Oxidizer Size Distribution Effects on Propellant Combustion
- 1 August 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (8) , 877-883
- https://doi.org/10.2514/3.61240
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The Effect of Oxidizer Particle Size Distribution on the Steady and Nonsteady Combustion of Composite Propellants.Published by Defense Technical Information Center (DTIC) ,1978
- On Statistical Analysis of Composite Solid Propellant CombustionAIAA Journal, 1974
- A model of composite solid-propellant combustion based on multiple flamesAIAA Journal, 1970
- A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat GenerationAIAA Journal, 1966
- Burning Mechanism of Ammonium Perchlorate PropellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1960