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Results 1 to 25 of 2028

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ALLUMEURS DE PROPULSEURS A PROPERGOL SOLIDELARUE P.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 39; PP. 67-80; ABS. ANGL. ALLEM.; BIBL. 4 REF.Serial Issue

BREVET 2.234.246 (B) (7322267). A 19 JUIN 1973. CHARGEMENT PYROTECHNIQUE A PALIERS DE PRESSION DECROISSANTS ET PROCEDE DE GENERATION DE GAZ CHAUDSsdPatent

A NON LINEAR MODEL OF COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET ENGINESBURSTEIN SA; CHINITZ W; SCHECHTER HS et al.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 1146; PP. 1-14; BIBL. 9 REF.Conference Paper

DESIGN AND DEVELOPMENT OF A HOT PARTICLE IGNITERCROSBY R; MULLENIX GC; SWENSON I et al.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 1196; PP. 1-22Conference Paper

THERMAL STRUCTURAL OPTIMIZATION OF CRYOGENIC STORAGE SYSTEMSNAVICKAS J; MELTON HR.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 927-929Serial Issue

MESURE DE LA VITESSE DE COMBUSTION DES PROPERGOLS SOLIDES PAR ULTRASONSKUENTZMANN P; DEMARAIS JC; CAUTY F et al.1979; RECH. AEROSPAT.; FRA; DA. 1979; NO 1; PP. 55-72; ABS. ENG; BIBL. 12 REF.Article

BREVET PROCEDE DE MOULAGE A CHAUD DE BLOCS DE PROPERGOLS A DOUBLE BASE1978; ; FRA; DA. 1978-09-01; FR/A1/2.376.094; DEP.7639455/1976-12-29Patent

CRYOGENE LIQUID O2/H2 REACTION CONTROL SYSTEMS FOR SPACE SHUTTLEKELLY PJ; MCKEE HB; PATTEN TC et al.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1155; PP. 1-11; BIBL. 9 REF.Conference Paper

BREVET 2.213.254 (B) (7236739). A 17 OCTOBRE 1972. PROCEDE D'OBTENTION RAPIDE D'UN GRAND VOLUME DE GAZ NON TOXIQUE A TEMPERATURE MODEREE PAR COMBUSTION D'UN BLOC DE PROPERGOLsdPatent

MOYENS D'ETUDE EXPERIMENTALE DE LA COMBUSTION D'UN PROPERGOL SOLIDE METALLISE EN ROTATIONDOIN B; BRULARD J; LARUE P et al.1974; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FR.; DA. 1974; NO 229; PP. 1-38; ABS. ANGL.; BIBL. 18 REF.Article

CHEMICAL ENGINEERING IN SOLID PROPELLANT INDUSTRY.MURTHY JSN.1976; CHEM. ENGNG WORLD; INDIA; DA. 1976; VOL. 11; NO 12; PP. 67-70; BIBL. 7 REF.Article

PHENOMENES DE COMBUSTION DE PROPERGOLS SOLIDES. IVKUBOTA N.1980; KOGYO KAYAKU; ISSN 0368-6450; JPN; DA. 1980; VOL. 41; NO 5; PP. 255-261; ABS. ENGArticle

SPACE SHUTTLE BIPROPELLANT RCS ENGINE = MOTEUR RCS A DEUX PROPERGOLS POUR NAVETTE SPATIALESANSCRAINTE W; CHAZEN M.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 839; PP. 1-24; BIBL. 1 P.Conference Paper

IMPORTANCE OF CONDENSED-PHASE REACTIONS IN SOLID PROPELLANT COMBUSTIONPAI VERNEKER VR; KISHORE K; RADHAKRISHNAN NAIR MN et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1202; PP. 1-9; BIBL. 8 REF.Conference Paper

THE SIMULATION OF HIGH PRESSURE HYDROGEN/OXYGEN ROCKET ENGINES = LA SIMULATION DES MOTEURS DE FUSEE A HYDROGENE/OXYGENE A HAUTE PRESSIONHOPKINS H; KONOPKA W; LENG J et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-10; BIBL. 13 REF.Conference Paper

BREVET 2.121.356 (B) (7100174). A 6 JANVIER 1971. NOUVELLE COMPOSITION DE LINER POUR BLOCS DE PROPERGOLS, MOULES-COLLESsdPatent

BREVET 2.114.101 (B) (7041018). A 16 NOVEMBRE 1970. NOUVEAU PROCEDE DE FABRICATION DES BLOCS DE PROPERGOLS COMPOSITESsdPatent

THE CLOSED BOMB TEST FOR THE ASSESSMENT OF SOLID PROPELLANT GRAINS UTILIZED IN GUNSSHIMPI SA; KRIER H.1975; COMBUST. AND FLAME; U.S.A.; DA. 1975; VOL. 25; NO 2; PP. 229-240; BIBL. 12 REF.Article

CONTRIBUTION A L'ETUDE DES PERTES D'IMPULSION SPECIFIQUE DANS LES FUSEES A PROPERGOL SOLIDEKUENTZMANN P.1973; AO-CNRS-8969; FR.; DA. 1973; PP. 1-138; H.T. 31; BIBL. 6 P. 1/2; (THESE DOCT. SCI. PHYS.; PARIS)Thesis

INFLUENCE DE LA DIFFUSION D'UN GAZ INERTE SUR LA MESURE DE LA CHALEUR D'EXPLOSION DE PROPERGOLS A DOUBLE BASEKIMURA J; KUBOTA N.1976; J. INDUSTR. EXPLOS. SOC. JAP.; JAP.; DA. 1976; VOL. 37; NO 1; PP. 22-28; ABS. ANGL.; BIBL. 8 REF.Article

THE THERMAL DECOMPOSITION OF NITROGLYCERIN AND ITS RELATION TO THE STABILITY OF CMBD PROPELLANTSHARTMAN KO; MUSSO RC.sdIN: FALL MEET. WEST. STATES SECT. COMBUST. INST.; 1972; S.L.; DA. S.D.; VOL. 7; PP. 1-29; BIBL. 1 P. 1/2Conference Paper

BREVET 1.605.107 (P.V.908.872). A 7 SEPTEMBRE 1962. PROCEDE POUR LA PREPARATION DE CHARGES DE PROPERGOLS COMPOSITES AVEC UTILISATION DE COMBURANTS LIQUIDES STABLES A TEMPERATURE NORMALEsdPatent

BREVET 2.134.630 (B) (7215128). A 27 AVRIL 1972. COMPOSITION POUR CONE D'ALLUMAGEsdPatent

FLAME SPREADING PHENOMENA IN DOUBLE BASE PROPELLANTSSIDDIQUI KM; SMITH IE.1975; COMBUST. AND FLAME; U.S.A.; DA. 1975; VOL. 25; NO 3; PP. 335-341; BIBL. 7 REF.Article

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

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