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Studies on Nonaluminized High Burning Rate AP-Composite Propellants

โœ Scribed by GORE, G. M.; NAZARE, A. N.; DIVEKAR, C. N.; HAIT, S. K.; ASTHANA, S. N.

Book ID
120372058
Publisher
Taylor and Francis Group
Year
2004
Tongue
English
Weight
196 KB
Volume
22
Category
Article
ISSN
0737-0652

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โœ S. Krishnan; R. Jeenu ๐Ÿ“‚ Article ๐Ÿ“… 1990 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 455 KB

While burning at subatmospheric pressure, composite propellants generally fume and under certain conditions eject partially reacted particles. This characteristic property is exploited in this study to understand the mechanism of burning rate modification. The additives CuCr204, Fe203, Sb2 03, AI(OH