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Orbital heat rate packagePackage consisting of three separate programs used to accurately predict temperature distribution of spacecraft in planetary orbit is invaluable tool for design and analysis of other structures that must function in complex thermal environment.
Document ID
19780000554
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Lovin, J. K. (Lockheed Missiles and Space Co.)
Spradley, L. W. (Lockheed Missiles and Space Co.)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-23980
Accession Number
78B10554
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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