIZATION PHENOMENON IN A TEFLON PULSED PLASMA THRUSTER, Lei Yang, Yuping Huang, Haibin Tang, Xiangyang Liu, Beijing Research Institute of Precise Mechatronic Controls, China

2015-79: INVESTIGATION OF DISCHARGE ARC PHENOMENA IN ABLATIVE PPT, Tony SchÃ¶nherr, Marcus Stein, Kimiya Komurasaki, Georg Herdrich, The University of Tokyo, Japan

2015-80: SHORT PULSE CHARACTERISTICS OF A LASER-ASSISTED PULSED PLASMA THRUSTER, Kota Matsubara, Hiroshi Hosokawa, Nao Akashi, Yuji Oigawa, Hideyuki Horisawa, Tokai University, Japan

2015-81: HIGH PULSE REPETITION FREQUENCY OPERATION OF LOW-POWER SHORT-PULSE PLASMA THRUSTER, Yuki Nakamura, Hideyuki Horisawa, Tokai University, Japan

2015-82: STUDY OF A COAXIAL VACUUM ARC THRUSTER PLUME AND ITS INTERACTION WITH APPLIED MAGNETIC FIELD, Manuel Jimenez Diaz, Laurent Garrigues, Gerjan J M Hagelaar, Freddy Gaboriau, Laurent Liard, Luc Herrero, Antoine Blanchet, University of Toulouse, France

2015-83: AN APPROACH FOR THRUST AND LOSSES IN INERTIAL ELECTROSTATIC CONFINEMENT DEVICES FOR ELECTRIC PROPULSION APPLICATIONS, G. Herdrich, C. Syring, T. Torgau, Y. Chan, D. Petkow, University of Stuttgart, Germany

2015-84: ANALYSIS OF VERY-LOW-POWER E X B DISCHARGE SEEDED BY VACUUM ARC PLASMA, Igal Kronhaus, Technion - Israel Institute of Technology, Israel

2015-87: A HIGH POWER ELECTRODELESS PLASMA THRUSTER OPERATED WITH A FET-BASED INVERTER POWER SUPPLY, Takayoshi Ishiyama, Aiki Chiba, Kazunori Takahashi, Atsushi Komuro, Akira Ando, Tohoku University, Japan

2015-88: IN-FLIGHT OPERATION OF THE DAWN ION PROPULSION SYSTEM-ARRIVAL AT CERES, Charles E Garner, Marc D Rayman, John Brophy, California Institute of Technology, USA

2015-89: OVERVIEW OF THE RESEARCH ACTIVITIES OF THE RITSAT-PROJECT, Peter J. Klar, Klaus Hannemann, Ubbo Ricklefs, Hans Leiter, Justus Liebig University, Germany

2015-90: EVOLUTION OF THE AIRBUS DS GMBH RADIO FREQUENCY ION THRUSTER FAMILY, Leiter Juergen Hans, Christian Altmann, Ralf Kukies, Juergen Kuhmann, Jan-Patrick Porst, Marcel Berger, Michael Rath, Airbus DS GmbH, Germany

2015-91: OVERVIEW OF RIT SIMULATION AREAS IN GIESSEN WITH FOCUS ON PLASMA SIMULATION, Robert Henrich, Michael Becker, Waldemar Gaertner, Kristof Holste, Christian Heiliger, Chris Volkmar, Justus-Liebig-University, Germany

2015-95: A RELATION BETWEEN FUEL-OPTIMAL LOW-THRUST TRAJECTORIES AND TWO-BODY ORBITS, Shengxian Yu, Changyin Zhao, Rongyu Sun, Wei Zhang, Hongbo Wang, Chinese Academy of Sciences, China

2015-96: INTEGRATION OF A ELECTRIC PROPULSION ORBIT TRANSFER OPTIMISER INTO A SPACECRAFT SIMULATOR (ESPSS -ECOSIMPRO^Â® EUROPEAN SPACE PROPULSION SYSTEM SIMULATION), Christophe R Koppel, KopooS Consulting ind., France

2015-97: ELECTRIC PROPULSION FOR STATION KEEPING AND ELECTRIC ORBIT RAISING ON EUTELSAT PLATFORMS, Cosmo Casaregola, Eutelsat, France

2015-98: ELECTRIC PROPULSION MODULE FOR THE EXTENSION OF VEGA LAUNCH VEHICLE PAYLOAD CAPABILITY, Gianluca Ascanio, Tommaso Fossati, Mauro Federici, Marco Pizzarelli, Davide Nicolini, CGS SpA Compagnia Generale per lo Spazio, Italy

2015-99: PLAS-40 DEVELOPMENT STATUS: NEW RESULTS, Mira Potapenko, Vladimir Gopanchuk, Sergey Olotin, EDB Fakel, Russia

2015-100: MAGNETICALLY SHIELDED MINIATURE HALL THRUSTER: DESIGN IMPROVEMENT AND PERFORMANCE ANALYSIS, Ryan Conversano, Dan Goebel, Richard Hofer, Ioannis Mikellides, Ira Katz, Richard Wirz, University of California Los Angeles, USA

2015-102: SITAEL LOW POWER HALL EFFECT THRUSTERS FOR SMALL SATELLITES, Tommaso Misuri, Cosimo Ducci, Riccardo Albertoni, Mariano Andrenucci, Daniela Pedrini, Sitael S.p.A., Italy

2015-103: WALL MATERIAL SELECTION PROCESS FOR CAM200 LOW POWER HALL THRUSTER, Raanan Eytan, Dan Lev, Gal Alon, Abraham Warshavsky, Alexander Kapulkin, Maxim Rubanovitz, Rafael - Advanced Defense Systems Ltd., Israel

2015-105: THE EXPERIMENTAL STUDY ON ELECTRON BEAM EXTRACTION FROM ECR NEUTRALIZER, Juan Yang, Yizhou Jin, Litao Luo, Yuquan Wang, Hei Liu, Northwestern Polytechnic University, China

2015-106: PRELIMINARY MEASUREMENTS OF TIME-RESOLVED ION VELOCITY DISTRIBUTIONS NEAR A HOLLOW CATHODE, Marcel Pierre Georgin, Christopher Durot, Alec Gallimore, University of Michigan, USA

2015-108: EXPERIMENTAL STUDY OF THE EFFECTS OF DIFFERENT DESIGN PARAMETERS ON THE PLASMA CHARACTERISTICS AND THE EXTRACTED CURRENT OF A PROTOTYPE RADIO-FREQUENCY PLASMA CATHODE, Sina Jahanbakhsh, Murat Celik, Bogazici University, Turkey

2015-109: PLASMA BEHAVIOURS AND MAGNETIC FIELD DISTRIBUTIONS OF A SHORT-PULSE LASER-ASSISTED PULSED PLASMA THRUSTER, Nao Akashi, Moriya Hiroto, Yuji Oigawa, Hiroshi Hosokawa, Hideyuki Horisawa, Tokai Univertsity, Japan

2015-112: STUDY ON THE THERMAL RADIATION MECHANISM IN PULSED PLASMA THRUSTER, Siyu Wang, Xiangyang Liu, Zhiwen Wu, Kan Xie, Yue Cheng, Ningfei Wang, Beijing Institute of Technology, China

2015-114: PROOF-OF-CONCEPT DEMONSTRATION OF THE PEGASES PLASMA THRUSTER, Trevor Alain Lafleur, Dmytro Rafalskyi, Pascal Chabert, Ane Aanesland, Ecole Polytechnique, France

2015-115: A DIRECT WAVE-DRIVE THRUSTER USING THE MAGNETOSONIC MODE , Matthew Solomon Feldman, Benjamin Jorns, Edgar Choueiri, Princeton University, USA

2015-116: ALTERNATIVE NEUTRALIZATION TECHNIQUE FOR A 40 WATT QUAD CONFINEMENT THRUSTER, Thomas Harle, Tarek Ahmed, Aaron Kombai Knoll, University of Surrey, UK

2015-117: COLLISIONLESS ELECTRON COOLING ON MAGNETIZED PLASMA EXPANSIONS: ADVANCES ON MODELLING, Jaume Navarro-Cavalle, Sara Correyero, Eduardo Ahedo, Universidad Politecnica de Madrid, Spain

2015-119: ION-EMITTERS FOR POTENTIAL MICRO-THRUSTER APPLICATIONS, Daniel Reppin, Florian Kuhl, Torsten Henning, Peter J Klar, Juergen Janek, Justus Liebig University, Germany

2015-120: COLLOID EMITTERS IN PHOTOSTRUCTURABLE POLYMER TECHNOLOGY: FABRICATION AND CHARACTERIZATION PROGRESS REPORT, Katharina Huhn, Torsten Henning, Peter J Klar, Stefan Hengsbach, Justus Liebig University, Germany

2015-121: NANOFEEP ON UWE PLATFORM - FORMATION FLYING OF CUBESATS USING MINIATURIZED FIELD EMISSION ELECTRIC PROPULSION THRUSTERS, Daniel Bock, Alexander Kramer, Philip Bangert, Klaus Schilling, Martin Tajmar, Technische Universitaet Dresden, Germany

2015-123: TESTING AND MODELLING OF THE MN-FEEP START-UP PERFORMANCE, Alexander M Reissner, Nembo Buldrini, Bernhard Seifert, Thomas Horbe, Florin Plesescu, Jose Gonzalez Del Amo, Luca Massotti, FOTEC Forschungs- und Technologietransfer GmbH, Austria

2015-124: BUSEK BHT-1500 EXTERNAL VS CENTER CATHODE EMC STUDY, Edward Beiting, William Cox, Kevin Diamant, Rostislav Spektor, Bruce Pote, Vlad Hruby, The Aerospace Corporation, USA

2015-125: 30-KW PERFORMANCE OF A 100-KW CLASS NESTED-CHANNEL HALL THRUSTER, Scott James Hall, Sarah E Cusson, Alec D Gallimore, University of Michigan, USA

2015-126: INVESTIGATION OF A 5 KW CLASS HALL-EFFECT THRUSTER OPERATING WITH DIFFERENT XENON-KRYPTON MIXTURES, Cosimo Ducci, Tommaso Andreussi, Alexey Arkhipov, Andrea Passaro, Mariano Andrenucci, Alexandra Bulit, Clive Edwards, Sitael S.p.A., Italy

2015-127: END-TO-END TESTING OF THE PPS^Â®5000 HALL THRUSTER SYSTEM WITH A 5-KW POWER PROCESSING UNIT, Olivier B Duchemin, David Le Mehaute, Michael Oberg, Xavier Cavelan, Matthias Guilhem-Ducleon, Gael Khimeche, Frederic Payot, Laurent Soubrier, Denis Galiana, Guillaume Glorieux, Snecma, Safran Group, France

2015-130: RING CUSP ION ENGINE DEVELOPMENT IN THE UK, Michele Coletti, Neil Wallace, Stephen Gabriel, Daniele Frollani, Huw Simpson, Mars Space Ltd, UK

2015-131: QINETIQ’S T6 AND T5 ION THRUSTER ELECTRIC PROPULSION SYSTEM ARCHITECTURES AND PERFORMANCES, Mark Hutchins, Huw Simpson, Javier Jimenez, QinetiQ, UK

2015-132: QUALIFICATION OF THE T6 THRUSTER FOR BEPICOLOMBO, Rhodri A. Lewis, J. Perez Luna, N. Coombs, F. Guarducci, QinetiQ, UK

2015-133: 7500-HOUR LIFE TEST OF THE QM LIPS-200 ION THRUSTER, Tianping Zhang, Wei Meng, Hai Geng, Weiwen Zhang, Yang Hao, Lanzhou Institute of Physics, China

2015-134: MITIGATION OF ENERGETIC IONS AND KEEPER EROSION IN A HIGH-CURRENT HOLLOW CATHODE, Benjamin Alexander Jorns, Ioannis G. Mikellides, Dan M. Goebel, Alejandro Lopez Ortega, California Institute of Technology, USA

2015-137: MEASUREMENTS OF TRANSPORT DUE TO LOW FREQUENCY OSCILLATIONS IN A ROTATING HOLLOW CATHODE PLASMA, Taylor S Matlock, Christopher A Dodson, Dan M Goebel, Richard E Wirz, University of California Los Angeles, USA

2015-138: INFLUENCE OF ELECTRODE CONFIGURATION OF A LIQUID PROPELLANT PPT ON ITS PERFORMANCE, Kinya Miyagi, Kuroki Shotaro, Tagawa Takeru, Masui Soichi, Kakami Akira, Tachibana Takeshi, Kyushu Institute of Technology, Japan

2015-139: USE OF LIQUID PROPELLANTS IN PULSED PLASMA THRUSTERS FOR SMALL SATELLITES, William Yeong Liang Ling, Hiroyuki Koizumi, Tony SchÃ¶nherr, The University of Tokyo, Japan

2015-140: DISCHARGE CHARACTERISTICS OF A GAS-FED SHORT-PULSE PLASMA THRUSTER, Hiroshi Hosokawa, Nao Akashi, Kouta Matsubara, Haruna Hasegawa, Yuji Oigawa, Hideyuki Horisawa, Tokai University, Japan

2015-141: TIME-OF-FLIGHT SPECTROMETRY AND PERFORMANCE OF A PULSED PLASMA THRUSTER WITH NON-VOLATILE PROPELLANT, Serge Barral, Jacek Kurzyna, Agnieszka Szelecka, Hubert Rachubiński, Dariusz Daniłko, Martin Ricardo, E. Remirez, Pablo Ortiz, J. Alonso, Yann Mabillard, S. Bottinelli, Ana Zaldivar, P. Rangsten, Christophe Koppel, QuinteScience, Poland

2015-142: A LASER-ELECTROSTATIC HYBRID THRUSTER, Ryo Edamura, Akihiro Osamura, Kenta Hara, Hideyuki Horisawa, University of Tokai, Japan

2015-143: LOW-NOISE THRUST GENERATION BY LASER-ABLATIVE MICROPROPULSION, Stefan Scharring, Stephanie Karg, Raoul-Amadeus Lorbeer, Nancy Dahms, Hans-Albert Eckel, German Aerospace Center (DLR), Germany

2015-144: ASSESSMENT OF AN INTERSTELLAR PHOTON PROPULSION CONCEPT, John E Sinko, Tyler R Baxter, Saint Cloud State University, USA

2015-145: A FEASIBILITY AND DESIGN STUDY OF UTILIZING HIGH-POWERED LASERS FOR MPD THRUSTERS, Thomas Charles Millen, American Military University, USA

2015-146: DEVELOPMENT OF AN ALTERNATING ELECTRIC FIELD ACCELERATOR FOR LASER-ABLATION PLASMA ACCELERATION, Akihiro Osamura, Ryo Edamura, Kenta Hara, Hideyuki Horisawa, Tokai University, Japan

2015-148: THRUST MEASUREMENTS OF ION ELECTROSPRAY THRUSTERS USING A CUBESAT COMPATIBLE MAGNETICALLY LEVITATED THRUST BALANCE, Fernando Mier-Hicks, Paulo Lozano, Massachusetts Institute of Technology, USA

2015-149: DESIGN AND CHARACTERIZATION OF A SCALABLE ION ELECTROSPRAY PROPULSION SYSTEM, David Krejci, Fernando Mier-Hicks, Corey Fucetola, Paulo Lozano, Andrea Hsu Schouten, Francois Martel, Massachusetts Institute of Technology, USA

2015-151: RESEARCH AND DEVELOPMENT OF HIGH-POWER, HIGH-SPECIFIC-IMPULSE MAGNETIC-LAYER-TYPE HALL THRUSTERS FOR MANNED MARS EXPLORATION, Yuya Takahata, Tomoyuki Ikeda, Masato Nishida, Taisuke Kagota, Tetsuo Kakuma, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-152: EFFECTS OF BACKGROUND PRESSURE ON THE NASA 173M HALL CURRENT THRUSTER PERFORMANCE, William Tighe, Rostislav Spektor, Kevin Diamant, Hani Kamhawi, The Aerospace Corporation, USA

2015-153: PERFORMANCE CHARACTERISTICS OF HIGH-POWER, HIGH-SPECIFIC-IMPULSE ANODE-LAYER-TYPE HALL THRUSTERS FOR IN-SPACE PROPULSION, Taisuke Kagota, Yuya Takahata, Tetsuo Kakuma, Masato Nishida, Tomoyuki Ikeda, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-154: EXPERIMENTAL STUDY OF A HIGH SPECIFIC IMPULSE PLASMA THRUSTER PLAS-120CM, Mira Potapenko, Vladimir Gopanchuk, Denis Merkuriev, Pavel Smirnov, EDB Fakel, Russia

2015-155: WEAR TESTING OF A MAGNETICALLY SHIELDED HALL THRUSTER AT 2000 S SPECIFIC IMPULSE, Michael James Sekerak, Richard R Hofer, James E Polk, Benjamin A Jorns, Ioannis G Mikellides, Jet Propulsion Laboratory, USA

2015-156: TEST PROCEDURE FOR LOCALLY ASSESSING POTENTIAL RISKS OF SPUTTER DAMAGE DUE TO THRUSTER PLUMES, Markus Piechotka, Kristof Holste, Torsten Henning, Klaus Hannemann, Peter J Klar, Vladislav V Nigmatzyanov, Andreas Neumann, Justus Liebig University, Germany

2015-157: EFFECT OF PLASMA PLUME ON CUBESAT STRUCTURES AS A FUNCTION OF THRUST VECTORING, Andrew Davis Hine, Kristina Lemmer, Western Michigan University, USA

2015-159: INVESTIGATION OF ELECTRON EXTRACTION FROM A MICROWAVE DISCHARGE NEUTRALIZER FOR A MINIATURE ION PROPULSION SYSTEM, Yoshinori Takao, Hiroyuki Koizumi, Yusuke Kasagi, Kimiya Komurasaki, Yokohama National University, Japan

2015-160: BACKFLOW OF CHARGED PARTICLES ONTO A SPACECRAFT IN OPERATION OF ION THRUSTERS UNDER LACK OF THE NEUTRALIZATION, Takanobu Muranaka, Kento Hoshi, Hirotsugu Kojima, Hiroshi Yamakawa, Satoshi Hosoda, Kazutaka Nishiyama, Chukyo University, Japan

2015-163: DEVELOPMENT OF A LOW CURRENT HEATERLESS HOLLOW CATHODE FOR HALL THRUSTERS, Dan Lev, Gal Alon, Dima Mikitchuk, Leonid Appel, RAFAEL - Advanced Defense Systems, Israel

2015-164: CONCEPTUAL DESIGN OF A RADIATIVE COOLING SYSTEM FOR HEATERLESS HOLLOW CATHODES, Daniel Katz Franco, Dan Lev, Israel institute of Technology, Israel

2015-166: 1-A CLASS MICROWAVE DISCHARGE CATHODE USING IMPREGNATED TUNGSTEN, Yoshitaka Tani, Ryudo Tsukizaki, Daiki Koda, Satoshi Hosoda, Hitoshi Kuninaka, The University of Tokyo, Japan

2015-168: ACCELERATION OF A PLASMA FLOW IN A MAGNETIC LAVAL NOZZLE APPLIED TO AN MPD THRUSTER, Yohei Kobayashi, Kiyotaka Suzuki, Hiroaki Nabuchi, Atsushi Komuro, Kazunori Takahashi, Akira Ando, Tohoku University, Japan

2015-169: APPLIED-FIELD MPD THRUSTER WITH MAGNETIC-CONTOURED ANODES, Tatsuya Kimura, Kohei Kojima, Masaaki Yasui, Daisuke Ichihara, Tomoki Uno, Hisashi Kataoka, Akira Iwakawa, Akihiro Sasoh, Shigeru Yokota, Mitsubishi Heavy Industries, Ltd, Japan

2015-171: OPERATION CHARACTERISTICS OF SMALL-DC-CURRENT, APPLIED-FIELD MPD THRUSTER, Daisuke Ichihara, Tomoki Uno, Hisashi Kataoka, Akira Iwakawa, Akihiro Sasoh, Nagoya University, Japan

2015-172: IMPROVED TARGET METHOD FOR AF-MPDT THRUST MEASUREMENT, Baojun Wang, Haibin Tang, Wenjiang Yang, Mengdi Kong, Yujie Xu, Beihang University, China

2015-173: THRUST GENERATION OF LASER ABLATION IN HELIUM AND ARGON AMBIENT GASES WITH REPETITIVE LASER PULSES, Bin Wang, Hisashi Tsuruta, Zhongyuan Wang, Akihiro Sasoh, Nagoya University, Japan

2015-174: STUDY OF LASER-SUPPORTED DETONATION THRESHOLD USING GRAPHICAL ANALYSIS, Shiraishi Hiroyuki, Matsumoto Yuji, Daido University, Japan

2015-175: SIMULATION OF LSD WAVE CHARACTERISTICS IN AR AND N₂ USING A 1-D LASER-INDUCED DISCHARGE MODEL COUPLED WITH HYDRODYNAMIC RELATIONS FOR LASER-PROPELLED THRUSTER STUDIES, Joseph Ampadu Ofosu, Kohei Matsui, Kimiya Komurasaki, Kohei Shimamura, Hiroyuki Koizumi, The University of Tokyo, Japan

2015-176: THRUST PERFORMANCE OF MICROWAVE ROCKET AT LOW AMBIENT PRESSURE, Masayuki Takahashi, Naofumi Ohnishi, Tohoku University, Japan

2015-177: ACCELERATION OF A PROJECTILE WITH A HIGH-POWER LASER-PRODUCED MAGNETIC FIELD, Taichi Morita, Saito Naoya, Ryosuke Kawashima, Yamamoto Naoji, Nakashima Hideki, Shinsuke Fujioka, Kyushu University, Japan

2015-178: ELECTRICAL DOUBLE LAYERS IN ELECTROSPRAY PROPULSION, Kento Masuyama, Paulo Lozano, Massachusetts Institute of Technology, USA

2015-179: THE EFFECTS OF METASTABLE SOLVATED IONS ON ELECTROSPRAY ION THRUSTER EFFICIENCY, Catherine Miller, Paulo Lozano, Massachusetts Institute of Technology, USA

2015-182: OPTIMIZATION OF THE DESIGN OF A WALL-LESS HALL THRUSTER, Stephane Mazouffre, Tsikata Vaudolon, Sedina Tsikata, C. Henaux, D. Harribey, A. Rossi, CNRS, France

2015-183: DESIGN OF VARIABLE GEOMETRY MEDIUM POWER HALL THRUSTER, Brendan Plecque, Mark Crofton, Kevin Diamant, Rostislav Spektor, Jason Young, William Cox, A. Hubble, The Aerospace Corporation, USA

2015-185: DEVELOPMENT OF PERMANENT MAGNET HALL THRUSTERS FOR APPLICATIONS ON FUTURE BRAZILIAN SPACE MISSIONS, Jose Leonardo Ferreira, Alexandre A Martins, Ernesto G Costa, Helbert O C Junior, Lui T C Habl, Lais S Souza, Artur C B Serra, Felipe O Nathan, Paolo Gessini, Rodrigo M Miranda, Adriane Schellin, University of Brasilia, Brazil

2015-186: DEVELOPMENT APPROACH AND STATUS OF THE 12.5 KW HERMES HALL THRUSTER FOR THE SOLAR ELECTRIC PROPULSION TECHNOLOGY DEMONSTRATION MISSION, Richard Robert Hofer, Hani Kamhawi, Daniel Herman, James Polk, John Snyder, Ioannis Mikellides, Wensheng Huang, James Myers, John Yim, George Williams, Alejandro Ortega, Benjamin Jorns, Michael Sekerak, Christopher Griffiths, Rohit Shastry, Thomas Haag, Timothy Verhey, Bradley Gilliam, Ira Katz, Dan Goebel, John Anderson, James Gilland, Lauren Clayman, California Institute of Technology, USA

2015-187: GRID WEAR ANALYSIS OF A MINIATURE ION ENGINE, Masakatsu Nakano, Hiroyuki Koizumi, Tokyo Metropolitan College of Industrial Technology, Japan

2015-188: THREE-DIMENSIONAL ANALYSIS OF ION OPTICS WITH DEVIATION OF THE APERTURES GEOMETRY FROM AXIAL SYMMETRY, Andrey A. Shagayda, Keldysh Research Centre, Russia

2015-192: 100 A CLASS HOLLOW CATHODE, Shigeru Yokota, Kojima Kohei, Kimura Tatsuya, Kataoka Hisashi, Sasoh Akihiro, University of Tsukuba, Japan

2015-193: INVESTIGATION OF HEATERLESS HOLLOW CATHODE BREAKDOWN, Alexander Daykin-Iliopoulos, Steve Gabriel, Igor Golosnoy, Kenichi Kubota, Ikkoh Funaki, University of Southampton, UK

2015-194: PERFORMANCE EVALUATION OF RADIO FREQUENCY PLASMA CATHODE FOR HALL EFFECT THRUSTER, Hiroki Watanabe, Takanori Deguchi, Chisato Ota, Jun Sato, Shuka Takeda, Yuki Miura, Yuki Sato, Masanori Ichimura, Haruki Takegahara, Tokyo Metropolitan University, Japan

2015-197: PERFORMANCE CHARACTERISTICS OF STEADY-STATE MPD THRUSTERS WITH PERMANENT MAGNETS AND MULTI HOLLOW CATHODES FOR MANNED MARS EXPLORATION, Tomoya Suzuki, Norihide Koyama, Yoshikazu Sugiyama, Hisao Sakoda, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-198: THERMAL CHARACTERISTICS OF RADIATION-COOLED STEADY-STATE MPD THRUSTERS WITH PERMANENT MAGNETS AND MULTI HOLLOW CATHODES FOR IN-SPACE PROPULSION, Yoshikazu Sugiyama, Norihide Koyama, Tomoya Suzuki, Hisao Sakoda, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-199: DYNAMIC RESISTANCE PROBE FOR THE MEASUREMENT OF THE MASS DEPOSITION RATE FROM A CONDENSIBLE PROPELLANT THRUSTER, William J. Coogan, Michael A. Hepler, Edgar Y. Choueiri, Princeton University, USA

2015-200: NUMERICAL STUDY ON DIFFUSION EFFECTS IN MAGNETOPLASMADYNAMIC ARCJET THRUSTERS, Arsad Quraishi, Amit Kumar, M. Mahendhran, Indian Institute of Technology Madras, India

2015-201: PLASMA FLOW SIMULATION OF AN MPD THRUSTER WITH AN ELECTRODE MODEL, Akira Kawasaki, Kenichi Kubota, Ikkoh Funaki, Yoshihiro Okuno, Tokyo Institute of Technology, Japan

2015-202: MODELING OF ELASTIC COLLISIONS BETWEEN HIGH ENERGY AND SLOW NEUTRAL ATOMS, Samuel Jun Araki, Richard Edward Wirz, Edwards Air Force Base, USA

2015-203: BENCHMARKS FOR MAGNETIC FIELD ALIGNED MESHES IN ELECTROMAGNETIC PLASMA THRUSTER SIMULATIONS, Daniel Perez-Grande, O. Gonzalez-Martinez, Pablo Fajardo, Eduardo Ahedo, Universidad Carlos III de Madrid, Spain

2015-206: HYBRID MODELING OF A HALL THRUSTER USING HYPERBOLIC SYSTEM OF ELECTRON CONSERVATION LAWS, Rei Kawashima, Kimiya Komurasaki, Tony SchÃ¶nherr, Hiroyuki Koizumi, The University of Tokyo, Japan

2015-207: FLOWFIELD SIMULATION AND PERFORMANCE PREDICTION OF ELECTROTHERMAL PULSED PLASMA THRUSTERS ONBOARD OSAKA INSTITUTE OF TECHNOLOGY PROITERES NANO-SATELLITE SERIES, Ryota Fujita, Rikio Muraoka, Keita Kanaoka, Chen Huanjun, Masato Tanaka, Hirokazu Tahara, Takashi Wakizono, Osaka Institute of Technology, Japan

2015-208: QUALIFICATION OF A PULSED PLASMA THRUSTER FOR CUBESAT PROPULSION (PPTCUP), Simone Ciaralli, Michele Coletti, Stephen B Gabriel, Mars Space Ltd., UK

2015-209: R&D AND FINAL OPERATION OF OSAKA INSTITUTE OF TECHNOLOGY 1ST PROITERES NANO-SATELLITE WITH ELECTROTHERMAL PULSED PLASMA THRUSTERS AND DEVELOPMENT OF 2ND AND 3RD SATELLITES, Takuya Kamimura, Yoshifumi Nishimura, Tomoyuki Ikeda, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-212: THEORETICAL INVESTIGATION OF A 5 KW CLASS HALL EFFECT THRUSTER, Vittorio Giannetti, Andrea Leporini, Tommaso Andreussi, Mariano Andrenucci, Sitael S.p.A., Italy

2015-213: THRUST PERFORMANCE IN HALL THRUSTER WITH PULSATING OPERATION, Naoji Yamamoto, Takumi Ito, Haruki Takegahara, ,Hiroki Watanabe, Kyoichi Kuriki, Taichiro Tamida, Hiroyuki Osuga, Kyushu University, Japan

2015-215: DEVELOPMENT AND PERFORMANCE CHARACTERIZATION OF A 5 KW CLASS HALL-EFFECT THRUSTER, Cosimo Ducci, Alexey Arkhipov, Mariano Andrenucci, Sitael S.p.A., Italy

2015-217: PERFORMANCE EVALUATION OF TAL-TYPE HALL THRUSTER WITH RF PLASMA CATHODE, Hiroki Watanabe, Yuki Miura, Masanori Ichimura, Takanori Deguchi, Shuka Takeda, Chisato Ota, Haruki Takegahara, Tokyo Metropolitan University, Japan

2015-218: INVESTIGATION OF THE GEOMETRY CONFIGURATION VARIATIONS ON THE PERFORMANCE OF ION THRUSTER GRIDS WITH PIC-DSMC SIMULATIONS, Emre Turkoz, Firat Sik, Murat Celik, Bogazici University, Turkey

2015-219: EXPERIMENTAL INVESTIGATION OF PARTICLES FLUXES TO THE GRID SURFACES INSIDE ION OPTIC SYSTEMS, Maria Smirnova, Sergey Khartov, Davar Feili, Moscow Aviation Institute, Russia

2015-220: SIMULATION OF THE QINETIQ T6 ENGINE ION OPTICS AND COMPARISON TO THE EXPERIMENTAL DATA, Michele Coletti, Mars Space Ltd, UK

2015-221: MOLYBDENUM LIF AND NEXT EROSION RATE, Mark Crofton, Michael Patterson, The Aerospace Corporation, USA

2015-222: PLUME PLASMA MEASUREMENTS OF A 20-CM XENON ION THRUSTER USING A MULTIPLE-PROBE ARRAY, Zun Zhang, Haibin Tang, Jue Wang, Min Wang, Zheng Wen, Beihang University, China

2015-224: POWER PROCESSING UNIT ACTIVITIES AT THALES ALENIA SPACE BELGIUM (ETCA), Eric Bourguignon, Stephane Fraselle, Thierry Scalais, Jean-Marc Defise, Thales Alenia Space Belgium, Belgium

2015-225: POWER PROCESSING UNITS - ACTIVITIES IN EUROPE 2015, Matthias K.H. Gollor, Andreas Franke, Ulrich Schwab, Waldemar Dechent, Guillaume Glorieux, Michael Boss, Nicoletta Wagner, Javier Palencia, Paolo Galantini, Giovanni Tuccio, Eric Bourguignon, ESA, The Netherlands

2015-226: DEVELOPMENT OF A LOW PRESSURE SELF-PROPELLED VAPOR SUPPLY SUBSYSTEM FOR ELECTRIC PROPULSION, Hou-Yi Lee, Koichi Ushio, Naoji Yamamoto, Hideki Nakashima, Kyushu University, Japan

2015-229: PERFORMANCE CHARACTERISTICS OF LOW-POWER ARCJET THRUSTERS USING LOW-TOXICITY PROPELLANTS OF HAN, Yuki Fukutome, Suguru Shiraki, Kazuma Matsumoto, Fumihiro Inoue, Hirokazu Tahara, Yuichiro Nogawa, Ai Momozawa, Osaka Institute of Technology, Japan

2015-230: PERFORMANCE CHARACTERISTICS OF LOW-POWER ARCJET THRUSTER SYSTEMS WITH GAS GENERATORS FOR WATER, Suguru Shiraki, Yuki Fukutome, Fumihiro Inoue, Kazuma Matsumoto, Hirokazu Tahara, Yuichiro Nogawa, Ai Momozawa, Osaka Institute of Technology, Japan

2015-231: PERFORMANCE AND THERMAL CHARACTERISTICS OF HIGH-POWER HYDROGEN ARCJET THRUSTERS WITH RADIATION-COOLED ANODES FOR IN-SPACE PROPULSION, Fumihiro Inoue, Yuki Fukutome, Suguru Shiraki, Kazuma Matsumoto, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-232: AN AL-WATER FED DC ARCJET, Naoto Yanagida, Makoto Ohata, Hideyuki Horisawa, Akira Kobayashi, Tokai University, Japan

2015-234: CHARACTERIZATION OF CORONA IONIZATION BASED MICROTHRUSTERS, William Patrick Wright, Philippe Ferrer, University of the Witwatersrand, South Africa

2015-235: FULL ION VELOCITY DISTRIBUTION FUNCTION MEASUREMENT IN AN ELECTRIC THRUSTER, USING LIF-BASED TOMOGRAPHIC RECONSTRUCTION, Paul-Quentin Elias, Julien Jarrige, E. Cucchetti, Denis Packan, Alexandra Bulit, ONERA, France

2015-236: MEASUREMENT OF FORCES DUE TO SPUTTERING OF SOLID SURFACES, Alexander Spethmann, Thomas Trottenberg, Holger Kersten, University of Kiel, Germany

2015-237: EXPERIMENTAL VAPORIZATION AND COMPUTATIONAL MODELING OF IONIZATION OF HYDROXYLAMMONIUM NITRATE IN VACUUM CONDITIONS, Forrest G. Kidd, III, Matthew J. Baird, Greg Neff, Kristina Lemmer, Western Michigan University, USA

2015-240: PARTICLE-IN-CELL SIMULATION OF A MICRO ECR PLASMA THRUSTER, Ueno Keisuke, Mori Daisuke, Takao Yoshinori, Eriguchi Koji, Ono Kouichi, Kyoto University, Japan

2015-242: EXPERIMENTAL GEOMETRY INVESTIGATION OF A COAXIAL ECR PLASMA THRUSTER, Felix Cannat, Julien Jarrige, Trevor Lafleur, Paul-Quentin Elias, Denis Packan, ONERA, France

2015-243: INITIAL OPERATION OF THE CUBESAT AMBIPOLAR THRUSTER, J. P. Sheehan, Timothy A Collard, Frans H. Ebersohn, Benjamin W Longmier, University of Michigan, USA

2015-244: A COMPACT HELICON THRUSTER FOR CUBESAT APPLICATIONS, David Biggs, Sam Avery, Luke Raymond, Wei Liang, Nicolas Gascon, Andrea Fabris, Juan Rivas, Mark Cappelli, Stanford University, USA

2015-245: DEVELOPMENT OF NOVEL MINIATURE MICROWAVE DISCHARGE THRUSTER, Koichi Ushio, Yuji Toyoda, Naoji Yamamoto, Taichi Morita, Hideki Nakashima, Kyushu University, Japan

2015-246: EXPERIMENTAL INVESTIGATION OF THE NEAR-WALL REGION IN THE NASA HIVHAC EDU2 HALL THRUSTER, Rohit Shastry, Hani Kamhawi, Wensheng Huang, and Thomas Haag, NASA Glenn Research Center, USA

2015-247: INVESTIGATION OF THE "BACK" AND "RADIAL" ION FLOWS IN THE VICINITY OF THE STATIONARY PLASMA THRUSTER EXIT PLANE, Vladimir Kim, Alexey Arkhipov, Alexander Bishaev, Denis Merkurev, Alexander Pogorelov, Garri Popov, Moscow Aviation Institute, Russia

2015-249: HALL2DE NUMERICAL SIMULATIONS FOR THE ASSESSMENT OF POLE EROSION IN A MAGNETICALLY SHIELDED HALL THRUSTER, Alejandro Lopez Ortega, Ioannis G Mikellides, Ira Katz, Jet Propulsion Laboratory, USA

2015-250: SIMULATION OF A NESTED CHANNEL HALL THRUSTER, Dragnea C. Horatiu, Boyd D. Iain, University of Michigan, USA

2015-251: PARTICLE SIMULATION OF HIGH SPECIFIC IMPULSE OPERATION OF LOW-EROSION MAGNETIC LAYER TYPE HALL THRUSTERS, Shinatora Cho, Hiroki Watanabe, Kenichi Kubota, Shigeyasu Iihara, Kenji Fuchigami, Kazuo Uematsu, Ikkoh Funaki, JAXA, Japan

2015-252: HYBRID-PIC MODELING OF THE TRANSPORT OF ATOMIC BORON IN A HALL THRUSTER, Brandon Denis Smith, Iain Boyd, Hani Kamhawi, University of Michigan, USA

2015-254: HALL2DE SIMULATIONS OF A 12.5-KW MAGNETICALLY SHIELDED HALL THRUSTER FOR THE NASA SOLAR ELECTRIC PROPULSION TECHNOLOGY DEMONSTRATION MISSION, Ioannis G. Mikellides, Alejandro Lopez Ortega, Richard R. Hofer, James E. Polk, Hani Kamhawi, John T. Yim, James Myers, Jet Propulsion Laboratory, USA

2015-255: PARAMETRIC UNCERTAINTY ANALYSIS OF A HALL THRUSTER THROUGH A FULLY KINETIC CODE, Burak Karadag, Shinatora Cho, Ikkoh Funaki, The Graduate University for Advanced Studies, Japan

2015-256: A NEW THRUST MEASUREMENT METHOD FOR EVALUATING HIGHER FREQUENCY VARIATION BY APPLYING ACCELERATION MEASUREMENT TO NULL-BALANCE METHOD, Kakami Akira, Kashihara Kenji, Takeshida Shota, Yano Yasuyuki, University of Miyazaki, Japan

2015-257: LOW DRIFT THRUST BALANCE WITH HIGH RESOLUTION, Hans-Peter Harmann, Heiko Dartsch, Ellen Werner, AST Advanced Space Technologies GmbH, Germany

2015-258: VERIFICATION OF THE FOTEC μN THRUST BALANCE AT THE ESA PROPULSION LAB, Bernhard Seifert, Alexander Reissner, Nembo Buldrini, Thomas Hoerbe, Florin Plesescu, Alexandra Bulit, Eduard Bosch Borras, FOTEC Forschungs- und Technologietransfer GmbH, Austria

2015-259: ISO17025 ACCREDITATION OF THE ESA MICRO-NEWTON THRUST BALANCE, Eduard Bosch Borras, Jose Gonzalez Del Amo, Ben Hughes, ESA, The Netherlands

2015-260: DEVELOPMENT OF A HIGHLY SENSITIVE MICRO-NEWTON THRUST BALANCE: CURRENT STATUS AND LATEST RESULTS, Franz Georg Hey, Christian Altmann, Marcel Berger, Ewan Fitzsimons, Claus Braxmaier, Martin Tajmar, Dennis Weise, Ulrich Johann, Airbus Defence and Space, Germany

2015-261: PERFORMANCE OF A TORSIONAL THRUST STAND WITH 1 μN SENSITIVITY, Andrea Grace Hsu, Edward Beiting, Thomas Curtiss, The Aerospace Corporation, USA

2015-265: A THERMO-FLUIDIC MODEL FOR A LOW POWER XENON RESISTOJET, Federico Romei, Angelo N Grubisic, Dave Gibbon, Oliver Lane, Remi A. Herfort, Graham T. Roberts, University of Southampton, UK

2015-266: GLOBAL ENERGY TRANSFER MODEL OF MICROWAVE INDUCED PLASMA IN A MICROWAVE ELECTROTHERMAL THRUSTER RESONANT CAVITY, Mehmet Serhan Yildiz, Murat Celik, Turkish Air Force Academy, Turkey

2015-268: CHARACTERIZATION OF AIR BREATHING PLASMA THRUSTERS FUELLED BY ATMOSPHERIC MIXTURES ENCOUNTERED IN EARTH ATMOSPHERE AT AN ALTITUDE OF ABOUT 200 KM, Konstantinos Katsonis, Chloe Berenguer, Jose Gonzalez Del Amo, DEDALOS Ltd., Greece

2015-269: AIR-INTAKE DESIGN INVESTIGATION FOR AN AIR-BREATHING ELECTRIC PROPULSION SYSTEM, Francesco Romano, Tilman Binder, Georg Herdrich, Stefanos Fasoulas, Tony SchÃ¶nherr, University of Stuttgart, Germany

2015-270: STUDY OF AIRBREATHING ELECTRIC THRUSTER FOR NEARSPACE PROPULSION, Pan Chen, Zhiwen Wu, Xiangyang Liu, Kan Xie, Ningfei Wang, Ying Meng, Jiting Ouyang, Beijing Institute of Technology, China

2015-271: CONCEPTUAL DESIGN OF AN AIR-BREATHING ELECTRIC PROPULSION SYSTEM, Serge Barral, Gianluca Cifali, Riccardo Albertoni, Mariano Andrenucci, Louis Walpot, QuinteScience, Poland

2015-272: FIRST EXPERIMENTS TOWARDS AN ATMOSPHERE-BREATHING PPT, Tony SchÃ¶nherr, Gakuto Han, Caglayan Gurbuz, Hiroyuki Koizumi, Kimiya Komurasaki, The University of Tokyo, Japan

2015-273: IODINE-FUELED MINI RF ION THRUSTER FOR CUBESAT APPLICATIONS, Michael Tsay, John Frongillo, Kurt Hohman, Busek Co. Inc., USA

2015-274: THE RIT-μX MINIATURIZED ION ENGINE SYSTEM WAY TO TRL 5 FOR AN EXTENDED THRUST RANGE, Christian Altmann, Hans Leiter, Ralf Kukies, Airbus DS GmbH, Germany

2015-275: MINIATURE ION THRUSTERS: A REVIEW OF MODERN TECHNOLOGIES AND MISSION CAPABILITIES, Richard E. Wirz, University of California, Los Angeles, USA

2015-276: IN-FLIGHT OPERATION OF THE MINIATURE PROPULSION SYSTEM INSTALLED ON SMALL SPACE PROBE: PROCYON, Hiroyuki Koizumi, Hiroki Kawahara, Kazuya Yaginuma, Jun Asakawa, Ryu Funase, Kimiya Komurasaki, The University of Tokyo, Japan

2015-277: DESIGN, CONSTRUCTION AND TESTING OF A RADIO FREQUENCY MINI ION ENGINE ACCORDING TO THE PROPULSION REQUIREMENTS OF THE NEXT GENERATION GRAVITY MISSIONS "NGGM", Davar Feili, Maria Smirnova, Mantas Dobkevicius, Davina Maria Di Cara, Luca Massotti, Eduard Bosch Borras, A. Mingo Perez, Benjamin Lotz, Cheryl Collingwood, University of Southampton, UK

2015-278: MOLECULAR DYNAMICS COMPUTATION OF STEADY-STATE SPUTTER YIELDS OF HEXAGONAL BORON NITRIDE, Brandon Denis Smith, Iain Boyd, University of Michigan, USA

2015-279: HALL THRUSTER DISCHARGE WALL EROSION AS A FUNCTION OF OPERATING CONDITION AND BACKGROUND PRESSURE, Kristina M Lemmer, Wensheng Huang, Rohit Shastry, Hani Kamhawi, Western Michigan University, USA

2015-280: EVALUATION OF EROSION REDUCTION MECHANISMS IN HALL EFFECT THRUSTERS, Daniel Perez Grande, Pablo Fajardo, Eduardo Ahedo, Universidad Carlos III de Madrid, Spain

2015-282: MAGNETIC FIELD ANGLE EFFECTS ON SHEATH FORMATION NEAR A FLAT PLATE SURFACE WITH APPLICATIONS TO HALL THRUSTERS, Joseph Nicholas Lukas, Michael Keidar, The George Washington University, USA

2015-283: BREATHING MODE IN HALL EFFECT THRUSTERS, Kentaro Hara, Iain D Boyd, Michael J Sekerak, Alec D Gallimore, University of Michigan, USA

2015-284: STABILIZING LOW FREQUENCY OSCILLATION WITH TWO STAGES FILTER IN HALL THRUSTERS, Liqiu Wei, Jing Li, Liang Han, Daren Yu, Chaohai Zhang, Xiaobin He, Harbin Institute of Technology, China

2015-285: HIGH-SPEED IMAGE ANALYSIS AND FILTERED IMAGING OF NESTED HALL THRUSTER OSCILLATIONS, Ethan T Dale, Alec D Gallimore, University of Michigan, USA

2015-286: AXIAL-AZIMUTHAL HYBRID-DIRECT KINETIC SIMULATION OF HALL EFFECT THRUSTERS, Kentaro Hara, Iain D Boyd, University of Michigan, USA

2015-289: DEVELOPMENT OF A RADIO-FREQUENCY GENERATOR FOR RF ION THRUSTERS, Jens Simon, Uwe Probst, Peter J. Klar, University of Applied Sciences Giessen, Germany

2015-290: AIRBUS DS 5KW CLASS ELECTRIC PROPULSION SYSTEM BASED ON RADIO-FREQUENCY ION THRUSTERS, Jan-Patrick Porst, Juergen Kuhmann, Ralf Kukies, Hans J. Leiter, Airbus DS GmbH, Germany

2015-291: ION THRUSTERS DEVELOPMENT FOR A TRANSPORT AND POWER GENERATION MODULE PROJECT, Alexander Lovtsov, Andrey Shagayda, Vyacheslav Muravlev, Michael Selivanov, Keldysh Research Centre, Russia

2015-292: SYSTEM IDENTIFICATION OF A RADIO-FREQUENCY ION THRUSTER, Niklas Wolf, Uwe Probst, Peter J. Klar, University of Applied Sciences Giessen, Germany

2015-293: DEVELOPMENT OF A SUPERCONDUCTING MAGNET SYSTEM FOR A HELICON PLASMA THRUSTER, John Joseph Vitucci, Zachariah A. Brown, Raymond John Sedwick, University of Maryland, USA

2015-294: RECENT PROGRESS OF A HELICON PLASMA THRUSTER DEVELOPMENT, Takahashi Kazunori, Komuro Atsushi, Ando Akira, Tohoku University, Japan

2015-296: DEVELOPMENT OF HELICON ELECTROSTATIC THRUSTER (HEST), Akira Uchigashima, Teruaki Baba, Daisuke Ichihara, Akira Iwakawa, Akihiro Sasoh, Shota Harada, Takuya Yamazaki, Matsutaka Sasahara, Tomiji Iwasaki, Nagoya University, Japan

2015-297: DESIGN AND DEVELOPMENT OF A 1 KW-CLASS HELICON ANTENNA THRUSTER, Mario Merino, Jaume Navarro, Santiago Casado, Eduardo Ahedo, Victor Gomez, Mercedes Ruiz, Eduard Bosch, Jose Gonzalez Del Amo, Universidad Carlos III de Madrid, Spain

2015-298: PARTICLE-IN-CELL SIMULATIONS OF POTENTIAL STRUCTURE AROUND ELECTRIC SOLAR WIND SAIL TETHERS, Hoshi Kento, Kojima Hirotsugu, Yamakawa Hiroshi, Kyoto University, Japan

2015-299: OPTIMIZATION OF ORBITAL TRANSFER OF ELECTRODYNAMIC TETHER SATELLITE BY NONLINEAR PROGRAMMING, Ryusuke Harada, Koki Fujita, Toshiya Hanada, Kyushu University, Japan

2015-301: PREPARATION FOR ON-ORBIT DEMONSTRATION OF ELECTRODYNAMIC TETHER ON HTV, Yasushi Ohkawa, Satomi Kawamoto, Teppei Okumura, Kentaro Iki, Yuuta Horikawa, Kazutaka Kawashima, Yoshiyuki Miura, Moto Takai, Masahito Washiya, Osamu Kawasaki, Toru Kasai, Hirohiko Uematsu, Koichi Inoue, Daisuke Tsujita, JAXA, Japan

2015-302: RESEARCH AND DEVELOPMENT OF LOW-POWER CYLINDRICAL-TYPE HALL THRUSTERS FOR NANO/MICRO-SATELLITES, Tetsuo Kakuma, Tomoyuki Ikeda, Masato Nshida, Taisuke Kagota, Yuya Takahata, Hirokazu Tahara, Osaka Institute of Technology, Japan

2015-303: THE IODINE SATELLITE (ISAT) PROJECT DEVELOPMENT TOWARDS CRITICAL DESIGN REVIEW, John W. Dankanich, Derek Calvert, Hani Kamhawi, Tyler Hickman, James Szabo, Lawrence Byrne, NASA Marshall Space Flight Center, USA

2015-304: DESIGN OF A CUBESAT PROPULSION SYSTEM USING A CYLINDRICAL HALL THRUSTER, Lui T. C. Habl, Paolo Gessini, Stephen B. Gabriel, University of Brasilia, Brazil

2015-307: EFFECTS OF THE GAS PRESSURE ON LOW FREQUENCY OSCILLATIONS IN EΧB DISCHARGES, Yevgeny Raitses, Igor Kaganovich, Andrei Smolyakov, Princeton University, USA

2015-309: FACILITY EFFECTS ON HALL THRUSTER PERFORMANCE THROUGH CATHODE COUPLING, Rostislav Spektor, W. G. Tighe, P. H. Stoltz, K. R. C. Beckwith, The Aerospace Corporation, USA

2015-310: THE IMPORTANCE OF THE CATHODE PLUME AND ITS INTERACTIONS WITH THE ION BEAM IN NUMERICAL SIMULATIONS OF HALL THRUSTERS, Alejandro Lopez Ortega, Ioannis G Mikellides, Jet Propulsion Laboratory, USA

2015-311: FULLY TWO-DIMENSIONAL PARTICLE-IN-CELL MONTE CARLO COLLISIONS MODEL OF A WALL-LESS HALL THRUSTER, Laurent Garrigues, Stephane Mazouffre, Julien Vaudolon, Sedina Tsikata, University of Toulouse, France

2015-313: CHARACTERIZATION OF FLUCTUATIONS IN HYBRID AXIAL-AZIMUTHAL HALL THRUSTER SIMULATIONS, Eduardo Fernandez, Caleb Dowdy, Jacob Aley, Eckerd College, USA

2015-314: PSEUDOSPECTRAL MODEL FOR HYBRID PIC HALL-EFFECT THRUSTER SIMULATION, Justin W Koo, David Bilyeu, Robert Martin, AFRL/RQRS, USA

2015-315: DYNAMIC PARTICLE WEIGHT REMAPPING IN HYBRID PIC HALL-EFFECT THRUSTER SIMULATION, Robert Scott Martin, Justin Koo, David Bilyeu, ERC Inc., USA

2015-317: ION ENGINE COMBINING POSITIVE AND NEGATIVE IONS, Koda Daiki, Kuninaka Hitoshi, The University of Tokyo, Japan

2015-320: IN SEARCH OF ALTERNATIVE PROPELLANTS FOR ION THRUSTERS, Kristof Holste, Waldemar Gartner, Peter Kohler, Patrick Dietz, Jennifer Konrad, Stefan Schippers, Peter J. Klar, Alfred Muller, Peter R. Schreiner, Justus-Liebig-University Giessen, Germany

2015-322: LOW-POWER RADIO-FREQUENCY ION THRUSTER, Nikolay N. Antropov, Ruslan V. Akhmetzhanov, Aleksandr V. Bogatyi, Grigoriy A. Dyakonov, Garri A. Popov, Albert I. Belogurov, Pavel A. Dronov, Andrey V. Ivanov, Sergey A. Khartov, MAI, Russia

2015-323: SPATIAL PROFILE OF ION VELOCITY DISTRIBUTION FUNCTION IN HELICON HIGH-DENSITY PLASMA BY LASER INDUCED FLUORESCENCE METHOD, Yuriko Tanida, Daisuke Kuwahara, Shunjiro Shinohara, Tokyo University of Agriculture and Technology, Japan

2015-326: ANALYSIS OF PLASMA IMPEDANCE IN HELICON ANTENNA THRUSTERS, Bin Tian, Eduardo Ahedo, Jaume Navarro Cavalle, Universidad Carlos III de Madrid, Spain

2015-328: INCREASE IN THRUST OF MAGNETO PLASMA SAIL USING SOLID OR DEPLOYABLE SUPERCONDUCTING COIL, Yoh Nagasaki, Ikkoh Funaki, Taketsune Nakamura, Hiroshi Yamakawa, Kyoto University, Japan

2015-329: THRUST PERFORMANCE OF MAGNETO PLASMA SAIL WITH A MAGNETIC NOZZLE, Kajimura Yoshihiro, Tatsumasa Hagiwara, Oshio Yuya, Funaki Ikkoh, Yamakawa Hiroshi, National Institute of Technology Akashi, Japan

2015-330: EXPERIMENTAL AND NUMERICAL INVESTIGATION OF MAGNETOSPHERE INFLATION OF MAGNETOPLASMA SAIL, Oshio Yuya, Ueno Kazuma, Sano Tatsurou, Yoshiki Yamagiwa, Funaki Ikkoh, JAXA, Japan

2015-428p: INFLUENCE OF ILLUMINATING ANGLE ON IMPULSE CHARACTERISTICS WITH PULSED LASER ABLATION, Hisashi Tsuruta, Bin Wang, Yusuke Katagiri, Akihiro Sasoh, Nagoya University, Japan

2015-432p: THE EFFECTS OF MAGNETIC FIELD IN PLUME REGION ON THE PERFORMANCE OF MULTI-CUSPED FIELD THRUSTER, Peng Hu, Hui Liu, Daren Yu, Yuanyuan Gao, Harbin Institute of Technology, China

2015-434p: PLUME CHARACTERIZATION OF GAS-FED PULSED PLASMA DEFLAGRATION THRUSTERS, Keith Thomas Kessler Loebner, Thomas C. Underwood, Andrea Lucca Fabris, Mark Cappelli, James Szabo, Stanford University, USA

2015-435p: PARTICLE-IN-CELL SIMULATIONS FOR THE EFFECT OF MAGNETIC SHIELDING AND CHANNEL LENGTH ON CYLINDRICAL HALL THRUSTER, Yuanyuan Gao, Hui Liu, Daren Yu, Hongyan Huang, Hu Peng, Harbin Institute of Technology, China

2015-437p: TIME-SYNCHRONIZED LASER INDUCED FLUORESCENCE MEASUREMENT OF XENON ION AND NEUTRAL DYNAMICS IN A 350 W HALL THRUSTER, Christopher V. Young, Andrea Lucca Fabris, Mark A. Cappelli, Stanford Plasma Physics Laboratory, USA

2015-438p: COMPARISON OF HALL THRUSTER ION DYNAMICS BETWEEN LASER INDUCED FLUORESCENCE MEASUREMENTS AND A 2-D HYBRID SIMULATION, Christopher V. Young, Eunsun Cha, Eduardo Fernandez, Mark A. Cappelli, Stanford Plasma Physics Laboratory, USA

2015-439p: TWO-STAGE-TO-ORBIT TRANSPORTING SYSTEM COMBINING MICROWAVE ROCKET AND MICROWAVE THERMAL ROCKET FOR SMALL SATELLITE LAUNCH, Kaoru Kakinuma, Masafumi Fukunari, Toshikazu Yamaguchi, Yusuke Nakamura, Hiroyuki Koizumi, Kimiya Komurasaki, Kevin Parkin, The University of Tokyo, Japan

2015-440p: EXPERIMENT OF PARALLEL FIELD EMISSION CATHODE OPERATION PREPARING FOR ON-ORBIT DEMONSTRATION OF ELECTRODYNAMIC TETHER, Shin Imoto, Naoki Yuasa, Yasushi Ohkawa, Satomi Kawamoto, Yoshiki Yamagiwa, Shizuoka University, Japan

2015-442p: EXPERIMENTAL SETUP FOR THE DEVELOPMENT OF A TRAVELING MAGNETIC FIELD PLASMA ACCELERATOR, Simone Feraboli, Andrea Lucca Fabris, Mark A. Cappelli, Stanford University, USA

2015-444p: SIMULATION OF TEMPERATURE DEFORMATION OF ION THRUSTER ELECTRODES, Vladimir A. Fedorov, Vladimir A. Obukhov, Andrey I. Mogulkin, Moscow Aviation Institute, Russia

2015-446p: DEVELOPMENT OF A TAPERED-TUBE MILLIMETER-WAVE RECEIVER FOR DISTANT WIRELESS POWER TRANSFER IN MICROWAVE ROCKET SYSTEM, Masafumi Fukunari, Nat Wongsuryrat, Toshikazu Yamaguchi, Yusuke Nakamura, Kaoru Kakinuma, Hiroyuki Koizumi, Kimiya Komurasaki, The University of Tokyo, Japan

2015-450p: INTEGRAL DIAGNOSTICS METHOD CHARACTERIZING GAS DISCHARGE UNIT OF AN RF INDUCTIVE ION THRUSTER, Valentin A. Riaby, Vladimir A. Obukhov, Pavel E. Masherov, Andrey I. Mogulkin, Victor V. Balashov, Moscow Aviation Institute, Russia

2015-452p: DEVELOPMENT OF JÃ—B ARC DISCHARGE THRUSTER USING METAL AND GAS PROPELLANTS FOR FUTURE SPACE TRANSPORTERS, Yoshitaka Hisanaga, Tetsu Mieno, Shizuoka University, Japan

2015-453p: INVESTIGATION OF ION BEAM EXTRACTION MECHANISM FOR HIGHER THRUST DENSITY OF ION THRUSTERS, Kenta Hiramoto, Yokohama National University, Japan

2015-454p: NUMERICAL SIMULATION OF ECR PLASMA IN AIR BREATHING ION ENGINE (ABIE): NEUTRAL GAS DENSITY DISTRIBUTION AND ECR PLASMA FORMATION, Tubasa Yasukochi, Hideyuki Usui, Yohei Miyake, Shinichiro Kawaguchi, Masato Fukuda, Kumiko Yokota, Masahito Tagawa, Kobe University, Japan

2015-455p: THERMAL ANALYSIS OF LANTHANUM HEXABORIDE HOLLOW CATHODE WITH RADIATIVE CARBON HEATER, Oshio Yuya, Kubota Kenichi, Ohkawa Yasushi, Cho Shinatora, Watanabe Hiroki, Funaki Ikkoh, JAXA, Japan

2015-456p: EFFECTS OF ELECTRODE PROPERTIES OF A SHORT PULSE, Haruna Hasegawa, Kouta Matsubara, Hiroshi Hosokawa, Nao Akashi, Yuji Oigawa, Hideyuki Horisawa, Tokai University, Japan

2015-459p: THRUST PERFORMANCE IN A 5 KW CLASS ANODE LAYER TYPE HALL THRUSTER, Naoji Yamamoto, Kohei Takase, Yuya Hirano, Kimiya Komurasaki, Akira Kakami, Ryudo Tsukizaki, Satoshi Hosoda, Hitoshi Kuninaka, Shigeru Yokota, Kyushu University, Japan

2015-460p: GROUND EXPERIMENT FOR THE SMALL UNIFIED PROPULSION SYSTEM: I-COUPS INSTALLED ON THE SMALL SPACE PROBE: PROCYON, Hiroki Kawahara, Jun Asakawa, Kazuya Yaginuma, Hiroyuki Koizumi, Ryu Funase, Kimiya Komurasaki, The University of Tokyo, Japan

2015-461p: THRUST MEASUREMENT OF MAGNETO PLASMA SAIL WITH MAGNETIC NOZZLE BY USING THERMAL PLASMA INJECTION, Tatsumasa Hagiwara, Kajimura Yoshihiro, Oshio Yuya, Funaki Ikkoh, National Institute of Technology Akashi, Japan

2015-462p: THRUST EVALUATION OF MAGNETO PLASMA SAIL INJECTING THERMAL PLASMA BY USING 3D HYBRID PIC CODE, Ryu Yamashita, Yoshihiro Kajimura, Ikkoh Funaki, Hiroshi Yamakawa, National Institute of Technology Akashi, Japan

2015-463p: THREE DIMENSIONAL PARTICLE-IN-CELL SIMULATION FOR THE DEVELOPMENT OF AIR BREATHING ION ENGINE, Shinichiro Kawaguchi, Hideyuki Usui, Yohei Miyake, Tubasa Yasukochi, Masato Fukuda, Kumiko Yokota, Masahito Tagawa, Kobe University, Japan

2015-464p: THE EFFECT OF LASER INTENSITY ON LSD WAVE PROPAGATION VELOCITY AND ITS APPLICATION TO LASER PROPULSION SYSTEM, Kohei Matsui, Joseph A. Ofosu, Kohei Shimamura, Kimiya Komurasaki, Hiroyuki Koizumi, The University of Tokyo, Japan

2015-465p: OPTIMIZING A MAGNETIC FIELD STRENGTH OF A MAGNETIC THRUST CHAMBER, Naoya Saito, Ryosuke Kawashima, Taichi Morita, Naoji Yamamoto, Hideki Nakashima, Shinsuke Fujioka, Akifumi Yogo, Hiroaki Nishimura, Atsushi Sunahara, Yoshitaka Mori, Tomoyuki Johzaki, Kyushu University, Japan

2015-466p: EXTRACTION OF EXPLOSIVE CHARACTERISTICS FROM STABLE MATERIALS IRRADIATED BY LOW-POWER LASER DIODES, Shoko Shibagaki, Kai Wada, Yoshiki Fukuda, Keisuke Kondo, Hideyuki Horisawa, Tokai University, Japan

2015-467p: NUMERICAL ANALYSIS OF SHOCK WAVE SUPPORTED BY MICROWAVE DISCHARGE IN MICROWAVE-BEAMING PROPULSION, Kageyama Yoshiaki, Takahashi Masayuki, Ohnishi Naofumi, Tohoku University, Japan

2015-470p: OPTIMIZATION OF PLASMA PRODUCTION WITH IMPEDANCE ANALYSIS FOR A MICRO RF ION THRUSTER, Kaito Nakagawa, Yokohama National University, Japan

2015-471p: DEVELOPMENT OF THE THRUST STAND OF HIGH-POWER ELECTRIC PROPULSION USING A TUNING FORK ELECTRONIC BALANCE, Takahiro Sudo, University of Shizuoka, Japan

2015-472p: IGNITION CHARACTERISTICS OF 15 KW ARCJET WITH HOLLOW CATHODE, Koki Yoshida, The University of Tokyo, Japan

2015-474p: PARTICLE SIMULATION OF ELECTRODELESS PLASMA THRUSTER WITH ROTATING ELECTRIC FIELD, Dai Uchigasaki, Naofumi Ohnishi, Tohoku university, Japan

2015-475p: MAGNETIC FIELD DISTRIBUTIONS OF A LASER ASSISTED PULSED PLASMA THRUSTER, Kentaro Kato, Nao Akashi, Yuji Oigawa, Hiroshi Hosokawa, Hideyuki Horisawa, Tokai Univertsity, Japan

2015-477p: NANOSECOND LASER-TARGET INTERACTION FOR HIGHSPEED PLASMA EMISSION, Ryosuke Koyama, Ryo Edamura, Akihiro Osamura, Nao Akashi, Shigeru Yamaguchi, Hideyuki Horisawa, Ikkoh Funaki, Tokai Univertsity, Japan

2015-478p: TIME-INDEPENDENT FULLY KINETIC PARTICLE-IN-CELL FOR PLASMA MAGNETIC FIELD INTERACTIONS, Toshihiro Matsuguma, Takaya Inamori, Rei Kawashima, Shinichi Nakasuka, Ryu Funase, The University of Tokyo, Japan

2015-480p: DEVELOPMENT OF 5CM SIZE MICROWAVE DISCHARGE ION THRUSTER WITH VARIABLE MAGNETIC FIELD, Yoshiyuki Takao, Koichi Hashimoto, Masamitu Hata, Nishinippon Institute of Technology, Japan

2015-481p: ENDURANCE TEST OF PTFE-SHEET-FED PULSED PLASMA THRUSTER, Tetsushi Yoshikawa, Yokohama National University, Japan

2015-482p: HIGH-TEMPERATURE GENERATION OF A DIODE-LASER COUPLED FIBER-TIP HEAT SOURCE, Kai Wada, Shoko Shibagaki, Yoshiki Fukuda, Keisuke Kondo, Hideyuki Horisawa, Tokai University, Japan

2015-485p: A STUDY OF MINIATURIZATION OF TRAVELING WAVE DIRECT ENERGY CONVERTER FOR LOADING ON A SPACECRAFT, Hiromasa Takeno, Yusuke Togo, Tomohiro Katsura, Yasuyoshi Yasaka, Kazuya Ichimura, Yousuke Nakashima, Kobe University, Japan

2015-486p: INFLUENCE OF DOUBLY-IONIZED XENON ON THE LIFETIME OF MICROWAVE DISCHARGE CATHODE, Yoshitaka Tani, The University of Tokyo, Japan

2015-487p: PLASMA PROPERTY MEASUREMENT IN A MICROWAVE DISCHARGE USING LASER TOMSON SCATTERING TECHNIQUE, Kazuhiko Nakano, Kyushu University, Japan

2015-489p: EXPERIMENTAL INVESTIGATION OF THE HOLLOW CATHODE ELECTROMAGNETIC RADIATION, Andrey A. Plokhikh, Nikolay A. Vazhenin, Vladimir Kim, Sergey Baranov, Moscow Aviation Institute, Russia

2015-490p: TESTING TO INVESTIGATE STRESS-LIFETIME CHARACTERISTICS OF HIGH VOLTAGE PRINTED CIRCUIT BOARDS, Oliver El Korashy, Andreas Franke, Matthias Gollor, ESA, Netherlands

2015-491: MEPS PROGRAMME - NEW HORIZONS FOR LOW POWER ELECTRIC PROPULSION SYSTEMS, Tommaso Misuri, Mariano Andrenucci, Jacob Herscovitz, Barak Waldvogel, Kathe Dannenmayer, Sitael S.p.a., Italy

2015-492: AFFORDABLE EXPLORATION ARCHITECTURES USING THE SPACE LAUNCH SYSTEM AND HIGH POWER SOLAR ELECTRIC PROPULSION, Roger M. Myers, C. Russell Joyner, R. Joseph Cassady, Steven Overton, Timothy Kokan, James Horton, W. Andrew Hoskins, Aerojet Rocketdyne, USA

2015-493: ATTITUDE CONTROL OF UWE-4 FOR ORBIT CORRECTION DURING FORMATION FLYING, Siddharth Dadhich, Philip Bangert, Klaus Schilling, Lulea Technical University, Sweden

2015 FILE INDEX & FILE DIRECTORY