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Design criteria monograph on turbopump systemsTurbopump assembly for modern liquid propellant rocket engine is complete system in itself. It consists of many components, some of which are themselves subsystems. Monograph deals with turbopump as system, covering selection of proper system type for each application and integration of components into working system.
Document ID
19750000135
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Date Acquired
August 8, 2013
Publication Date
July 1, 1975
Subject Category
Mechanics
Report/Patent Number
LEW-12499
Report Number: LEW-12499
Accession Number
75B10135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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