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Self-driven cooling loop for a large superconducting magnet in spacePressurized cooling loops in which superfluid helium circulation is driven by the heat being removed have been previously demonstrated in laboratory tests. A simpler and lighter version which eliminates a heat exchanger by mixing the returning fluid directly with the superfluid helium bath was analyzed. A carefully designed flow restriction must be used to prevent boiling in this low-pressure system. A candidate design for Astromag is shown that can keep the magnet below 2.0 K during magnet charging. This gives a greater margin against accidental quench than approaches that allow the coolant to warm above the lambda point. A detailed analysis of one candidate design is presented.
Document ID
19920041224
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mord, A. J.
(Ball Aerospace Systems Group, Ball Electro-Optics/Cryogenics Div., Boulder CO, United States)
Snyder, H. A.
(Colorado, University Boulder, 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
92A23848
Funding Number(s)
CONTRACT_GRANT: NAGW-1388
Distribution Limits
Public
Copyright
Other

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