Turbopump systems for liquid rocket engines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8107, Turbopump systems for liquid rocket engines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), August,1974, pp. 168, Format(s): PDF 9814k

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The turbopump system, from preliminary design through rocket engine testing is examined. Selection of proper system type for each application and integration of the components into a working system are dealt with. Details are also given on the design of various components including inducers, pumps, turbines, gears, and bearings.

Keywords:	spacecraft propulsion and power, liquid propellant rocket engines, turbine pumps, performance prediction, reliability engineering, systems engineering
CASI Document ID Number:	75N20470
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	158
Deposited On:	23 May 2002