Mechanical Design of a Curtis Turbine for the Oxidizer Turbopump of the M-1 Engine
1966
169 pages
Report
No indication
English
Jet & Gas Turbine Engines , M- 1 rocket engine , Turbine , Turbopump , Aerodynamic , Assembly , Design , Exhaust , Function , Inlet , Interface , Manifold , Material , Mechanical , Nozzle , Oxidizer , Property , Reverse , Rotor , Row , Structural , System , Weight
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