Design procedures for combustion termination by nozzle area variation.
- 1 March 1966
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (3) , 419-425
- https://doi.org/10.2514/3.28462
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A theory of low-frequency combustion instability in solid rocket motorsAIAA Journal, 1964
- LOW PRESSURE ROCKET EXTINCTIONAIAA Journal, 1963
- Ignition of Solid Propellant Rocket Motors by Injection of Hypergolic FluidsARS Journal, 1961
- Rocket Thrust Termination TransientsARS Journal, 1959