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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 922 K (1200 F). 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
19820048363
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Basiulis, A.
(Hughes Aircraft Co. Torrance, CA, United States)
Camarda, C. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-0903
Meeting Information
Meeting: Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference
Location: St. Louis, MO
Start Date: June 7, 1982
End Date: June 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers
Accession Number
82A31898
Distribution Limits
Public
Copyright
Other

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