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An Overview of Long Duration Sodium Heat Pipe TestsHigh temperature heat pipes are being evaluated for use in energy conversion applications such as fuel cells, gas turbine re-combustors, and Stirling cycle heat sources; with the resurgence of space nuclear power, additional applications include reactor heat removal elements and radiator elements. Long operating life and reliable performance are critical requirements for these applications. Accordingly long-term materials compatibility is being evaluated through the use of high temperature life test heat pipes. Thermacore International, Inc., has carried out several sodium heat pipe life tests to establish long term operating reliability. Four sodium heat pipes have recently demonstrated favorable materials compatibility and heat transport characteristics at high operating temperatures in air over long time periods. A 3l6L stainless steel heat pipe with a sintered porous nickel wick structure and an integral brazed cartridge heater has successfully operated at 650 to 700 C for over 115,000 hours without signs of failure. A second 3l6L stainless steel heat pipe with a specially-designed Inconel 60 I rupture disk and a sintered nickel powder wick has demonstrated over 83,000 hours at 600 to 650 C with similar success. A representative one-tenth segment Stirling Space Power Converter heat pipe with an Inconel 718 envelope and a stainless steel screen wick has operated for over 41 ,000 hours at nearly 700 0c. A hybrid (i.e. gas-fired and solar) heat pipe with a Haynes 230 envelope and a sintered porous nickel wick structure was operated for about 20,000 hours at nearly 700 C without signs of degradation. These life test results collectively have demonstrated the potential for high temperature heat pipes to serve as reliable energy conversion system components for power applications that require long operating lifetime with high reliability, Detailed design specifications, operating hi story, and test results are described for each of these sodium heat pipes. Lessons learned and future life test plans are also discussed.
Document ID
20130013063
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Rosenfeld, John H.
(Thermacore International, Inc. Lancaster, PA, United States)
Ernst, Donald M.
(Thermacore International, Inc. Lancaster, PA, United States)
Lindemuth, James E.
(Thermacore International, Inc. Lancaster, PA, United States)
Sanzi, James L.
(Thermacore International, Inc. Lancaster, PA, United States)
Geng, Steven M.
(NASA Glenn Research Center Cleveland, OH, United States)
Zuo, Jon
(Advanced Cooling Technologies, Inc. Lancaster, PA, United States)
Date Acquired
August 27, 2013
Publication Date
March 1, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2004-212959
E-14407
Meeting Information
Meeting: Space Technology and Applications International Forum (STAIF-2004)
Location: Albuquerque, NM
Country: United States
Start Date: February 8, 2004
End Date: February 12, 2004
Sponsors: American Inst. of Physics
Funding Number(s)
WBS: WBS 972-20-01
CONTRACT_GRANT: NAS3-26925
CONTRACT_GRANT: ZA-2-11120-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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