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Simplified thermal estimation techniques for large space structuresA tool for making rapid estimates of the response of space structures to thermal environments encountered in earth orbits is provided for the designer of these structures. Charts giving heating rates and temperatures for certain typical large spacecraft structural elements are provided. Background information for spacecraft thermal design considerations is presented. Environments, requirements, thermal control techniques, design guidelines, and approaches available for more detailed thermal response analysis are discussed.
Document ID
19780005162
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brogren, E. W. (Boeing Aerospace Co. Huntsville, AL, United States)
Barclay, D. L. (Boeing Aerospace Co. Huntsville, AL, United States)
Straayer, J. W. (Boeing Aerospace Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-145253
D180-19334-2
Report Number: NASA-CR-145253
Report Number: D180-19334-2
Accession Number
78N13105
Funding Number(s)
CONTRACT_GRANT: NAS1-13967
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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