SOLID ROCKET MOTORS FOR THE SPACE SHUTTLE BOOSTER = MOTEURS FUSEES A COMBUSTIBLE SOLIDE POUR LE BOOSTER DE LA NAVETTE SPATIALEODOM JB.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 804; PP. 1-4Conference Paper

LOWER PAYLOAD COSTS THROUGH REFURBISHMENT AND MODULE REPLACEMENT = ABAISSEMENT DU COUT DES CHARGES UTILES PAR REMISE EN ETAT ET REMPLACEMENT PAR MODULESMURPHY JT; DARWIN CR.1973; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 40-47; BIBL. 8 REF.Serial Issue

REFURBISHABLE SPACECRAFT: MODULES AND COMPONENTS OF THE SHUTTLE ERA = VEHICULE SPATIAL RENOVABLE: MODULES ET COMPOSANTS DE L'ERE DE LA NAVETTEBOLTON FC.1973; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1973; VOL. 11; NO 4; PP. 44-50; BIBL. 6 REF.Serial Issue

AIRBREATHING ENGINES FOR SPACE SHUTTLE = MOTEURS AEROBIE POUR LA NAVETTE SPATIALEGLASSMAN AJ; STEWART WL; NOSEK SM et al.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 805; PP. 1-6; BIBL. 1 REF.Conference Paper

EVOLUTION OF THE SPACE SHUTTLE. I = EVOLUTION DE LA NAVETTE SPATIALE. IBAKER D.1973; SPACEFLIGHT; G.B.; DA. 1973; VOL. 15; NO 6; PP. 202-210Serial Issue

TURBOMACHINERY DESIGN FOR SPACE SHUTTLE AUXILIARY POWER SYSTEMS = CONCEPTION DES TURBOMACHINES POUR SYSTEMES DE PUISSANCE AUXILIAIRE DE NAVETTE SPATIALEBURRIS WL; ROWLET BH.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 835; PP. 1-10; BIBL. 5 REF.Conference Paper

THERMAL CONTROL EVALUATION OF A SHUTTLE ORBITER SOLAR OBSERVATORY USING SKYLAB ATM BACKUP HARDWARE. = EVALUATION DU CONTROLE THERMIQUE D'UN OBSERVATOIRE SOLAIRE SUR LA NAVETTE SPATIALE UTILISANT L'UNITE DE SECOURS DE L'APOLLO TELESCOP MOUNT DU SKYLABCLASS CR; PRESTA G; TRUCKS H et al.1975; IN: INTERSOC. CONF. ENVIRON. SYST.; SAN FRANCISCO, CALIF.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; PP. 1-8Conference Paper

SPACE SCIENCE PLANS FOR THE SHUTTLE ERA = PLANIFICATION DES SCIENCES SPATIALES POUR L'ERE DE LA NAVETTENAUGLE JE; JOHNSON DW.1973; ASTRONAUT. AND AERONAUT.; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 34-39Serial Issue

COMUNICAZIONI VIA NAVICELLA SPAZIALE = TELECOMMUNICATIONS VIA NAVETTE SPATIALEDANCE JB.1979; ANTENNA NUOVA; ITA; DA. 1979; VOL. 51; NO 3; PP. 102-107; (5 P.)Article

HEATING IN SHUTTLE RSI GAPS DERIVED FROM AN INVERSE HEAT TRANSFER SOLUTION. = CALCUL DE L'ECHAUFFEMENT DANS LES JOINTS DE L'ISOLATION SUPERFICIELLE REUTILISABLE DE LA NAVETTE SPATIALE A PARTIR D'UNE SOLUTION D'UN PROBLEME INVERSE DE TRANSFERT DE CHALEURCHRISTENSEN HE; KIPP HW.1975; IN: INTERSOC. CONF. ENVIRON. SYST.; SAN FRANCISCO, CALIF.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; VOL. 15; PP. 1-7; BIBL. 6 REF.Conference Paper

ERGEBNISSE EINER BETRIEBSSIMULATION FUER WIEDERVERWENDBARE RAUMTRANSPORTER = RESULTATS D'UNE SIMULATION D'EXPLOITATION DE TRANSPORTEURS SPATIAUX RECUPERABLESJOHENNING B; SPIESS WE.1972; RAUMFAHRTFORSCHUNG; DTSCH.; DA. 1972; VOL. 16; NO 5; PP. 240-247; BIBL. 6 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

DESIGN AND ANALYSIS OF AN APU MONOPROPELLANT GAS GENERATOR = CONCEPTION ET ANALYSE D'UN GENERATEUR DE GAZ A UN SEUL PROPERGOL POUR UNE UNITE DE PUISSANCE AUXILIAIREMARCY RD; MADDOX JP.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 834; PP. 1-8; BIBL. 2 REF.Conference Paper

IDENTIFICATION OF ROTATING ASSEMBLY INERTIAL AND BEARING PARAMETERSALSPACH DL.1972; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1972; DA. 1972; VOL. 8; NO 5; PP. 602-608; BIBL. 5 REF.Serial Issue

SPACE SHUTTLE: DAWN OF AN ERA = LA NAVETTE SPATIALE, LE DEBUT D'UNE EPOQUERECTOR WF III ED; PENZO PA ED.1980; ADV. ASTRONAUT. SCI.; USA; DA. 1980; VOL. 41; PART. 2; XVI-510 P.; BIBL. DISSEM.Conference Paper

DETERMINATION OF FLOW AREAS FOR SERIES-PARALLEL COMPARTMENT VENTING TO SATISFY PRESSURE DIFFERENTIAL REQUIREMENTSKIRBY CE; IVEY GW.1972; IN: AIAA 5TH FLUID PLASMA DYN. CONF. BOSTON, MASS., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 707; PP. 1-5; BIBL. 7 REF.Conference Paper

MAINTAINABILITY OF THE SPACE SHUTTLE ORBITER MAIN ENGINE = POSSIBILITE D'ENTRETIEN DU MOTEUR PRINCIPAL DE L'ORBITER DE NAVETTE SPATIALEGOE RT.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 808; PP. 1-12Conference Paper

MANEUVERING ENGINES FOR SPACE SHUTTLE ORBITER = MOTEURS DE MANOEUVRE POUR LE MODULE ORBITAL DE NAVETTE SPATIALEPOLIFKA RW.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 806; PP. 1-6Conference Paper

SPACE SHUTTLE ORBITER MAIN ENGINE DESIGN = CONCEPTION DU MOTEUR PRINCIPAL DE L'ORBITER DE NAVETTE SPATIALEWILHELM WF.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 807; PP. 1-10Conference Paper

SIMULATION OF ATMOSPHERIC TURBULENT GUSTS AND GUSTS GRADIENTSTATOM FB; SMITH SR; FICHTL GH et al.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 4; PP. 264-271; BIBL. 20 REF.Article

GAS-LASER BEHAVIOR IN A LOW-GRAVITY ENVIRONMENTOWEN RB.1981; OPT. LETT.; ISSN 0146-9592; USA; DA. 1981; VOL. 6; NO 7; PP. 331-333; BIBL. 18 REF.Article

USE OF RADIO EQUIPEMENT FOR SPACE SHUTTLE NAVIGATIONSCHIESSER ER.1978; I.E.E.E. TRANS. COMMUNIC.; USA; DA. 1978; VOL. 26; NO 11; PP. 1514-1520; BIBL. 15 REF.Article

SHUTTLE ACTIVE THERMAL CONTROL SYSTEM DEVELOPMENT TESTING = ESSAIS ACTIFS DU SYSTEME DE REGULATION DE TEMPERATURE DE LA NAVETTE SPATIALEFLEMING ML; HOWELL HR; DIETZ JB et al.1974; IN: AM. SOC. MECH. ENG. INTERSOC. CONF. ENVIRON. SYST.; SEATTLE; 1974; NEW YORK; A.S.M.E.; DA. 1974; VOL. 43; PP. 1-11Conference Paper

SIMULATION OF LOW THRUST GUIDANCE PROBLEMS.DAWKINS GS; LONG D.1974; AUTOMATICA; G.B.; DA. 1974; VOL. 10; NO 3; PP. 303-308; ABS. FR. ALLEM. RUSSE; BIBL. 7 REF.Article

SKYLAB: LE TRAIT D'UNION ENTRE APOLLO ET NAVETTE SPATIALEGEGERLE J.1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 317-321Serial Issue