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EMU Battery/module Service Tool Characterization StudyThe power tool which will be used to replace the attitude control system in the SMM spacecraft is being modified to operate from a self contained battery. The extravehicular mobility unit (EMU) battery, a silver zinc battery, was tested for the power tool application. The results obtained during show the EMU battery is capable of operating the power tool within the pulse current range of 2.0 to 15.0 amperes and battery temperature range of -10 to 40 degrees Celsius.
Document ID
19840025625
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palandati, C. F. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1984
Publication Information
Publication: The 1983 Goddard Space Flight Center Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
84N33696
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840025597Collected WorksThe 1983 Goddard Space Flight Center Battery Workshop
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