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Hybrid bearings for LH2 and LO2 turbopumpsHybrid combinations of hydrostatic and ball bearings can improve bearing performance for liquid hydrogen and liquid oxygen turbopumps. Analytic studies were conducted to optimize hybrid bearing designs for the SSME-type turbopump conditions. A method to empirically determine damping coefficients was devised. Four hybrid bearing configurations were designed, and three were fabricated. Six hybrid and hydrostatic-only bearing configurations will be tested for steady-state and transient performance, and quantification of damping coefficients. The initial tests were conducted with the liquid hydrogen bearing.
Document ID
19850018569
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Butner, M. F.
(Rockwell International Corp. Canoga Park, CA, United States)
Lee, F. C.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA. Marshall Space Flight Center Advan. High Pressure O2(H2 Technol.
Subject Category
Mechanical Engineering
Accession Number
85N26880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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