Supersonic combustion of storable liquid fuels in mach 3.0 to 5.0 air streams
- 31 December 1965
- journal article
- Published by Elsevier in Symposium (International) on Combustion
- Vol. 10 (1) , 1167-1178
- https://doi.org/10.1016/s0082-0784(65)80253-3
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Influence of injectant properties for fluid injection thrust vector controlJournal of Spacecraft and Rockets, 1964
- LIQUID INJECTION THRUST VECTOR CONTROLAIAA Journal, 1963