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Centrifugal pumps for rocket enginesThe use of centrifugal pumps for rocket engines is described in terms of general requirements of operational and planned systems. Hydrodynamic and mechanical design considerations and techniques and test procedures are summarized. Some of the pump development experiences, in terms of both problems and solutions, are highlighted.
Document ID
19750003130
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Campbell, W. E. (Aerojet Nuclear Systems Co. Azusa, CA, United States)
Farquhar, J. (Aerojet Nuclear Systems Co. Azusa, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Publication Information
Publication: Pennsylvania State Univ. Fluid Mech., Acoustics, and Design of Turbomachinery, Pt. 2
Subject Category
Mechanical Engineering
Accession Number
75N11202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19750003119Collected WorksFluid mechanics, acoustics, and design of turbomachinery, part 2
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