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Flywheel ElectronicsRequirements of the flywheel electronic system are to accelerate the momentum wheel to a fixed maximum speed when solar energy is available and to maintain a constant voltage on the spacecraft bus under varying loads when solar energy is not available. Requirements, energy flow control, types of motors considered, type of electronic control, and efficiency considerations, are outlined.
Document ID
19840004171
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nola, F. J. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1983
Publication Information
Publication: NASA. Langley Research Center Integrated Flywheel Technol., 1983
Subject Category
Spacecraft Propulsion And Power
Accession Number
84N12239
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19840004160Collected WorksIntegrated Flywheel Technology, 1983
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