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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

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

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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

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

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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

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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

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

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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

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