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Heat pipe investigationsThe OAO-C spacecraft has three circular heat pipes, each of a different internal design, located in the space between the spacecraft structural tube and the experiment tube, which are designed to isothermalize the structure. Two of the pipes are used to transport high heat loads, and the third is for low heat loads. The test problems deal with the charging of the pipes, modifications, the mobile tilt table, the position indicator, and the heat input mechanisms. The final results showed that the techniques used were adequate for thermal-vacuum testing of heat pipes.
Document ID
19730003240
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Marshburn, J. P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
X-322-72-153
NASA-TM-X-66072
Report Number: X-322-72-153
Report Number: NASA-TM-X-66072
Accession Number
73N11967
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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