Burning rate temperature sensitivity of composite solid propellants
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (3) , 290-292
- https://doi.org/10.2514/3.30262
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Mechanism of the decomposition of ammonium perchlorateCombustion and Flame, 1969
- Location of action of burning-rate catalysts in composite propellantcombustion.AIAA Journal, 1969
- Temperature sensitivity of solid propellant burning rate.AIAA Journal, 1967
- A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat GenerationAIAA Journal, 1966
- The Correlation of Interior Ballistic Data for Solid PropellantsJournal of Jet Propulsion, 1954