NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Replacement bearing for Rocketdyne SSME HPOTPs using alternate self-lubricating retainer materialsResearch was conducted to develop replacement bearings for the Rocketdyne Space Shuttle main engine (SSME) high pressure oxidizer turbopumps (HPOTPs). The replacement bearings consisted of standard balls and races with a special Battelle Self-Lubricating Insert Configuration (BASIC) retainer. The BASIC retainer consists of a phosphor bronze housing with inserts consisting of a polytetrafluoretheylene (PTFE) and bronze compound. The PTFE contacts the balls and the land guiding surface on the outer race. A PTFE transfer film is formed on balls and races, which lubricates the critical interfaces. The BASIC retainer is a one-to-one replacement for the current Armalon retainer, but has superior lubricating properties and is stronger over the broad temperature range anticipated for the HPOTP bearings. As a part of the project 40 sets of balls and races (two sizes) and 52 BASIC retainers were shipped to NASA/MSFC.
Document ID
19920019119
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gleeson, J.
(Battelle Columbus Labs. OH, United States)
Dufrane, K.
(Battelle Columbus Labs. OH, United States)
Kannel, J.
(Battelle Columbus Labs. OH, United States)
Date Acquired
September 8, 2013
Publication Date
April 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:184328
NASA-CR-184328
Report Number: NAS 1.26:184328
Report Number: NASA-CR-184328
Accession Number
92N28362
Funding Number(s)
CONTRACT_GRANT: NAS8-36996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available