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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
Goddard Space Flight Center
Document Type
Conference Paper
Authors
D A Baer (Goddard Space Flight Center Greenbelt, United States)
W J Schedler (Ford Aerospace (United States) Dearborn, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: The 1977 Goddard Space Flight Center Battery Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Energy Production and Conversion
Report/Patent Number
NASA-CP-2041
Meeting Information
Meeting: 10th Annual Battery Workshop
Location: Greenbelt, MD
Country: US
Start Date: November 15, 1977
End Date: November 17, 1977
Sponsors: Goddard Space Flight Center
Accession Number
79N21571
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle19790013394Collected WorksThe 1977 Goddard Space Flight Center Battery Workshop
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