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Advanced spacecraft fuel cell systems.The specific goals of the system selected for development are 10,000 hours of operation with refurbishment, 20 lb/kW at a sustained power of 7 kW, and 21 kW peaking capability for durations of two hours. The system is designed to operate on low pressure, propulsion grade hydrogen and oxygen. Product water is removed by a passive water removal method that employs a porous hydrophobic membrane as a part of the water transport plate. Aspects of system component testing are discussed together with advanced materials to be used. It was found that the initial performance of a cell with a gold catalyzed cathode is superior to a cell with platinum catalyst. The problem of a certain inability to maintain the desired gas-electrolyte-catalyst interface is the main source of difficulty with the gold-based catalysts.
Document ID
19720053977
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thaller, L. H.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Subject Category
Auxiliary Systems
Meeting Information
Meeting: U.S. Army, Power Sources Symposium
Location: Atlantic City, NJ
Start Date: May 23, 1972
End Date: May 25, 1972
Sponsors: U.S. Army
Accession Number
72A37643
Distribution Limits
Public
Copyright
Other

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