kw.\*:("COMPOSITE PROPELLANT")
Results 1 to 25 of 295
Selection :
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
IGNITION OF COMPOSITE SOLID PROPELLANTS BY THE HOT PLATE TECHNIQUE.GIRDHAR HL; ARORA AJ.1978; COMBUST. AND FLAME; USA; DA. 1978; VOL. 31; NO 3; PP. 245-250; BIBL. 9 REF.Article
EXPERIMENTAL STUDY ON OSCILLATORY COMBUSTION IN SOLID-PROPELLANT MOTORS.KOREKI T; AOKI I; SHIROTA K et al.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 9; PP. 534-539; BIBL. 9 REF.Article
A MASS-SPECTROMETRIC INVESTIGATION OF THE CHEMISTRY OF PLATEAU BURNING PROPELLANTS.FARBER M; SRIVASTAVA RD.1978; COMBUST. AND FLAME; USA; DA. 1978; VOL. 31; NO 3; PP. 302-323; BIBL. 26 REF.Article
BREVET 2.360.537 (A1) (77 12308). - 22 AVRIL 1977. PROPERGOL SOLIDE ET SON PROCEDE DE PREPARATION.sdPatent
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
RECHERCHE ET DEVELOPPEMENT SUR LES PROPERGOLS COMPOSITES DES SYTEMES DE PROPULSION DE FUSEE SOLIDES AU JAPONTODA Y.1982; KOGYO KAYAKU. (JOURNAL OF THE INDUSTRIAL EXPLOSIVES SOCIETY, JAPAN); ISSN 0368-6450; JPN; DA. 1982; VOL. 43; NO 6; PP. 353-359; ABS. ENGArticle
Combustion behaviour of composite propellant at sub-atmospheric pressureSCHOYER, H. F. R; KORTING, P. A. O. G.Acta astronautica. 1986, Vol 13, Num 2, pp 55-61, issn 0094-5765Article
THE EFFECT OF STRAND SIZE ON THE LOW-PRESSURE DEFLAGRATION LIMIT OF A COMPOSITE PROPELLANTSOHN HY.1980; CHEM. ENGNG. COMMUNIC.; GBR; DA. 1980; VOL. 4; NO 2-3; PP. 307-312; BIBL. 6 REF.Article
ON THE BURNING RATE CHARACTERISTICS OF CMDB PROPELLANTSSWAMINATHAN V; SOOSAI MARIAN M.1979; PROPELL. AND EXPLOS.; DEU; DA. 1979; VOL. 4; NO 5; PP. 107-111; ABS. GER/FRE; BIBL. 5 REF.Article
DEVELOPMENT OF HTPB PROPELLANTS FOR THE SRAM MOTORMCGEE L; MUNSON WO; WALKER RB et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: IAAA; DA. 1978; 78-173; 7 P.Conference Paper
MODELES DE COMBUSTION INSTATIONNAIRE DES PROPERGOLS SOLIDES COMPOSITES.KUENTZMANN P.1978; RECH. AEROSPAT.; FRA; DA. 1978; NO 2; PP. 77-93; ABS. ENG; BIBL. 18 REF.Article
EFFECT OF LITHIUM AND AMMONIUM FLUORIDES ON AMMONIUM PERCHLORATE DECOMPOSITION.JAIN SR; PATIL KC; PAI VERNEKER VR et al.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 12; PP. 1807-1808; BIBL. 14 REF.Article
EFFECT OF PREHEATING ON THE BURNING RATE OF SOLID PROPELLANTS.PAI VERNEKER VR; KISHORE K; PRASAD G et al.1976; A.I. A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 9; PP. 1330-1331; BIBL. 6 REF.Article
INFLUENCE DE PARTICULES DE PERCHLORATE D'AMMONIUM SUR LA VITESSE DE COMBUSTION D'UN PROPERGOL COMPOSITE SOUS PRESSION ATMOSPHERIQUEITO T; HAGIHARA Y; NIIKURA O et al.1975; J. INDUSTR. EXPLOS. SOC. JAP.; JAP.; DA. 1975; VOL. 36; NO 6; PP. 313-319; ABS. ANGL.; BIBL. 4 REF.Article
KINETICS OF PROPELLANT DECOMPOSITIONKAUSHAL KISHORE; KASHYAP AK; GANGA PRASAD et al.1979; J. CHEM. TECHNOL. BIOTECHNOL.; GBR; DA. 1979; VOL. 29; NO 2; PP. 116-118; BIBL. 13 REF.Article
BREVET. PROCEDE DE MOULAGE PAR INJECTION SIMULTANEE DANS PLUSIEURS MOULES, ET APPAREILLAGE DE MOULAGE CORRESPONDANT1979; ; FRA; DA. 1979-09-28; FR/A1/2.415.530; DEP.78-02019/1978-01-25Patent
PROPERGOL HTPBYOKOYAMA A; KINAME S.1978; J. INDUSTR. EXPLOS. SOC. JAP.; JPN; DA. 1978; VOL. 39; NO 5; PP. 238-247; ABS. ENG; BIBL. 39 REF.Article
EFFECT OF PRESSURE ON HEAT OF EXPLOSION.GIRDHAR HL; ARORA AJ.1977; COMBUST. AND FLAME; U.S.A.; DA. 1977; VOL. 28; NO 3; PP. 291-293; BIBL. 7 REF.Article
IGNITION OF LAMINATED COMPOSITE PROPELLANTS COMPOSED OF AMMONIUM PERCHLORATE SINGLE CRYSTAL AND FUEL-BINDER SLAB BY MEANS OF CO2 LASER.SAITO T; MARUYAMA T; HIGASHI K et al.1977; COMBUST. SCI. TECHNOL.; G.B.; DA. 1977; VOL. 15; NO 3-4; PP. 161-168; BIBL. 3 REF.Article
APPLICATION OF SCHAPERY'S THEORY OF VISCOELASTIC FRACTURE TO SOLID PROPELLANT.SWANSON SR.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 9; PP. 528-533; BIBL. 26 REF.Article
BREVET 2.352.030 (A1) (77 01093). - 14 JANVIER 1977. COMPOSITION DE LIANT DURCISSABLE POUR PROPERGOL COMPOSITE ET APPLICATION.sdPatent
REACTION INTERMEDIATES DURING COMBUSTION AND DECOMPOSITION OF SOME MODEL SOLID ROCKET FUELSKISHORE K; VERNEKER VRP; GAYATHRI V et al.1981; FUEL (GUILDF.); ISSN 0016-2361; GBR; DA. 1981; VOL. 60; NO 2; PP. 164-167; BIBL. 17 REF.Article
CONTROLE DE LA VITESSE DE COMBUSTION DE PROPERGOLS HTPBTSUJIKADO N; OHYUMI Y; OHMURA I et al.1980; KOGYO KAYAKU; ISSN 0368-6450; JPN; DA. 1980; VOL. 41; NO 5; PP. 287-292; ABS. ENG; BIBL. 13 REF.Article
MODEL FOR STEADY STATE COMBUSTION OF UNIMODAL COMPOSITE SOLID PROPELLANTSKING MK.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 11 P.; BIBL. 6 REF.Conference Paper