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SMM parallel battery operation in orbitA parallel battery system for the SMM spacecraft is described. The battery system performance as a function of lifetime over orbit was evaluated. The following equipment performance specifications were examined during a typical orbit: battery current and discharges, voltage limitations, battery temperature variations, and current sensor performance. Tabulated battery performance data is also included.
Document ID
19820012552
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Broderick, R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: The 1981 GSFC Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
82N20426
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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