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Time-to-failure analysis for NiCd batteries in a CPS orbitCells operating at five degrees Celsius or less, and going to 60 to 65 percent depth of discharge, were studied as to whether they could achieve a useful working life of 7.5 years in a GPS orbit. The characteristics of various orbits were compared and it is noted that the GPS orbit experiences only 220 cycles a year and must be treated as a geosynchronous rather than a low Earth orbit. Cell degradation is considered to be the result of both trickle-charge degradation and degradation due to cycling. Time-to-failure values are presented for selected temperatures and depth of discharges.
Document ID
19820012546
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sense, K. A.
(Rockwell International Corp. Seal Beach, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Goddard Space Flight Center The 1981 GSFC Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
82N20420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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