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Turbopump systems for liquid rocket enginesThe 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.
Document ID
19750012398
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-SP-8107
Report Number: NASA-SP-8107
Accession Number
75N20470
Funding Number(s)
CONTRACT_GRANT: NAS3-12013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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