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Radiative cooler for spacecraftThe design, construction, and testing of a passive radiative cooler that provides solutions to the design problems of withstanding mechanical stress, achieving the required thermal isolation, and maintaining optical alinement, cleanliness, and integration with the spacecraft are described.
Document ID
19730010146
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mccullough, J. E.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center The 7th Aerospace Mech. Symp.
Subject Category
Thermodynamics And Combustion
Accession Number
73N18873
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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