Model studies of the dynamics of launch vehicles.
- 1 June 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (6) , 936-938
- https://doi.org/10.2514/3.28568
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Supersonic combustion of storable liquid fuels in mach 3.0 to 5.0 air streamsSymposium (International) on Combustion, 1965
- Influence of injectant properties for fluid injection thrust vector controlJournal of Spacecraft and Rockets, 1964
- ANALYSIS OF THE FLUID MECHANICS OF SECONDARY INJECTION FOR THRUST VECTOR CONTROLAIAA Journal, 1963
- Approximate Analysis of Thrust Vector Control by Fluid InjectionARS Journal, 1961