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Cryogenic thermal control technology summariesA summarization and categorization is presented of the pertinent literature associated with cryogenic thermal control technology having potential application to in-orbit fluid transfer systems and/or associated space storage. Initially, a literature search was conducted to obtain pertinent documents for review. Reports determined to be of primary significance were summarized in detail. Each summary, where applicable, consists of; (1) report identification, (2) objective(s) of the work, (3) description of pertinent work performed, (4)major results, and (5) comments of the reviewer (GD/C). Specific areas covered are; (1) multilayer insulation of storage tanks with and without vacuum jacketing, (2) other insulation such as foams, shadow shields, microspheres, honeycomb, vent cooling and composites, (3) vacuum jacketed and composite fluid lines, and (4) low conductive tank supports and insulation penetrations. Reports which were reviewed and not summarized, along with reasons for not summarizing, are also listed.
Document ID
19750005989
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stark, J. A. (General Dynamics/Convair San Diego, CA, United States)
Leonhard, K. E. (General Dynamics/Convair San Diego, CA, United States)
Bennett, F. O., Jr. (General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
CASD-NAS-74-067
NASA-CR-134747
Accession Number
75N14061
Funding Number(s)
CONTRACT_GRANT: NAS3-17814
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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