Prediction of solid propellant burning rates in nozzleless motors
- 21 June 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Experimental and theoretical study of the effects of pressure and crossflow velocity on composite propellant burning rateSymposium (International) on Combustion, 1981
- A model of the effects of pressure and crossflow velocity on composite propellant burning ratePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Model for steady-state combustion of unimodal composite solid propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Simulative Study on the Erosive Burning of Solid Rocket MotorsAIAA Journal, 1976