A composite propellant subjected to radiant heating at the surface is theoretically investigated. Numerical solutions of the mathematical model which considers ignition as due to runaway chemical reactions at the propellant surface or in the adjacent gas-phase indicate that although inclusion of the
Role of condensed-phase reactions during the ignition of a composite solid propellant
โ Scribed by K. Kishore; V.R. Pai Verneker; M.R. Sunitha
- Publisher
- Elsevier Science
- Year
- 1977
- Tongue
- English
- Weight
- 328 KB
- Volume
- 19
- Category
- Article
- ISSN
- 0040-6031
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