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An evaluation of bearings operating in a cryogenic environment with silicon nitride rolling elementsThe bearings used in the space shuttle main engine (SSME) high pressure oxidizer turbopump (HPOTP) do not meet the expected life goals that were set for them. In an effort to improve their performance, many solutions are being studied. New bearing materials are being developed, better manufacturing techniques are being investigated, and improved cage materials for better lubrication are being tested. The focus is on the replacement of steel balls with ones made of silicon nitride in 57-mm HPOTP bearings. The bearings were then installed in a test rig and run at near turbopump operating conditions. The results from this test series are encouraging, with silicon nitride showing good wear resistance and thermal stability.
Document ID
19910009123
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gibson, H. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:103524
NASA-TM-103524
Report Number: NAS 1.15:103524
Report Number: NASA-TM-103524
Accession Number
91N18436
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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