IN SEARCH OF AN IDEALIZED MODEL OF HOMOGENEOUS SOLID PROPELLANT COMBUSTIONMILLER MS.1982; COMBUST. FLAME; ISSN 0010-2180; USA; DA. 1982; VOL. 46; NO 1; PP. 51-73; BIBL. 33 REF.Article

FLAME-SPREADING OVER THE SURFACE OF A SOLID PROPELLANT. I: EXPERIMENTAL RESULTSANDOH E; MIZOMOTO M; IKAI S et al.1981; COMBUST. SCI. TECHNOL.; ISSN 0010-2202; GBR; DA. 1981; VOL. 26; NO 3-4; PP. 135-146; BIBL. 10 REF.Article

FREQUENCY RESPONSE FUNCTION OF BURNING SOLID PROPELLANTSDE LUCA L.1980; MECCANICA; ISSN 0025-6455; ITA; DA. 1980; VOL. 15; NO 4; PP. 195-205; ABS. ITA; BIBL. 13 REF.Article

MODELING OF CONVECTIVE MODE COMBUSTION THROUGH GRANULATED PROPELLANT TO PREDICT DETONATION TRANSITION.KRIER H; GOKHALE SS.1978; A.I. A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 2; PP. 177-183; BIBL. 26 REF.Article

NON-LINEAR, NON-STEADY BURNING OF A SOLID PROPELLENT IN THREE CORDINATE SYSTEMS.COBBLE MH.1977; INTERNATION. J. NON-LINEAR MECH.; G.B.; DA. 1977; VOL. 12; NO 4; PP. 233-239; ABS. FR. ALLEM.; BIBL. 10 REF.Article

EXPERIMENTAL STUDY OF PRESSURE WAVE PROPAGATION IN GRANULAR PROPELLANT BED.ALKIDAS AC; MORRIS SO; CAVENY LH et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 6; PP. 789-792; BIBL. 10 REF.Article

IGNITION OF DOUBLE-BASE PROPELLANT IN A HOT STAGNATION-POINT FLOWNIIOKA T; TAKAHASHI M; IZUMIKAWA M et al.1979; COMBUST. AND FLAME; USA; DA. 1979; VOL. 35; NO 1; PP. 81-87; BIBL. 11 REF.Article

RESPONSE OF THREE TYPES OF TRANSIENT COMBUSTION MODELS TO GUN PRESSURIZATIONNELSON CW.1978; COMBUST. AND FLAME; USA; DA. 1978; VOL. 32; NO 3; PP. 317-319; BIBL. 8 REF.Article

EXPLOSIVE BEHAVIOR OF SIMPLIFIED PROPELLANT MODELS.PRICE D; CLAIRMONT AR JR.1977; COMBUST. AND FLAME; U.S.A.; DA. 1977; VOL. 29; NO 1; PP. 87-93; BIBL. 4 REF.Article

TEMPERATURE SENSITIVITY OF PROPELLANT BURNING RATES.CONDON JA; RENIE JP; OSBORN JR et al.1977; COMBUST. AND FLAME; U.S.A.; DA. 1977; VOL. 30; NO 3; PP. 267-276; BIBL. 10 REF.Article

A MATHEMATICAL MODEL TO PREDICT TRANSIENT BURNING RATE AND PRESSURE DECAY RATES FOR EXTINCTION OF COMPOSITE PROPELLANTS.SUHAS HK; BOSE TK.1977; COMBUST. AND FLAME; U.S.A.; DA. 1977; VOL. 28; NO 2; PP. 145-153; BIBL. 23 REF.Article

THEORIE DE LA STABILITE DE COMBUSTION DES PROPERGOLS SOLIDES PRENANT EN COMPTE LES INTERACTIONS DE PHASESASLANOV SK.1976; DOP. AKAD. NAUK UKRAJIN. R.S.R., A; S.S.S.R.; DA. 1976; NO 8; PP. 701-704; ABS. ANGL. RUSSE; BIBL. 10 REF.Article

ON THE NUMERICAL ACCURACY OF HOMOGENEOUS SOLID PROPELLAND COMBUSTION MODELSMILLER MS; COFFEE TP.1983; COMBUSTION AND FLAME; ISSN 0010-2180; USA; DA. 1983; VOL. 50; NO 1; PP. 75-88; BIBL. 11 REF.Article

FLAME SPREADING IN GRANULAR PROPELLANT: COMPARISON OF THEORY TO EXPERIMENTSHORST AW; NELSON CW; MAY IW et al.1978; A.I.A.A. J., NEW YORK; USA; DA. 1978; VOL. 16; NO 8; PP. 769-770; BIBL. 5 REF.Article

IGNITION DELAY OF COMPOSITE SOLID PROPELLANTS.GIRDHAR HL; ARORA AJ.1977; COMBUST. AND FLAME; U.S.A.; DA. 1977; VOL. 28; NO 2; PP. 109-111; BIBL. 5 REF.Article

COMMENT ON: A MODIFICATION OF THE COMPOSITE PROPELLANT EROSIVE BURNING MODEL OF LENOIR AND ROBILLARD.GLICK RL; KING MLK.1976; COMBUST. AND FLAME; U.S.A.; DA. 1976; VOL. 27; NO 3; PP. 405-408; BIBL. 7 REF.Article

Comments on cars probe of RDX decompositionSTUFFLEBEAM, J. H; ECKBRETH, A. C.Chemical physics letters. 1984, Vol 109, Num 1, pp 110-111, issn 0009-2614Article

Reply to comment on cars probe of RDX decompositionHARRIS, L. E.Chemical physics letters. 1984, Vol 109, Num 1, pp 112-113, issn 0009-2614Article

Solution Combustion Synthesis of Nanosized Copper Chromite and Its Use as a Burn Rate Modifier in Solid PropellantsSATHISKUMAR, P. S; THOMAS, C. R; MADRAS, Giridhar et al.Industrial & engineering chemistry research. 2012, Vol 51, Num 30, pp 10108-10116, issn 0888-5885, 9 p.Article

Importance of surface reactions during radiative ignition of composite solid propellantsKUMAR, R. K.Combustion and flame. 1985, Vol 59, Num 1, pp 63-68, issn 0010-2180Article

IGNITION TIMES OF COMPOSITE PROPELLANTS BASED ON NITRO-PHENOLIC BINDERSGIRDHAR HL; ARORA AJ; MALIK GN et al.1980; COMBUST. SCI. TECHNOL.; ISSN 0010-2202; GBR; DA. 1980; VOL. 23; NO 5-6; PP. 243-249; BIBL. 16 REF.Article

PRESSURE DEPENDENCE OF BURNING RATE OF NITROPHENOL-FORMALDEHYDE COMPOSITE PROPELLANTSGIRDHAR HL; ARORA AJ; MALIK GN et al.1980; COMBUST. FLAME; ISSN 0010-2180; USA; DA. 1980; VOL. 39; NO 3; PP. 283-286; BIBL. 9 REF.Article

THERMAL DECOMPOSITION AND COMBUSTION STUDIES ON POTASSIUM PERCHLORATE/POLYSTYRENE PROPELLANT SYSTEMSKISHORE K; PAI VERNEKER VR; SUNITHA MR et al.1980; AIAA J.; ISSN 0001-1452; USA; DA. 1980; VOL. 18; NO 8; PP. 966-967; BIBL. 11 REF.Article

MECHANISM OF CATALYTIC ACTIVITY OF TRANSITION METAL OXIDES ON SOLID PROPELLANT BURNING RATEKISHORE K; SUNITHA MR.1978; COMBUST. AND FLAME; USA; DA. 1978; VOL. 33; NO 1; PP. 311-314; BIBL. 22 REF.Article

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