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Top-off procedure for space-bound superfluid helium cryostatsTests have been carried out on the transfer of pressurized liquid helium, slightly above the lambda temperature, in order to determine the optimum transfer parameters for a ground-based top-off just prior to launch. It is shown that the maximum mass fill of a spaceborne cryostat can be accomplished with the low-pressure top-off after initial fill with normal helium. The realistic maximum fill at temperatures below the lambda temperature can be expected to be at least 90 percent, which results in about 40 to 50 percent more mass at launch than without the top-off. In each case, specific ground support equipment is required to satisfy the individual cryostat requirements and extreme care is necessary during the transfer procedure.
Document ID
19830062030
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Petrac, D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Engineering (General)
Meeting Information
Meeting: Advances in cryogenic engineering. Volume 27 - Proceedings of the Cryogenic Engineering Conference
Location: San Diego, CA
Start Date: August 11, 1981
End Date: August 14, 1981
Accession Number
83A43248
Distribution Limits
Public
Copyright
Other

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