Dependence of the burning rate of a composite propellant on the chemical structure of the fuel
โ Scribed by L. D. Romodanova; V. I. Pepekin; A. Ya. Apin; P. F. Pokhil
- Book ID
- 112393584
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 1973
- Tongue
- English
- Weight
- 319 KB
- Volume
- 6
- Category
- Article
- ISSN
- 0010-5082
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๐ SIMILAR VOLUMES
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
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