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An analytical and experimental evaluation of shadow shields and their support membersExperimental tests were performed on a model shadow shield thermal protection system to examine the effect of certain configuration variables. The experimental results were used to verify the ability of an analytical program to predict the shadow shield performance including the shield-support interaction. In general, the analysis (assuming diffuse surfaces) agreed well with the experimental support temperature profiles. The agreement for the shield profiles was not as good. The results demonstrated: (1) shadow shields can be effective in reducing the heat transfer into cryogenic propellant tanks, and (2) the conductive heat transfer through supports can be reduced by selective surface coatings.
Document ID
19720020316
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stochl, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Boyle, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
E-7023
NASA-TM-X-68099
Report Number: E-7023
Report Number: NASA-TM-X-68099
Meeting Information
Meeting: Cryog. Eng. Conf.
Location: Boulder, CO
Country: United States
Start Date: August 9, 1972
End Date: August 11, 1972
Accession Number
72N27966
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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