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In Flight Performance of a Six Ampere-hour Nickel-cadmium Battery in Low Earth OrbitFlight data for 17,000 orbital cycles are reviewed and summarized. The nickel cadmium battery system operated without failure or abnormality. Battery trend analysis used in determining the feasibility of extending mission life is discussed. The life test data for 20% depth of discharge indicates design life requirements would be reached even at a deeper depth of discharge.
Document ID
19840025619
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcdermott, J. K.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1984
Publication Information
Publication: NASA. Goddard Space Flight Center The 1983 Goddard Space Flight Center Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
84N33690
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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