๐”– Bobbio Scriptorium
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Burning rates of solid propellants

โœ Scribed by J. M. Smith

Publisher
American Institute of Chemical Engineers
Year
1960
Tongue
English
Weight
772 KB
Volume
6
Category
Article
ISSN
0001-1541

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๐Ÿ“œ SIMILAR VOLUMES

Dependence of burning rate of composite
Dependence of burning rate of composite solid propellants on pressure
โœ R.P. Rastogi; Ram Raj Singh; Anand P. Rao ๐Ÿ“‚ Article ๐Ÿ“… 1982 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 164 KB

Various theories [1,2] have been proposed for the pressure dependence of burning rate of composite propellants since a knowledge of this pressure dependence is vital for the design of a solid propellant rocket motor. Recently, Girdhar and Arora [3] have measured the burning rate of phenol-formaldehy

Burning rate catalysts for composite sol
Burning rate catalysts for composite solid propellants
โœ R.P. Rastogi; Gurdip Singh; Ram Raj Singh ๐Ÿ“‚ Article ๐Ÿ“… 1977 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 506 KB

The combustion of composite solid propellants was studied using ammonium dichromate, chromium carbonate, chromium oxide, basic copper carbonate and cupric oxide as additives. Burning rates were considerably enhanced in each case. Flame temperatures were measured and found to be higher than in cases