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Cryogenic Magnetic Bearing Test Facility (CMBTF)The Cryogenic Magnetic Bearing Test Facility (CMBTF) was designed and built to evaluate compact, lightweight magnetic bearings for use in the SSME's (space shuttle main engine) liquid oxygen and liquid hydrogen turbopumps. State of the art and tradeoff studies were conducted which indicated that a hybrid permanent magnet bias homopolar magnetic bearing design would be smaller, lighter, and much more efficient than conventional industrial bearings. A test bearing of this type was designed for the test rig for use at both room temperature and cryogenic temperature (-320 F). The bearing was fabricated from state-of-the-art materials and incorporated into the CMBTF. Testing at room temperature was accomplished at Avcon's facility. These preliminary tests indicated that this magnetic bearing is a feasible alternative to older bearing technologies. Analyses showed that the hybrid magnetic bearing is one-third the weight, considerably smaller, and uses less power than previous generations of magnetic bearings.
Document ID
19920021920
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:189087
NASA-CR-189087
Report Number: NAS 1.26:189087
Report Number: NASA-CR-189087
Accession Number
92N31164
Funding Number(s)
CONTRACT_GRANT: NAS3-25572
PROJECT: RTOP 590-21-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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