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Bipolar nickel-hydrogen battery designThe initial design for the NASA-Lewis advanced nickel-hydrogen battery is discussed. Fabrication of two 10-cell boilerplate battery stacks will soon begin. The test batteries will undergo characterization testing and low Earth orbit life cycling. The design effectively deals with waste heat generated in the cell stack. Stack temperatures and temperature gradients are maintained to acceptable limits by utilizing the bipolar conduction plate as a heat path to the active cooling fluid panel external to the edge of the cell stack. The thermal design and mechanical design of the battery stack together maintain a materials balance within the cell. An electrolyte seal on each cell frame prohibits electrolyte bridging. An oxygen recombination site and electrolyte reservoir/separator design does not allow oxygen to leave the cell in which it was generated.
Document ID
19850023087
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Koehler, C. W.
(Ford Aerospace and Communications Corp. Palo Alto, CA, United States)
Applewhite, A. Z.
(Ford Aerospace and Communications Corp. Palo Alto, CA, United States)
Kuo, Y.
(Ford Aerospace and Communications Corp. Palo Alto, CA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1985
Publication Information
Publication: NASA. Goddard Space Flight Center The 1984 Goddard Space Flight Center Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
85N31400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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