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Spacecraft radiator systemsA spacecraft radiator system designed to provide structural support to the spacecraft. Structural support is provided by the geometric "crescent" form of the panels of the spacecraft radiator. This integration of radiator and structural support provides spacecraft with a semi-monocoque design.
Document ID
20120007608
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
Authors
Anderson, Grant A.
Date Acquired
August 25, 2013
Publication Date
April 17, 2012
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-12/428,421
Patent Number: US-Patent-8,157,217
Funding Number(s)
CONTRACT_GRANT: NNJ05JD49C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,157,217
Patent Application
US-Patent-Appl-SN-12/428,421

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