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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

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

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

SERT II 1979-1981 TESTS: ION THRUSTER PERFORMANCE AND DURABILITYKERSLAKE WR; GINACZAK LR.1982; J. SPACECR. ROCKETS; ISSN 0022-4650; USA; DA. 1982; VOL. 19; NO 3; PP. 241-245; BIBL. 9 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

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

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

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

HOCHFREQUENZGENERATOR FUER DAS IONENTRIEBWERK RIT 10 = GENERATEUR HAUTE FREQUENCE POUR LE PROPULSEUR IONIQUE RIT 10BUTTNER M; PALZ G.1978; SIEMENS Z.; DEU; DA. 1978; VOL. 52; NO 10; PP. 581-583; BIBL. 2 REF.Article

MEASUREMENTS OF PLASMA FLUCTUATION IN AN 8 CM MERCURY ION THRUSTER.SERAFINI JS; NAKANISHI S.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 11; PP. 692-698; BIBL. 10 REF.Article

ONE-MILLIPOUND MERCURY ION THRUSTER.HYMAN J JR; DULGEROFF CR; KAMI S et al.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 6; PP. 366-372; BIBL. 12 REF.Article

A POWER CONDITIONER SUBSYSTEM FOR AN ION ENGINE.KUDO I; MACHIDA K; MURAKAMI H et al.1976; ELECTR. ENGNG JAP.; U.S.A.; DA. 1976; VOL. 96; NO 2; PP. 128-137; BIBL. 9 REF.Article

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

ELECTROSTATIC THRUSTERSKAUFMAN HR; READER PD.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 1123; PP. 1-8; BIBL. 1 P. 1/2Conference Paper

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

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

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

ION THRUSTER ESKA 8 FOR NORTH-SOUTH STATIONKEEPING OF SYNCHRONOUS SATELLITES.AU GF; BAUMGARTH FJ.1974; J. SPACECR. ROCK.; U.S.A.; DA. 1974; VOL. 11; NO 9; PP. 618-620; BIBL. 2 REF.Article

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

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