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Permanent Magnetic Bearing for Spacecraft ApplicationsA permanent, totally passive magnetic bearing rig was designed, constructed, and tested. The suspension of the rotor was provided by two sets of radial permanent magnetic bearings operating in the repulsive mode. The axial support was provided by jewel bearings on both ends of the rotor. The rig was successfully operated to speeds of 5500 rpm using an air impeller. Radial and axial stiffnesses of the permanent magnetic bearings were experimentally measured and then compared to finite element results. The natural damping of the rotor was measured and a damping coefficient was calculated.
Document ID
20080040677
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Morales, Winfredo
(NASA Glenn Research Center Cleveland, OH, United States)
Fusaro, Robert
(NASA Glenn Research Center Cleveland, OH, United States)
Kascak, Albert
(Army Research Lab. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2003-211996/REV1
E-13668-1
Meeting Information
Meeting: STLE Annual Meeting
Location: New York, NY
Country: United States
Start Date: April 27, 2003
End Date: May 2, 2003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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