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EUROPA III HEAT SHIELDS AEROTHERMODYNAMIC ANALYSIS AND DESIGNVALLERANI E.1973; REV. SCI. TECH. C.E.C.L.E.S./C.E.R.S.; FR.; DA. 1973; VOL. 5; NO 1; PP. 3-34; ABS. FR. ALLEM.; BIBL. 18 REF.Serial Issue

SHORT GUIDE TO TITAN III LAUNCH VEHICLES = PETIT GUIDE POUR LES VEHICULES LANCEURS TITAN III.DRIGGERS GW.1973; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1973; VOL. 11; NO 2; PP. 68-73Serial Issue

STRAP-DOWN INERTIAL GUIDANCE SYSTEMS STUDYBALDASSINI FONTANA R.1973; REV. SCI. TECH. C.E.C.L.E.S./C.E.R.S.; FR.; DA. 1973; VOL. 5; NO 1; PP. 35-57; ABS. FR. ALLEMSerial Issue

ROLE DE L'ELECTRICITE STATIQUE DANS LES INCIDENTS RELEVES LORS DU TIR F 11TAILLET J; HANUISE G.1972; REV. SCI. TECH. C.E.C.L.E.S./C.E.R.S.; FR.; DA. 1972; VOL. 4; NO 4; PP. 371-434; ABS. ANGL.; BIBL. 1 P.Serial Issue

RELATIVE MAGNITUDES OF STRESSES CAUSED BY STATIC AND DYNAMIC LAUNCH VEHICLE LOADS = GRANDEURS RELATIVES DES CONTRAINTES DUES A DES CHARGES STATIQUES ET DYNAMIQUES SUR UN VEHICULE LANCEURERICSSON LE; REDING JP; GUENTHER RA et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 276; BIBL. 3 REF.Serial Issue

LE LANCEUR DIAMANT B-P4ROUSSEL JG.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 5-20; ABS. ANGL. ALLEMSerial Issue

DER EINFLUSS DER LUFTVORKUEHLUNG VOR DER VERDICHTUNG BEI LUFTATMENDEN ANTRIEBEN EINES RAUMFAHRZEUGTRAEGERS = L'INFLUENCE DU PRE-REFROIDISSEMENT DE L'AIR ASPIRE AVANT LA COMPRESSION DANS LE LANCEUR D'UN VEHICULE SPATIALKUNKLER H.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-18; H.T. 11; BIBL. 6 REF.Conference 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

LONGITUDINAL VIBRATION ANALYSIS OF PARTIALLY-FILLED ELLIPSOIDAL TANKSGOLDMAN RL; RUDD TJ.1973; COMPUTERS AND STRUCT.; G.B.; DA. 1973; VOL. 3; NO 1; PP. 205-215; BIBL. 8 REF.Serial Issue

SUR LA STABILISATION EN AMPLITUDE DES OSCILLATIONS LONGITUDINALES D'UN LANCEUR AEROSPATIALRABINOVICH BI.1972; IZVEST. AKAD. NAUK. S.S.S.R., ENERGET. TRANSP.; S.S.S.R.; DA. 1972; NO 5; PP. 135-138; BIBL. 3 REF.Serial Issue

STAND UND GEGENWAERTIGE ENTWICKLUNG DER STEUERUNG FUER RAUMFAHRZEUGE = SITUATION ACTUELLE ET DEVELOPPEMENT DE LA COMMANDE DES ENGINS SPATIAUXLANDWEHR VON PRAGENAU G.1973; OSTERR. INGR-Z.; OSTERR.; DA. 1973; VOL. 16; NO 2; PP. 56-64; BIBL. 16 REF.Serial Issue

COMPUTERIZED OPTIMAL CONTROL SYSTEM DESIGN FOR BOOST VEHICLES = CONCEPTION PAR LE CALCUL D'UN SYSTEME DE COMMANDE OPTIMAL POUR VEHICULES LANCEURSTRAUTWEIN W; LIVINGSTON JM.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 227-235; BIBL. 12 REF.Serial Issue

ELASTIC LAUNCH VEHICLE RESPONSE TO SINUSOIDAL GUSTS = REPONSE D'UN VEHICULE LANCEUR ELASTIQUE A DES RAFALES SINUSOIDALESERICSSON LE; REDING JP; GUENTHER RA et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 244-252; BIBL. 23 REF.Serial Issue

REAL-TIME LAUNCH VEHICLE STEERING PROGRAMME SELECTION = CHOIX DU PROGRAMME DE PILOTAGE D'UN VEHICULE LANCEUR EN TEMPS REELBRUSCH RG; REED TE.1973; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1973; VOL. 26; NO 5; PP. 279-290Serial Issue

THE ROLE OF TESTING IN ACHIEVING AEROSPACE SYSTEMS EFFECTIVENESSSMITH AM; MATTESON TD.1973; IN: PROC. 1973 ANNU. RELIAB. MAINTAINABILITY SYMP.; PHILADELPHIA, PA.; 1973; NEW YORK, U.S.A.; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 36-41Conference Paper

DAS APOLLO-MONDPROGRAMM UND DIE SATURN V-TRAEGERRAKETE = LE PROGRAMME LUNAIRE APOLLO ET LA FUSEE PORTEUSE SATURN VKORDIK EJT.1973; OSTERR. INGR-Z.; OSTERR.; DA. 1973; VOL. 16; NO 2; PP. 40-49; BIBL. 11 REF.Serial Issue

APOLLO QUALITY THROUGH PREDICTIVE TESTINGWHITE GC JR.1972; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1972; NO 515; PP. 253-267; (TEST. PREDICT. MATER. PERFORMANCE STRUCT. COMPONENTS. SYMP. I. II.; ANAHEIM, CALIF.-ATLANTIC CITY, N.J.: 1971)Conference Paper

THE USE OF AN EXPANSION TUBE WITH COLD GAS TO DETERMINE ROCKET ENGINE STARTING TRANSIENT PRESSURES DURING SILO LAUNCH = L'UTILISATION D'UN TUBE DE DETENTE A GAZ FROID POUR DETERMINER LES PRESSIONS TRANSITOIRES DE DEPART DES MOTEURS DE FUSEE PENDANT LE DECOLLAGEWAYTE MJ; GRUENICH FA.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-9; BIBL. 3 REF.Conference Paper

EXTENDING THE LIFE AND RECYCLE CAPABILITY OF EARTH STORABLE PROPELLANT SYSTEMS = EXTENSION DE LA DUREE DE VIE ET DES POSSIBILITES DE REUTILISATION DES SYSTEMES TERRESTRES A PROPERGOL STOCKABLESCHWEICKERT TF.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 837; PP. 1-8Conference Paper

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