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Liquid rocket engine axial-flow turbopumpsThe 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.
Document ID
19780023221
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Authors
Scheer, D. D. (NASA Lewis Research Center Cleveland, OH, United States)
Huppert, M. C. (Rocketdyne Cleveland, OH, United States)
Viteri, F. (Aerojet Liquid Rocket Co.)
Farquhar, J. (Aerojet Liquid Rocket Co.)
Keller, R. B., Jr. (NASA Lewis Research Center)
Date Acquired
September 3, 2013
Publication Date
April 1, 1978
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-SP-8125
Report Number: NASA-SP-8125
Accession Number
78N31164
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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