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Fabrication and evaluation of aluminum heat pipesAn evaluation is presented for the current heat pipe system on the OAO spacecraft, in order to increase its capability for future missions. A detailed analysis was made of the requirements, and approaches for the design of optimized heat pipes to meet future needs were identified. A composite wick heat pipe was developed, which has significantly higher transport capability than those of conventional wick design.
Document ID
19720015291
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 6, 2013
Publication Date
July 1, 1970
Subject Category
Thermodynamics And Combustion
Report/Patent Number
DTM-70-2
NASA-CR-122380
Report Number: DTM-70-2
Report Number: NASA-CR-122380
Accession Number
72N22941
Funding Number(s)
CONTRACT_GRANT: NAS5-11271
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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