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Evaluation of commercially-available spacecraft-type heat pipesAs part of an effort to develop reliable, cost effective spacecraft thermal control heat pipes, life tests on 30 commercially available heat pipes in 10 groups of different design and material combinations were conducted. Results for seven groups were reported herein. Materials are aluminum and stainless steel, and working fluids are methanol and ammonia. The formation of noncondensible gas was observed for times exceeding 11,000 hours. The heat transport capacities of the pipes were also determined.
Document ID
19780012516
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaufman, W. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Tower, L. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-78826
Report Number: NASA-TM-78826
Meeting Information
Meeting: Intern. Heat Pipes Conf.
Location: Palo Alto, CA
Country: United States
Start Date: May 22, 1978
End Date: May 24, 1978
Sponsors: AIAA
Accession Number
78N20459
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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