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Cooling options for AstromagA comparison of the various cooling options for the Astromag particle physics experiment is presented. The baseline design for the cryogenic system involves using a natural circulation fountain-effect driven flow loop (Hofmann type). The present paper considers two alternative options for cooling. The first design involves a thermal strap made of a high-conductivity metal, e.g., high-purity aluminum or copper, which connects the coil to the helium reservoir. Venting helium vapor can also be used to minimize the temperature of the magnet and recover from a quench. The second design is based on an He II heat pipe concept where steady state heat transport is by counterflow. Cavitation is prevented by use of a porous plug. Forced flow He II is also available but only during extraordinary operating conditions.
Document ID
19920041206
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Maytal, B. Z.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Van Sciver, S. W.
(Wisconsin, University Madison, 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
Engineering (General)
Accession Number
92A23830
Funding Number(s)
CONTRACT_GRANT: NAG5-1417
Distribution Limits
Public
Copyright
Other

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