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Update on Development of 360V, 28kWh Lithium-Ion BatteryEngineering unit submodule batteries (EUSB) the 360V, 28kWh EAPU battery were designed and assembled by COM DEV. These submodules consist of Sony Li-Ion 18650HC cells in a 5P-41S array yielding 180V, 1.4 kWh. Tests of these and of substrings and single cells at COM DEV and at JSC under various performance and abuse conditions demonstrated that performance requirements can be met. The thermal vacuum tests demonstrated that the worst case hot condition is the design driver. Deficiencies in the initial diode protection scheme of the battery were identified as a result of test failures. Potential solutions to the scheme are under development and will be presented.
Document ID
20060013093
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Davies, Francis
(NASA Johnson Space Center Houston, TX, United States)
Darcy, Eric
(NASA Johnson Space Center Houston, TX, United States)
Cowles, Phil
(COM DEV Ltd. Cambridge, Ontario, Canada)
Irlbeck, Brad
(NASA Johnson Space Center Houston, TX, United States)
Weintritt, John
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
September 1, 2005
Publication Information
Publication: The 2003 NASA Aerospace Battery Workshop
Subject Category
Energy Production And Conversion
Distribution Limits
Public
Copyright
Public Use Permitted.
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