A PROPULSION SYSTEM FOR ORBIT-TO-ORBIT SHUTTLEWELLS WW; LAMONT EA.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2586-2597Serial Issue

FULL CONTROL OF SOLID PROPELLANT ROCKETS BY SECONDARY INJECTION = CONTROLE COMPLET DE FUSEES A PROPERGOLS SOLIDES PAR INJECTION SECONDAIREZEIERMAN I; MANHEIMER TIMNAT Y.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 161-162; BIBL. BIBL. (2 REF.Serial Issue

BUOYANCY EFFECT ON FUEL CONTAINMENT IN A GAS-CORE NUCLEAR ROCKET = EFFET DE FLOTTABILITE SUR L'EMMAGASINAGE DU COMBUSTIBLE DANS UNE FUSEE NUCLEAIRE A COEUR GAZEUXPUTRE HA.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 932-934; BIBL. 4 REF.Serial Issue

SCHWIERIGKEITEN BEIM BAROMETRISCHEN AUSSCHLEUSEN VON FLUESSIGKEITEN AUS DEM VAKUUM MITTELS FALLROHREN = DIFFICULTES RENCONTREES AU COURS DE L'EVACUATION BAROMETRIQUE DE LIQUIDES D'UNE ENCEINTE SOUS VIDE A L'AIDE DE TUBES DE GRAVITELAMBRECHT H.1973; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1973; NO 10; PP. 1-27; BIBL. 3 REF.Serial Issue

AIAA SOUNDING ROCKET TECHNOLOGY CONFERENCE. 4. PROCEEDINGS; BOSTON, MASS.; 1976.1976; ; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. (308P.); 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

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

MANOEUVRE OPTIMALE D'ATTERRISSAGE SUR UNE PLANETE PAR UN MOTEUR A POUSSEE LIMITEE AVEC ANGLE D'ENTREE DONNE DANS L'ATMOSPHERE PLANETAIREKLIMKO AS.1973; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1973; NO 1; PP. 94-105; ABS. ANGL.; BIBL. 5 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

ADVANCED PINTLE-CONTROLLED MOTOR WITH THRUST VECTOR CONTROLSAYLES DC; LEVINSKY CT.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2557-2564Serial Issue

DYNAMIC RESPONSES OF SOLID ROCKETS DURING RAPID PRESSURE CHANGE = REPONSES DYNAMIQUES DE FUSEES A PROPERGOLS SOLIDES DURANT DES VARIATIONS RAPIDES DE PRESSIONTURK SL; BATTISTA RA; KUO KK et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 2; PP. 137-142; BIBL. 14 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

ATTITUDES OF THE ANTARCTIC SOUNDING ROCKET VEHICLESTOHYAMA F; AOYAMA I.1978; MEM. NATION. INST. POLAR RES., SPEC. ISSUE; JPN; DA. 1978; NO 9; PP. 87-91Conference Paper

MINIMUM SMOKE SOLID PROPELLANT ROCKET MOTORSEVANS GI.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 1192; PP. 1-11; H.T. 4Conference Paper

DEVELOPMENT OF THE ALGOL III SOLID ROCKET MOTOR FOR SCOUTFELIX BR; MCBRIDE NM.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2565-2575; BIBL. 5 REF.Serial Issue

EXPERIMENTAL DETERMINATION OF THREE-DIMENSIONAL LIQUID ROCKET NOZZLE ADMITTANCESZINN BT; BELL WA; DANIEL BR et al.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 267-272; BIBL. 15 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

ROCKET PLUMES IN THE THERMOSPHERE.DRAPER JS; BIEN F; HUFFMAN RE et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 6; PP. 825-827; BIBL. 8 REF.Article

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

RESEARCH ON COMPATIBILITY OF DATA FROM RADIOSONDES, ROCKETSONDES AND SATELLITESFINGER FG; MCINTURFF RM.1978; WORLD METEOROL. ORGANIZ., TECH. NOTE; CHE; DA. 1978; NO 163; PP. 3-26; ABS. FRE/RUS/SPA; BIBL. 9 REF.Article

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

ENTWICKLUNG VON BETANKUNGSANLAGEN UND CHECKOUT-SYSTEMEN FUER DIE SATELLITENPROJEKTE TD-1A UND AEROS = MISE AU POINT DES INSTALLATIONS DE REMPLISSAGE ET DES SYSTEMES DE CONTROLE POUR LES PROJETS DE SATELLITE TD-1A ET AEROSSCHNEIDER E.1973; RAUMFAHRTFORSCHUNG; DTSCH.; DA. 1973; VOL. 17; NO 1; PP. 23-28; ABS. ANGLSerial 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

CONVECTIVE HEATING ON DELTA-WING SPACE-SHUTTLE BOOSTERS INCLUDING INTERFERENCE EFFECTSDOUGHTY RO; ERICKSON RC; BROCK OR et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 876-882; BIBL. 16 REF.Serial Issue

COMPUTERIZED TOMOGRAPHY INSPECTION OF TRIDENT ROCKET MOTORS: A CAPABILITY DEMONSTRATIONBURSTEIN P; MASTRONARDI R; KIRCHNER T et al.1982; MATER. EVOL.; ISSN 0025-5327; USA; DA. 1982; VOL. 40; NO 12; PP. 1280-1284Article