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DEPENDENCE OF BURNING RATE OF COMPOSITE SOLID PROPELLANTS ON PRESSURERASTOGI RP; RAM RAJ SINGH; RAO AP et al.1982; COMBUST. FLAME; ISSN 0010-2180; USA; DA. 1982; VOL. 45; NO 2; PP. 205-207; BIBL. 10 REF.Article

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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

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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

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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

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