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Design, fabrication and test of a hydrogen heat pipeRe-entrant groove technology was extended to hydrogen heat pipes. Parametric analyses are presented which optimize the theoretical design while considering the limitations of state-of-the-art extrusion technology. The 6063-T6 aluminum extrusion is 14.6 mm OD with a wall thickness of 1.66 mm and contains 20 axial grooves which surround a central 9.3 mm diameter vapor core. Each axial groove is 0.775 mm diameter with a 0.33 mm opening. An excess vapor reservoir is provided at the evaporator to minimize the pressure containment hazard during ambient storage. Modifications to the basic re-entrant groove profile resulted in improved overall performance. While the maximum heat transport capacity decreased slightly to 103 w-m the static wicking height increased markedly to 4.5 cm. The heat pipe became operational between 20 and 30 K after a cooldown from 77 K without any difficulty. Steady state performance data taken over a 19 to 23 K temperature range indicated: (1) maximum heat transport capacity of 5.4 w-m; (2) static wicking height of 1.42 cm; and (3) overall heat pipe conductance of 1.7 watts/deg C.
Document ID
19790016127
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Alario, J.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1979
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-152267
Report Number: NASA-CR-152267
Accession Number
79N24298
Funding Number(s)
CONTRACT_GRANT: NAS2-9291
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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