Theory of dynamic extinguishment of solid propellants with special reference to nonsteady heat feedback law
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (3) , 251-258
- https://doi.org/10.2514/3.30256
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
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- Contribution of solid-phase heat release to AP composite-propellant burning rate.AIAA Journal, 1968
- Nonsteady burning phenomena of solid propellants - Theory and experiments.AIAA Journal, 1968
- REVIEW OF SOVIET TRANSIENT COMBUSTION RESEARCHPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
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- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961
- M. Combustion of Solid PropellantsPublished by Walter de Gruyter GmbH ,1956