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Development of Passive Fuel Cell Thermal Management Heat ExchangerThe 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 highly thermally conductive cooling plates to move the heat from the central portion of the cell stack out to the edges of the fuel cell stack. Using the passive approach eliminates the need for a coolant pump and other cooling loop components within the fuel cell system which reduces mass and improves overall system reliability. Previous development demonstrated the performance of suitable highly thermally conductive cooling plates that could conduct the heat, provide a sufficiently uniform temperature heat sink for each cell of the fuel cell stack, and be substantially lighter than the conventional thermal management approach. Tests were run with different materials to evaluate the design approach to a heat exchanger that could interface with the edges of the passive cooling plates. Measurements were made during fuel cell operation to determine the temperature of individual cooling plates and also to determine the temperature uniformity from one cooling plate to another.
Document ID
20110002807
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Burke, Kenneth A.
(NASA Glenn Research Center Cleveland, OH, United States)
Jakupca, Ian J.
(Analex Corp. Cleveland, OH, United States)
Colozza, Anthony J.
(Analex Corp. Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
NASA/TM-2010-216892
E-17471
Report Number: NASA/TM-2010-216892
Report Number: E-17471
Funding Number(s)
WBS: WBS 038957.04.06.02.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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