๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Burning rate anomaly of composite propellant grains

โœ Scribed by Hasegawa, H.; Fukunaga, M.; Kitagawa, K.; Shimada, T.

Book ID
121741174
Publisher
SP MAIK Nauka/Interperiodica
Year
2013
Tongue
English
Weight
783 KB
Volume
49
Category
Article
ISSN
0010-5082

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

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

The mechanism of burning rate catalysis
The mechanism of burning rate catalysis in composite HTPB๎—ธAP propellant combustion
โœ C.W. Fong; B.L. Hamshere ๐Ÿ“‚ Article ๐Ÿ“… 1986 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 646 KB

Evidence has been presented in this study that binder thermal degradation is rate limiting at low pressures (2-7 MPa) in HTPB/AP propellant combustion when catalyzed by copper chromite, Cr(Salen-N-decyl)3, and copper phthalocyanine. The condensed phase chemistry governing binder degradation is proba

Subatmospheric burning charaterristics o
Subatmospheric burning charaterristics of AP/CTPB composite propellants with burning rate modifiers
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