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Long titanium heat pipes for high-temperature space radiatorsTitanium heat pipes are being developed to provide light weight, reliable heat rejection devices as an alternate radiator design for the Space Reactor Power System (SP-100). The radiator design includes 360 heat pipes, each of which is 5.2 m long and dissipates 3 kW of power at 775 K. The radiator heat pipes use potassium as the working fluid, have two screen arteries for fluid return, a roughened surface distributive wicking system, and a D-shaped cross-section container configuration. A prototype titanium heat pipe, 5.5-m long, has been fabricated and tested in space-simulating conditions. Results from startup and isothermal operation tests are presented. These results are also compared to theoretical performance predictions that were used to design the heat pipe initially.
Document ID
19830045909
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Girrens, S. P.
(Los Alamos National Laboratory Los Alamos, NM, United States)
Ernst, D. M.
(Thermacore, Inc. Lancaster, PA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: IECEC ''82; Seventeenth Intersociety Energy Conversion Engineering Conference
Location: Los Angeles, CA
Start Date: August 8, 1982
End Date: August 12, 1982
Accession Number
83A27127
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-955935
Distribution Limits
Public
Copyright
Other

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