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Design, fabrication and test of liquid metal heat-pipe sandwich panelsIntegral heat-pipe sandwich panels, which synergistically combine the thermal efficiency of heat pipes and the structural efficiency of honeycomb sandwich panel construction, were fabricated and tested. The designs utilize two different wickable honeycomb cores, facesheets with screen mesh sintered to the internal surfaces, and potassium or sodium as the working fluid. Panels were tested by radiant heating, and the results indicate successful heat pipe operation at temperatures of approximately 922K (1200F). These panels, in addition to solving potential thermal stress problems in an Airframe-Integrated Scramjet Engine, have potential applications as cold plates for electronic component cooling, as radiators for space platforms, and as low distortion, large area structures.
Document ID
19830014270
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Basiulis, A.
(Hughes Aircraft Co. Torrance, Calif., United States)
Camarda, C. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:84631
NASA-TM-84631
Report Number: NAS 1.15:84631
Report Number: NASA-TM-84631
Meeting Information
Meeting: AIAA/ASME 3rd Joint Thermophys., Fluids, Plasma and Heat Transfer Conf.
Location: St. Louis
Start Date: June 7, 1982
End Date: June 11, 1982
Accession Number
83N22541
Funding Number(s)
PROJECT: RTOP 506-53-53-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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