Results obtained with technique of obtaining thrust vector control by injection of various liquids into supersonic region of rocket nozzle; liquids studied were water, Freon-12, perchloroethylene, nitrogen tetroxide, and bromine; unsymmetrical dimethylhydrazine and inhibited red fuming nitric acid were injected simultaneously to explore effect of energy release in nozzle exit cone with bipropellant injection; data on relationships of side force to injectant flow rate, effect of axial location of injection port, pressure, and properties.
Liquid injection thrust vector control
AIAA J
AIAA Journal ; 1 , n 3
1963
6 pages
Aufsatz (Zeitschrift)
Englisch
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Liquid-Injection Thrust Vector Control.
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