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Proton Exchange Membrane Fuel Cell Transient Load ResponseSpaceflight mission profiles may not be limited to constant power loads. It is necessary for the
associated power system to support changes in load in addition to being energy dense. H2-O2 proton exchange membrane (PEM) fuel cells can accommodate such requirements without significant current smoothing or additional devices to provide transient power. This testing involved current load step changes to characterize non-flow-through PEM fuel cell response to increasing and decreasing load step changes over a range of 0 to 0.5 A/sq. cm. It was determined that fuel cell output voltage stabilizes within 4 ms with no noticeable steady-state performance degradation, following exposure of the fuel cell to transient loads of up to ~1.5 A/sq. cm. Faster stabilization generally occurred following larger step changes.
Document ID
20210018094
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Phillip J. Smith
(Glenn Research Center Cleveland, Ohio, United States)
William R. Bennett
(Glenn Research Center Cleveland, Ohio, United States)
Ian J. Jakupca
(Glenn Research Center Cleveland, Ohio, United States)
Ryan P. Gilligan
(Glenn Research Center Cleveland, Ohio, United States)
Lawrence G. Edwards
(Vantage Partners, LLC. St Louis, Missouri, United States)
Date Acquired
June 30, 2021
Publication Date
December 1, 2021
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-19964
Funding Number(s)
WBS: 596118.04.59.22
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
fuel cell
hydrogen
oxygen
non-flow-through
proton exchange membrane
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