Liquid rocket engine axial-flow turbopumps, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical)

NASA/SP-8125, Scheer, D. D., Liquid rocket engine axial-flow turbopumps, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), April,1978, pp. 130, Format(s): PDF 11578k

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The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pump rotor assembly, pump materials for liquid hydrogen applications, and safety factors as utilized in state of the art pumps are among the topics discussed. Axial pump applications are included.

Keywords:	spacecraft propulsion and power, axial flow pumps, engine design, liquid propellent rocket engines, spacecraft desian, chemical propulsion, hydrodynamics, liquid hydrogen, rotors, safety factors, stators, technology assessment
CASI Document ID Number:	78N31164
Subjects:	Astronautics: Spacecraft Propulsion And Power
ID Code:	190
Deposited On:	10 June 2002