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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

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

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

PROPELLER SPINDOWN OF ROTATING MAGNETSHOLLOWAY N; KUNDT W; WANG YM et al.1978; ASTR. AND ASTROPHYS.; DEU; DA. 1978; VOL. 70; NO 3; PP. L23-L26; BIBL. 11 REF.Article

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

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

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

MDT-2A TEFLON PULSED PLASMA THRUSTERSHIH MING AN; HAN JI WU.1982; J. SPACECR. ROCKETS; ISSN 0022-4650; USA; DA. 1982; VOL. 19; NO 5; PP. 385-386; BIBL. 5 REF.Article

EXPERIMENTAL STUDIES ON A LOW-POWER DUOPLASMATRON-TYPE MPD THRUSTER.KIMURA I; KUMAZAWA R.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 8; PP. 456-460; BIBL. 20 REF.Article

ESTABLISHMENT OF QUASI-STEADY OF OPERATION IN A PULSED MPD ARCJETKURIKI K; INUTAKE M.1972; IN: AIAA 9TH ELECTR. PROPUL. CONF. BETHESDA, MD, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 496; PP. 1-7; BIBL. 11 REF.Conference Paper

SERT II 1979-1981 TESTS: PLASMA THRUST AND NEUTRALIZER MEASUREMENTSKERSLAKE WR; IGNACZAK LR.1982; J. SPACECR. ROCKETS; ISSN 0022-4650; USA; DA. 1982; VOL. 19; NO 3; PP. 236-240; BIBL. 9 REF.Article

ADVANCED FUEL FUSION APPLICATION TO MANNED SPACE PROPULSION.HO R.1977; NUCL. INSTRUM. METHODS; NETHERL.; DA. 1977; VOL. 144; NO 1; PP. 69-72; BIBL. 7 REF.; (SYMP. CLEAN FUSION. 1. PROC.; WASHINGTON, D.C.; 1976)Conference Paper

FLIGHT QUALIFIED PULSED ELECTRIC THRUSTER FOR SATELLITE CONTROL.VONDRA RJ; THOMASSEN KI.1974; J. SPACECR. ROCK.; U.S.A.; DA. 1974; VOL. 11; NO 9; PP. 613-617; BIBL. 13 REF.Article

PROSPECTS FOR ROCKET PROPULSION WITH LASER-INDUCED FUSION MICROEXPLOSIONSHYDE R; WOOD L; NUCKOLLS J et al.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 1063; PP. 1-15; BIBL. 32 REF.Conference Paper

FLOWFIELD CHARACTERISTICS AND PERFORMANCE LIMITATIONS OF QUASI-STEADY MAGNETOPLASMADYNAMIC ACCELERATORS.BOYLE MJ; CLARK KE; JAHN RG et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 7; PP. 955-962; BIBL. 21 REF.Article

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

THRUST MEASUREMENT OF KIII MPD ARCJETKURIKI K; ONISHI M; MORIMOTO S et al.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1414-1419; BIBL. 10 REF.Article

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

JET-DIAGNOSTICS OF A SELF-FIELD ACCELERATOR WITH LANGMUIR PROBES.MAISENHALDER F; MAYERHOFER W.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 9; PP. 1203-1209; BIBL. 17 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

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

AIAA-JSASS-DGLR 15TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, LAS VEGAS NV, APRIL 22-23, 19811981; INTERNATIONAL ELECTRIC PROPULSION CONFERENCE. 15/1981-04-21/LAS VEGAS NV; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PAG. MULT.; 27 CMConference Proceedings

CONVERTISSEURS MAGNETOHYDRODYNAMIQUES D'UN GENRE NOUVEAU: APPAREILS A INDUCTION.PETIT JP; VITON M.1977; C.R. ACAD. SCI., B; FR.; DA. 1977; VOL. 284; NO 9; PP. 167-169; ABS. ANGL.; BIBL. 2 REF.Article

A THEORETICAL MODEL OF VELOCITY NONUNIFORMITY BETWEEN HEAVY PARTICLES IN A MPD THRUSTER.PIPERNO F; STRANI M.1975; NUOVO CIMENTO, B; ITAL.; DA. 1975; VOL. 26; NO 2; PP. 409-418; ABS. ITAL., RUSSE; BIBL. 7 REF.Article

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