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Combustion of Double-Base Propellants

The approach taken in the development of an analytical model for the combustion of double-base propellants has been based on the decomposition behavior of the two principal propellant ingredients, nitrocellulose and nitroglycerin. The results of several studies reviewed by Huggett (HI2) and Adams (Al) show that nitrocellulose undergoes exothermic decomposition between 90° and 175°C. In this temperature range, the rate of decomposition follows the simple first-order expression... [Pg.31]

Adams, G. K., and Wiseman, L. A., The Combustion of Double-Base Propellants, Selected Combustion Problems, Butter-worth s Scientific Publications, London, 1954, pp. 277-288. [Pg.141]

Heath, G. A., and Hirst, R., Some Characteristics of the High-Pressure Combustion of Double-Base Propellants, 8 th Symposium (International) on Combustion, Williams WiDdns Co., Baltimore, 1962, pp. 711-720. [Pg.142]

See other pages where Combustion of Double-Base Propellants is mentioned: [Pg.1]    [Pg.31]    [Pg.143]    [Pg.143]    [Pg.144]    [Pg.146]    [Pg.148]    [Pg.150]    [Pg.152]    [Pg.154]    [Pg.156]    [Pg.158]    [Pg.160]    [Pg.162]    [Pg.164]    [Pg.166]    [Pg.168]    [Pg.170]    [Pg.172]    [Pg.174]    [Pg.176]    [Pg.178]    [Pg.180]    [Pg.143]    [Pg.143]    [Pg.144]    [Pg.146]    [Pg.148]    [Pg.150]    [Pg.152]    [Pg.154]    [Pg.156]    [Pg.158]    [Pg.160]    [Pg.162]    [Pg.164]    [Pg.166]    [Pg.168]    [Pg.170]    [Pg.172]    [Pg.174]    [Pg.176]    [Pg.178]    [Pg.180]   


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