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Heat pipe investigationsTechniques associated with thermal-vacuum and bench testing, along with flight testing of the OAO-C spacecraft heat pipes are outlined, to show that the processes used in heat transfer design and testing are adequate for good performance evaluations.
Document ID
19730023095
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Marshburn, J. P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
G-7311
NASA-TN-D-7219
Report Number: G-7311
Report Number: NASA-TN-D-7219
Accession Number
73N31827
Funding Number(s)
PROJECT: RTOP 831-41-25-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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