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Intermediate Temperature Fluids Life Tests - ExperimentsThere are a number of different applications that could use heat pipes or loop heat pipes (LHPs) in the intermediate temperature range of 450 to 725 K (170 to 450 C), including space nuclear power system radiators, fuel cells, and high temperature electronics cooling. Historically, water has been used in heat pipes at temperatures up to about 425 K (150 C). Recent life tests, updated below, demonstrate that titanium/water and Monel/water heat pipes can be used at temperatures up to 550 K (277 C), due to water's favorable transport properties. At temperatures above roughly 570 K (300 C), water is no longer a suitable fluid, due to high vapor pressure and low surface tension as the critical point is approached. At higher temperatures, another working fluid/envelope combination is required, either an organic or halide working fluid. An electromotive force method was used to predict the compatibility of halide working fluids with envelope materials. This procedure was used to reject aluminum and aluminum alloys as envelope materials, due to their high decomposition potential. Titanium and three corrosion resistant superalloys were chosen as envelope materials. Life tests were conducted with these envelopes and six different working fluids: AlBr3, GaCl3, SnCl4, TiCl4, TiBr4, and eutectic diphenyl/diphenyl oxide (Therminol VP-1/Dowtherm A). All of the life tests except for the GaCl3 are ongoing; the GaCl3 was incompatible. As the temperature approaches 725 K (450 C), cesium is a potential heat pipe working fluid. Life tests results are also presented for cesium/Monel 400 and cesium/70-30 copper/nickel heat pipes operating near 750 K (477 C). These materials are not suitable for long term operation, due to copper transport from the condenser to the evaporator.
Document ID
20070031908
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Anderson, William G.
(Advanced Cooling Technologies, Inc. Lancaster, PA, United States)
Bonner, Richard W.
(Advanced Cooling Technologies, Inc. Lancaster, PA, United States)
Dussinger, Peter M.
(Advanced Cooling Technologies, Inc. Lancaster, PA, United States)
Hartenstine, John R.
(Advanced Cooling Technologies, Inc. Lancaster, PA, United States)
Sarraf, David B.
(Advanced Cooling Technologies, Inc. Lancaster, PA, United States)
Locci, Ivan E.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
June 25, 2007
Subject Category
Metals And Metallic Materials
Report/Patent Number
E-16231
AIAA Paper 2007-4808
Report Number: E-16231
Report Number: AIAA Paper 2007-4808
Meeting Information
Meeting: International Energy Conversion Engineering Conference (IECEC-AIAA)
Location: Saint Louis, MO
Country: United States
Start Date: June 25, 2007
End Date: June 27, 2007
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 850661.04.01.03
CONTRACT_GRANT: NNC05TA36T
CONTRACT_GRANT: NNC06CA74C
CONTRACT_GRANT: N65538-05-M-0139
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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