QUELQUES RESULTATS DES ESSAIS DE VOLS D'UN MODELE DE REACTEUR A IONS AVEC UNE IONISATION SUPERFICIELLE DE CESIUM AU WOLFRAMGAVRILOV FV; MYASNIKOV AS; ZHADAN GG et al.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 1; PP. 140-144; BIBL. 9 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

ION THRUSTER THERMAL CHARACTERISTICS AND PERFORMANCEWEN L; CROTTY JD; PAWLIK EV et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 35-41; BIBL. 12 REF.Serial Issue

STAR TRACKING THROUGH THE EXHAUST BEAM OF MERCURY BOMBARDMENT THRUSTERS = POURSUITE D'ETOILES AU TRAVERS DU FAISCEAU DE SORTIE DE PROPULSEURS A BOMBARDEMENT DE MERCUREMILDER NL; SOVEY JS.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 47-51; BIBL. 18 REF.Serial Issue

THE ELECTRICAL PROPULSION OF SPACE VEHICULESBRIGHT AW; MAKIN B.1973; CONTEMPOR. PHYS.; G.B.; DA. 1973; VOL. 14; NO 1; PP. 25-38; BIBL. 4 REF.Serial Issue

AN ION THRUSTER MODULE FOR PRIMARY PROPULSION SYSTEMSKING HJ; POESCHEL RL.1973; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1973; VOL. 26; NO 4; PP. 203-219; BIBL. 10 REF.Serial Issue

FRENCH RESEARCH ON CESIUM CONTACT ION SOURCESLE GRIVES E; LABBE J.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 113-118; BIBL. 8 REF.Serial Issue

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

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

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

COMPONENT DEVELOPMENT FOR A 10-CM MERCURY ION THRUSTERPYE JW.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 106-112; BIBL. 19 REF.Serial Issue

ALL-ELECTRIC THRUSTER CONTROL OF A GEOSTATIONARY COMMUNICATIONS SATELLITE = CONTROLE D'UN SATELLITE DE TELECOMMUNICATIONS GEOSTATIONNAIRE ENTIEREMENT PAR PROPULSEURS ELECTRIQUESKAPLAN MH.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 119-125; BIBL. 8 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

DIRECT THRUST MEASUREMENTS AND BEAM DIAGNOSTICS ON AN 18-CM KAUFMAN ION THRUSTERJUNGE HJ; SPRENGEL UW.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 101-105; BIBL. 6 REF.Serial Issue

EFFECTS OF THE HOLLOW CATHODE DISCHARGE ON THROTTLED ION THRUSTER PERFORMANCEWILBUR PJ.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 3-4; BIBL. 4 REF.Serial Issue

THE FEASIBILITY OF GEOSTATIONARY EMPLACEMENT OF SATELLITES BY SOLAR ELECTRIC TUGHOLDAWAY R; JANSSON REW.1973; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1973; VOL. 26; NO 4; PP. 220-227; BIBL. 13 REF.Serial Issue

VISCOUS EFFECTS ON BIOWASTE RESISTOJET NOZZLE PERFORMANCEKALLIS JM; GOODMAN M; HALBACH CR et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 11; PP. 869-875; BIBL. 7 REF.Serial Issue

INFLUENCE OF MAGNETIC FIELDS ON ANODE LOSSES IN MPD-ARCSSCHALL W.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 1; PP. 10-11; BIBL. 3 REF.Serial Issue

LOW-COST SOLAR ELECTRIC TEST BED FOR ION THRUSTER SYSTEMSSCHEEL HW.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 853-857; BIBL. 6 REF.Serial Issue