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The 250AH/90A active lithium-thionyl chloride cell for Centaur-G applicationA high rate active Li/SOCl2 cell was designed for use in a 28 volt, 250 amp-hour space battery system. The lithium battery is being considered as a replacement of its heavier silver-zinc counterpart on board the Centaur-G booster rocket which is used to launch payloads from the Space Shuttle cargo bay into deep-space. Basically a feasibility study, this development effort is demonstrating the ability of the lithium cell to deliver up to 90 amps safely at power densities of approximately 25 watts per pound. Test data on 4 prototype units is showing an energy density of 85 watt-hours per pound and 9.0 watt-hours/cu in. The cells tested typically delivered 280 to 300 amp-hours under ambient temperature test conditions using alternating continuous loads of 90, 55, and 20 amperes throughout life. Data from four cells tested are presented to demonstrate the capability of Li/SOCl2 technology for a C/3 discharge rate in active and hermetic cell units.
Document ID
19880001641
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zolla, A. E.
(Altus Corp. San Jose, CA, United States)
Tura, D. D.
(Altus Corp. San Jose, CA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Publication Information
Publication: NASA Goddard Space Flight Center, Greenbelt, Md. The 1986 Goddard Space Flight Center Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
88N11023
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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