Burning-rate behavior in aluminized wide-distribution AP composite propellants
โ Scribed by M. Q. Brewster; J. C. Mullen
- Book ID
- 110157481
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 2011
- Tongue
- English
- Weight
- 309 KB
- Volume
- 47
- Category
- Article
- ISSN
- 0010-5082
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
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
The burning rates of series of bi-and trimodal AP-HTPB propellants have been incorporated into an empirical statistical model which describes a hypothetical pentamodal polydisperse AP pseudopropellant. This pseudopropellant is the linear summation of five unimodal polydisperse AP pseudopropellants.