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Development of Passive Fuel Cell Thermal Management TechnologyThe NASA Glenn Research Center is developing advanced passive thermal management technology to reduce the mass and improve the reliability of space fuel cell systems for the NASA exploration program. The passive thermal management system relies on heat conduction within the cooling plate to move the heat from the central portion of the cell stack out to the edges of the fuel cell stack rather than using a pumped loop cooling system to convectively remove the heat. Using the passive approach eliminates the need for a coolant pump and other cooling loop components which reduces fuel cell system mass and improves overall system reliability. Previous analysis had identified that low density, ultra-high thermal conductivity materials would be needed for the cooling plates in order to achieve the desired reductions in mass and the highly uniform thermal heat sink for each cell within a fuel cell stack. A pyrolytic graphite material was identified and fabricated into a thin plate using different methods. Also a development project with Thermacore, Inc. resulted in a planar heat pipe. Thermal conductivity tests were done using these materials. The results indicated that lightweight passive fuel cell cooling is feasible.
Document ID
20110002805
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Burke, Kenneth A.
(NASA Glenn Research Center Cleveland, OH, United States)
Jakupca, Ian
(Analex Corp. Brook Park, OH, United States)
Colozza, Anthony
(Analex Corp. Brook Park, OH, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2011
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-17399
NASA/TM-2010-216773
Report Number: E-17399
Report Number: NASA/TM-2010-216773
Meeting Information
Meeting: Seventh International Energy Conversion Engineering Conference (IECEC)
Location: Denver, CO
Country: United States
Start Date: August 2, 2009
End Date: August 5, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 038957.04.06.02.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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