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The O2 reduction at the IFC modified O2 fuel cell electrodeThe International Fuel Corporation (IFC) state of the art (SOA) O2 electrode (Au-10 percent Pt electrocatalyst by weight) is currently being used in the alkaline H2-O2 fuel cell in the NASA Space Shuttle. Recently, IFC modified O2 electrode, as a possible replacement for the SOA electrode. In the present study, O2 reduction data were obtained for the modified electrode at temperatures between 23.3 and 91.7 C. BET measurements gave an electrode BET surface area of about 2070 sq. cm/sq. cm of geometric surface area. The Tafel data could be fitted to two straight line regions. The slope for the lower region, designated as the 0.04 V/decade region, was temperature dependent, and the transfer coefficient was about 1.5. The 'apparent' energy of activation for this region was about 19 kcal/mol. An O2 reduction mechanism for this 0.04 region is presented. In the upper region, designated as the 0.08 V/decade region, diffusion may be the controlling process. Tafel data are presented to illustrate the increase in performance with increasing temperature.
Document ID
19920020424
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fielder, William L.
(NASA Lewis Research Center Cleveland, OH, United States)
Singer, Joseph
(NASA Lewis Research Center Cleveland, OH, United States)
Baldwin, Richard S.
(NASA Lewis Research Center Cleveland, OH, United States)
Johnson, Richard E.
(LeTourneau Coll. Longview, TX., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-7073
NASA-TM-105691
NAS 1.15:105691
Report Number: E-7073
Report Number: NASA-TM-105691
Report Number: NAS 1.15:105691
Accession Number
92N29667
Funding Number(s)
PROJECT: RTOP 506-41-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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