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Spacecraft thermal environments.Definitions are given for spacecraft-surface thermal environment characteristics. Lumped-parameter thermal network modeling techniques are derived for spacecraft thermal environment analysis. The application of these techniques to thermal/vacuum testing is described. A major computer program required by these techniques is outlined. It is noted that this approach has been used to determine thermal environments for the Skylab ATM.
Document ID
19730034694
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chapter, J. J.
(Martin Marietta Corp. Aerospace Div., Denver, Colo., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 10
Subject Category
Thermodynamics And Combustion
Accession Number
73A19496
Funding Number(s)
CONTRACT_GRANT: NAS8-24000
Distribution Limits
Public
Copyright
Other

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