An approximate but complete model for the ignition response of solidpropellants.
- 1 May 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (5) , 872-877
- https://doi.org/10.2514/3.4612
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Heat-transfer processes during ignition of ignition of solid propellant rockets.Journal of Spacecraft and Rockets, 1967
- Ignition of ammonium perchlorate composite propellants by convectiveheating.AIAA Journal, 1966
- Theory of ignition of solid propellants.AIAA Journal, 1966
- Ignition of composite propellants by low radiant fluxesAIAA Journal, 1965
- Measurement of Heat Flux From Initiators for Solid PropellantsARS Journal, 1961
- Theory of Ignition Considered as a Thermal ReactionThe Journal of Chemical Physics, 1954