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Performance of battery reconditioning on the communications technology satelliteSome real life data on the flight performance and reconditioning on the Communications Technology Satellite are presented. There are two 24-cell nominal 5 amp-hour nickel cadmium batteries on board. The two batteries are operated in parallel with isolating diodes in between and permanently connected to the housekeeping buses. The recharge can be at C over 10 or C over 20 to a 1.4 charge/discharge ratio; and recharge is terminated either when a computed 1.4 charge/discharge ratio is reached, or a charge voltage peak is reached.
Document ID
19790013415
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lackner, J.
(Defence Research Establishment Ottawa Ottawa Ontario, Canada)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA. Goddard Space Flight Center The 1977 Goddard Space Flight Center Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
79N21586
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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