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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

AIAA 9TH ELECTRIC PROPULSION CONFERENCE. BETHESDA, MD, APRIL 17-19, 19721972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; PP. (872 P.); H.T. 7; BIBL. DISSEM.; 91 FASCConference Paper

OPTIMAL QUASI-STEADY PLASMA THRUSTER SYSTEM CHARACTERISTICSLUDWIG DE; KELLY AJ.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 165-169; BIBL. 8 REF.Serial Issue

PRINCIPE DE FONCTIONNEMENT ET CARACTERISTIQUES DES SYSTEMES DE PROPULSION ELECTRIQUE. APPLICATION A LA STABILISATION DES SATELLITES. IREYNIER M; LANDRAULT C.1972; AERONAUT. ET ASTRONAUT.; FR.; DA. 1972; NO 37; PP. 55; ABS. ANGL. ALLEMSerial Issue

EXHAUST FLOW AND PROPULSION CHARACTERISTICS OF A PULSED MPD-ARC THRUSTERMICHELS CJ; YORK TM.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 579-580; BIBL. 4 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

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

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

PROPULSEURS A PLASMAsdIN: PROPUL. ELECTR. APPL. SPAT. 2EME JOURN. ETUD. TOULOUSE, 1972; S.L.; DA. S.D.; PP. 171-235; ABS. FR.; BIBL. DISSEM.Conference Paper

EXHAUST PLUME STRUCTURE IN A QUASI-STEADY MPD ARCBRUCKNER AP; JAHN RG.1972; IN: AIAA 9TH ELECTR. PROPUL. CONF. BETHESDA, MD, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 499; PP. 1-12; BIBL. 2 P.Conference Paper

PROPULSEURS.1977; NAV. PORTS CHANTIERS; FR.; DA. 1977; NO 325; PP. 415Article

PLASMA DIAGNOSTICS OF THE RF-ION THRUSTER "RIT-10"WALTHER RJ; SCHAEFER M; FREISINGER J et al.1972; IN: AIAA 9TH ELECTR. PROPUL. CONF. BETHESDA, MD, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 472; PP. 1-8; BIBL. 11 REF.Conference Paper

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

OPTIMIERUNG DER BETRIEBSBEDINGUNGEN IN EINEM PLASMAWINDKANAL DURCH KONTROLLE DER DRUCKVERTEILUNG IN DER BESCHLEUNIGUNGSSTRECKE = OPTIMISATION DES CONDITIONS DE FONCTIONNEMENT DANS UNE SOUFFLERIE A PLASMA PAR LE CONTROLE DE LA DISTRIBUTION DE LA PRESSION DANS LA SECTION D'ACCELERATIONZABKA W.1972; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1972; NO 70-72; PP. 1-103; ABS. ANGL.; BIBL. 26 REF.Serial Issue

MHD PROPULSION BY ABSORPTION OF LASER RADIATION.MYRABO LN.1976; J. SPACER. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 8; PP. 466-472; BIBL. 83 REF.Article

INFLUENCE OF MAGNETIC FIELDS ON ANODE LOSSES IN MPD-ARCSSCHALL W.1972; IN: AIAA 9TH ELECTR. PROPUL. CONF. BETHESDA, MD, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 502; PP. 1-10; BIBL. 8 REF.Conference Paper

SYSTEM TRADEOFFS FOR PULSED MPD THRUSTER IN SPACE MISSION APPLICATIONHWACHII LIEN.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 858-862; BIBL. 8 REF.Serial Issue

ELECTRON NUMBER DENSITY AND TEMPERATURE IN MPD-ARC THRUSTER EXHAUSTSMICHELS CJ; ROSE JR; SIGMAN DR et al.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 11; PP. 1395-1396; 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

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

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