Gao Hanru, chen Qizhi, Yang Loping. EXPERIMENTAL RESEARCH ON A BIPROPELLANT THROTTLING LIQUID ROCKET ENGINE WITH CONTROLLABLE INJECTOR AND THROTTLING CAVITATING VENTURI[J]. Journal of Aerospace Power, 1989, 4(1): 45-49,91.
Citation:
Gao Hanru, chen Qizhi, Yang Loping. EXPERIMENTAL RESEARCH ON A BIPROPELLANT THROTTLING LIQUID ROCKET ENGINE WITH CONTROLLABLE INJECTOR AND THROTTLING CAVITATING VENTURI[J]. Journal of Aerospace Power, 1989, 4(1): 45-49,91.
Gao Hanru, chen Qizhi, Yang Loping. EXPERIMENTAL RESEARCH ON A BIPROPELLANT THROTTLING LIQUID ROCKET ENGINE WITH CONTROLLABLE INJECTOR AND THROTTLING CAVITATING VENTURI[J]. Journal of Aerospace Power, 1989, 4(1): 45-49,91.
Citation:
Gao Hanru, chen Qizhi, Yang Loping. EXPERIMENTAL RESEARCH ON A BIPROPELLANT THROTTLING LIQUID ROCKET ENGINE WITH CONTROLLABLE INJECTOR AND THROTTLING CAVITATING VENTURI[J]. Journal of Aerospace Power, 1989, 4(1): 45-49,91.
A bipropellant throttling liquid rocket engine with controllable injector and throttling cavitating venturi has been designed,tested and analyzed.In result the relationships of pressure, pressure recovery coefficient of venturi, stroke of injector pintle, propellant flow rate and mixture ratio, combustion efficiency, specific impulse, thrust, stability and response time to control voltage signal are obtained and the corresponding plots and data are also presented.
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