APPLICATIONS (I): STABILISATION DE SATELLITESsdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 309-358; ABS. ANGL. FR.; BIBL. DISSEM.Conference Paper

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EFFECTS OF HEAT ADDITION IN DIVERGENT NOZZLES WITH APPLICATION TO MPD THRUSTERS = INFLUENCE D'UNE ADDITION DE CHALEUR DANS DES TUYERES DIVERGENTES, AVEC APPLICATION AUX PROPULSEURS MPDSAJBEN M; CHMIELEWSKI GE.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 6; PP. 476-478; BIBL. 1 REF.Serial Issue

FEASIBILITY STUDIES ON AN AUXILIARY PROPULSION SYSTEM USING MPD THRUSTERS = ETUDES DE LA POSSIBILITE D'UN SYSTEME DE PROPULSION AUXILIAIRE UTILISANT DES PROPULSEURS MPDBURKHART JA; SEIKEL GR.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 7; PP. 487-488; BIBL. 3 REF.Serial Issue

DEVELOPMENT OF ELECTRICAL PROPULSION IN THE FEDERAL REPUBLIC OF GERMANYLOSCH HR.sdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 3-14; ABS. FR.; BIBL. 2 P. 1/2Conference Paper

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LES RECHERCHES EN FRANCE SUR LA PROPULSION IONIQUEMUTIN MJ.sdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 21-25; ABS. ANGL.; BIBL. 2 REF.Conference Paper

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ION-THRUSTER PROPELLANT UTILIZATION = UTILISATION DU COMBUSTIBLE DANS UN PROPULSEUR IONIQUEKAUFMAN HR.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 7; PP. 511-517; BIBL. 12 REF.Serial Issue

ESRO'S ACTIVITY ON ELECTRIC PROPULSIONBRACHER JE.sdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 15-20; ABS. FRConference Paper

RESISTOJET AND PLASMA PROPULSION SYSTEM TECHNOLOGYGRECO RV; BLISS JR; MURCH CK et al.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH. JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK, N.Y.; A.I.A.A.; DA. S.D.; NO 1124; PP. 1-17; BIBL. 27 REF.Conference Paper

PERFORMANCE OF A FILTEEN-CENTIMETER ION THRUSTER WITH RELIABLE RESTART CAPABILITY.WILBUR PJ.1974; J. SPACECR. ROCK.; U.S.A.; DA. 1974; VOL. 11; NO 9; PP. 621-624; BIBL. 9 REF.Article

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LA PROPULSION ELECTRIQUE DANS SES APPLICATIONS SPATIALES. 2EMES JOURNEES D'ETUDES. TOULOUSE, 21-23 JUIN 1972sd; S.L.; DA. S.D.; PP. 1-447; BIBL. DISSEM.Conference Paper

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ION THRUSTER PERFORMANCE CALIBRATIONPAWLIK EV; GOLDSTEIN R; FITZGERALD DJ et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 327-332; BIBL. 16 REF.Serial Issue

RADIATION FROM PULSED ELECTRIC THRUSTERSTHOMASSEN KI.sdIN: AIAA 11TH AEROSP. SCI. MEET.; WASHINGTON; 1973; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 263; PP. 1-4; BIBL. 11 REF.Conference Paper

HOCHFREQUENZGENERATOR FUER DAS IONENTRIEBWERK RIT 10 = GENERATEUR HAUTE FREQUENCE POUR LE PROPULSEUR IONIQUE RIT 10BUTTNER M; PALZ G.1978; SIEMENS Z.; DEU; DA. 1978; VOL. 52; NO 10; PP. 581-583; BIBL. 2 REF.Article

MEASUREMENTS OF PLASMA FLUCTUATION IN AN 8 CM MERCURY ION THRUSTER.SERAFINI JS; NAKANISHI S.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 11; PP. 692-698; BIBL. 10 REF.Article

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A POWER CONDITIONER SUBSYSTEM FOR AN ION ENGINE.KUDO I; MACHIDA K; MURAKAMI H et al.1976; ELECTR. ENGNG JAP.; U.S.A.; DA. 1976; VOL. 96; NO 2; PP. 128-137; BIBL. 9 REF.Article

SURVEY OF ELECTRIC PROPULSION CAPABILITY.CLARK KE.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 11; PP. 641-654; BIBL. 58 REF.Article

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