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Augmented orbiter heat rejection studySpacecraft radiator concepts are presented that relieve attitude restrictions required by the shuttle orbiter space radiator for baseline and extended capability STS missions. Cost effective heat rejection kits are considered which add additional capability in the form of attached spacelab radiators or a deployable radiator module.
Document ID
19810016600
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hixon, C. W. (Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
February 18, 1981
Subject Category
Space Transportation
Report/Patent Number
REPT-2-53020/IR-52679
NASA-CR-160992
Report Number: REPT-2-53020/IR-52679
Report Number: NASA-CR-160992
Accession Number
81N25135
Funding Number(s)
CONTRACT_GRANT: NAS9-14907
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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