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. Gölz, Monika Auweter-Kurtz, Helmut L. Kurtz, and P. Christian Sleziona, Institut für Raumfahrtsysteme, Universität 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 für Raumfahrtsysteme, Universität 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