Liquid Rocket Engine Turbopump Inducers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion)

NASA/SP-8052, Liquid Rocket Engine Turbopump Inducers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), NASA Lewis Research Center (Cleveland, OH, United States), May,1971, pp. 107, Format(s): PDF 5966k

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Design criteria for liquid rocket engine turbopump inducers

Keywords:	propulsion systems, aerospace engineering, intake systems, liquid propellant, rocket engines, turbine pumps, cavitation flow, hydrodynamics, mathematical models, optimization, turbine blades
CASI Document ID Number:	71N34950
Subjects:	Astronautics: Spacecraft Propulsion And Power: Rocket Engines, Nozzles And Thrust Chambers
ID Code:	95
Deposited On:	15 May 2002