Initial temperature and pressure effects on composite solid-propellant burning rates - Comparisons with theory
- 1 August 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (8) , 1439-1443
- https://doi.org/10.2514/3.5921
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A phalanx flame model for the combustion of composite solid propellantsCombustion and Flame, 1968
- Burning Mechanism of Ammonium Perchlorate PropellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1960