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Synchronous meteorological and geostationary operational environmental satellites battery and power system designThe battery was a three ampere hour nickel cadmium prismatic cell. The battery consists of 20 cells connected in series and there were two batteries per spacecraft. The battery operations (voltage and temperature) that the spacecraft sees during a normal operational day are discussed.
Document ID
19790013400
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baer, D. A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Schedler, W. J.
(Natl. Environ. Satellite Serv. Suitland, Md., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Publication Information
Publication: The 1977 Goddard Space Flight Center Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
79N21571
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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