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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

A CAPILLARY-FED ANNULAR COLLOID THRUSTER = UN PROPULSEUR COLLOIDAL ANNULAIRE A ALIMENTATION PAR CAPILLARITEBAILEY AG; BRACHER JE; VON ROHDEN HJ et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 7; PP. 518-521; BIBL. 2 REF.Serial Issue

DISHED ACCELERATION GRIDS ON A 30-CM ION THRUSTERRAWLIN VK; BANKS BA; BYERS DC et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 29-35; BIBL. 16 REF.Serial Issue

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

DURABILITY TESTS OF A FIVE-CENTIMETER DIAMETER ION THRUSTER SYSTEMNAKANISHI S.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1151; PP. 1-12; BIBL. 12 REF.Conference Paper

PROPULSEURS IONIQUESsdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 27-111; ABS. FR. ANGL.; BIBL. DISSEM.Conference Paper

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

LOW CURRENT PULSED ABLATION PLASMA THRUSTER.LIEBING L; SEIDEL F.1974; J. SPACECR. ROCK.; U.S.A.; DA. 1974; VOL. 11; NO 9; PP. 609-610; BIBL. 2 REF.Article

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

PROPULSIVE PERFORMANCE OF A 30 KW ARC-JET THRUSTER STABILIZED BY VORTEX AND MAGNETIC FORCESOGGERO MV; BERTOLO CV.1972; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1972; VOL. 25; NO 8; PP. 477-490; BIBL. 6 REF.Serial Issue

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

TECHNOLOGY OF ELECTRON-BOMBARDMENT ION THRUSTERS.KAUFMAN HR.1974; ADV. ELECTRON. ELECTRON PHYS.; U.S.A.; DA. 1974; VOL. 36; PP. 265-373; BIBL. 5 P. 1/2Article

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

PROTOTYPE NORTH-SOUTH STATIONKEEPING ION THRUSTER.RAMSEY WD; JAMES EL.1975; SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 7; PP. 441-443; BIBL. 3 REF.Article

SOLAR ELECTRIC PROPULSION SYSTEMS AND APPLICATIONSMOLITOR JH; KING HJ.1972; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1972; VOL. 25; NO 8; PP. 463-476; BIBL. 7 REF.Serial Issue

APPLICATIONS (II): PROPULSION PRIMAIREsdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 359-442; ABS. ANGL. FR.; BIBL. DISSEM.Conference Paper

A FACILITY FOR LONG-TERM ION THRUSTER SYSTEM TESTINGMCKINNEY HF; SUTTON RA.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 42-46; BIBL. 5 REF.Serial Issue

PERFORMANCE IMPROVEMENTS IN SOLID FUEL MICROTHRUSTERS = AMELIORATIONS DE PERFORMANCES DANS DES MICROPROPULSEURS A COMBUSTIBLE SOLIDEVONDRA RJ; THOMASSEN KI.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 10; PP. 738-742; BIBL. 7 REF.Serial Issue

ELECTROTHERMAL HYDRAZINE THRUSTER ANALYSES AND PERFORMANCE EVALUATIONCALLENS RA; MURCH CK.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH. JOINT PROPUL. SPEC. CONF., NEW ORLEANS, LA., 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1152; PP. 1-6; BIBL. 3 REF.Conference Paper

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