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Low gravity thermal stratification of liquid helium on SHOOTEstimates of the extent and impact of thermal stratification are presented as well as predictions of the behavior of the HeI/HeII boundary. Although thermal stratification of cryogens can be problematic and lead to their inefficient use in low gravity, for SHOOT the occurrence is beneficial both during ground hold and in orbit and presents no hazards. On the ground the parasitic heat load is both reduced and more efficiently removed. In orbit the pumpdown proceeds at a much more rapid rate, allowing orbital operations to begin earlier. The thermal conductivity of the aluminum tank and the normal liquid plus cooling at the liquid/vapor interface as the vapor bubble grows are sufficient to prevent undesirably high vapor pressures in the tank.
Document ID
19920041216
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Shirron, P. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Dipirro, M. J.
(NASA Goddard Space Flight Center Greenbelt, MD, 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
92A23840
Distribution Limits
Public
Copyright
Other

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