Results of experiments performed at Johns Hopkins Univ on secondary gas injection into hot supersonic propellant flow in small rocket motor are presented; data on effects of injectant gas properties and injectant orifice size were obtained; motor operating conditions, nozzle geometry, and injectant location were kept fixed; main propellant was hot gas (catalytically decomposed 90% H2O 2), and motor conditions were held essentially constant.
Secondary gas injection in conical rocket nozzle
AIAA J
AIAA Journal ; 1 , n 2
1963
5 pages
Aufsatz (Zeitschrift)
Englisch
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SECONDARY GAS INJECTION IN A CONICAL ROCKET NOZZLE
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