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The LiAl/FeS2 battery power source for the futureAdvanced high power density rechargeable batteries are currently under development. These batteries have the potential of greatly increasing the power and energy densities available for space applications. Depending on whether the system is optimized for high power or high energy, values up to 150 Wh/kg and 2100 W/kg (including hardware) are projected. This is due to the fact that the system uses a high conductivity molten salt electrolyte. The electrolyte also serves as a separator layer with unlimited freeze thaw capabilities. Life of 1000 cycles and ten calendar years is projected. The electrochemistry consists of a lithium aluminum alloy negative electrode, iron disulfide positive electrode, and magnesium oxide powder immobilized molten salt electrolyte. Processed powders are cold compacted into circular discs which are assembled into bipolar cell hardware with peripheral ceramic salts. The culmination of the work will be a high energy battery of 40 kWh and a high power battery of 28 kWh.
Document ID
19920013520
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Briscoe, J. Douglass
(SAFT America, Inc. Cockeysville, MD, United States)
Embrey, J.
(SAFT America, Inc. Cockeysville, MD, United States)
Oweis, S.
(SAFT America, Inc. Cockeysville, MD, United States)
Press, K.
(SAFT America, Inc. Cockeysville, MD, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Publication Information
Publication: NASA. Marshall Space Flight Center, The 1991 NASA Aerospace Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
92N22763
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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