kw.\*:("PROPERGOL COMPOSITE")
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BREVET 2.114.101 (B) (7041018). A 16 NOVEMBRE 1970. NOUVEAU PROCEDE DE FABRICATION DES BLOCS DE PROPERGOLS COMPOSITESsdPatent
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 2.131.136 (B) (7112436 ). A 8 AVRIL 1971. PERFECTIONNEMENTS AUX BLOCS DE PROPERGOLS A DEUX COMPOSITIONSsdPatent
BREVET 2.134.630 (B) (7215128). A 27 AVRIL 1972. COMPOSITION POUR CONE D'ALLUMAGEsdPatent
PROPELLANT COMBUSTION INSTABILITY AS MEASURED BY COMBUSTION RECOILMIHLFEITH CM; BAER AD; RYAN NW et al.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 10; PP. 1280-1285; BIBL. 16 REF.Serial Issue
EFFET DES PARTICULES DE AL SUR LA V DE COMBUSTION DE PROPERGOLS COMPOSITESTSUGANEZAWA Y; ITO T.1972; J. INDUSTR. EXPLOS. SOC.; JAP.; DA. 1972; VOL. 33; NO 4; PP. 207-213; ABS. ANGL.; BIBL. 8 REF.Serial Issue
PREDICTION OF THE CRITICAL DIAMETER OF COMPOSITE PROPELLANTSSALZMAN PK; DUNCAN TC.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 1117; PP. 1-9; BIBL. 9 REF.Conference Paper
BREVET 2.134.765 (B) (7113862). A 20 AVRIL 1971. PROPERGOL COMPOSITE A LIANT POLYURETHANE FONCTIONNANT AUX BASSES TEMPERATURESsdPatent
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
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
AN EXPERIMENTAL STUDY OF AMMONIUM PERCHLORATE-BINDER SANDWICH COMBUSTION IN STANDARD AND HIGH ACCELERATION ENVIRONMENTSBROWN WE; KENNEDY JR; NETZER DW et al.1972; COMBUST. SCI. TECHNOL.; G.B.; DA. 1972; VOL. 6; NO 4; PP. 211-222; BIBL. 21 REF.Serial Issue
BREVET 2.360.537 (A1) (77 12308). - 22 AVRIL 1977. PROPERGOL SOLIDE ET SON PROCEDE DE PREPARATION.sdPatent
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
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
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
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
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
MECHANICAL BEHAVIOR OF A POLYESTER COMPOSITE PROPELLANTWANG ASD; YUAN HL; TUNG TP 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. 1332; PP. 1-6Conference Paper
INFLUENCE OF LITHIUM FLUORIDE ON THE BURNING RATE OF AP-POLYESTER PROPELLANTDHAMEJA RK; SARADHY YP; JAIN VK et al.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 874; BIBL. 3 REF.Article