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The Astromag superconducting magnet facility configured for a free-flying satelliteThe magnet parameters of a free-flying version of Astromag and the parameters of the space cryogenic system for the magnet are presented. Consideration is given to the free-flyer version of the Astromag magnet. The diameter of the magnet, its cryostat, the satellite and the two instruments is limited by the 4.27-m shroud diameter of the Atlas IIa. The magnet coil must use a stable reliable superconductor which can carry the full magnet current at 4.2 K at a peak induction in the coil of 7.5 T. The magnet must operate in the persistent mode. The changes in the overall design and operating requirements for the free-flying-design Astromag suggest that the coils, the cryogenic system, and the charging system can be simplified without a loss of required magnet function. Attention is given to switches, trim coils, and plumbing in the low field region between the coils; the magnet charging system and the quench protection system; and cooled helium supply to the magnet gas-cooled electrical leads.
Document ID
19920041205
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Green, M. A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Smoot, G. F.
(Lawrence Berkeley Laboratory Berkeley, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: Cryogenics
Volume: 32
Issue: 2 19
ISSN: 0011-2275
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
92A23829
Funding Number(s)
CONTRACT_GRANT: NASA ORDER S-556472-D
CONTRACT_GRANT: DE-AC03-76SF-00098
Distribution Limits
Public
Copyright
Other

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