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The 2.5 inch nickel-hydrogen developmentThe topics covered are presented in viewgraph form and include the following: reasons for developing a 2.5 in. nickel-hydrogen cell; the 2.5 in. nickel-hydrogen development history; RNHC-6-1 cell design; RNHC-6-1 charge voltage at 0.6 A; RNHC-6-1 discharge voltage at 3.0 A; RNHC-6-1 qualification testing; flight unit testing; RNHC-6-1 technical data; technical data for the SAR-10027 Battery; and RNHC-10-1 life test.
Document ID
19930011323
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cook, William D. (Eagle-Picher Industries, Inc. Joplin, MO, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Marshall Space Flight Center, The 1992 NASA Aerospace Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
93N20512
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930011301Collected WorksThe 1992 NASA Aerospace Battery Workshop
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