Theoretical study of propellant behavior during thrust chamber depressurization
- 1 October 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (10) , 1884-1890
- https://doi.org/10.2514/3.5476
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Design procedures for combustion termination by nozzle area variation.Journal of Spacecraft and Rockets, 1966
- LOW PRESSURE ROCKET EXTINCTIONAIAA Journal, 1963
- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961