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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.
Document ID
19840004171
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Frank Nola (Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1983
Publication Information
Publication: Integrated Flywheel Technology 1983
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Meeting: Proceedings of a workshop held at NASA Goddard Space Flight Center
Location: Greenbelt, MD
Country: US
Start Date: August 2, 1983
End Date: August 3, 1983
Sponsors: Goddard Space Flight Center
Accession Number
84N12239
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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