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Heat dissipation of high rate Li-SOCl sub 2 primary cellsThe heat dissipation problem occurring in the lithium thionyl chloride cells discharged at relatively high rates under normal discharge conditions is examined. Four heat flow paths were identified, and the thermal resistances of the relating cell components along each flow path were accordingly calculated. From the thermal resistance network analysis, it was demonstrated that about 90 percent of the total heat produced within the cell should be dissipated along the radial direction in a spirally wound cell. In addition, the threshold value of the heat generation rate at which cell internal temperature could be maintained below 100 C, was calculated from total thermal resistance and found to be 2.9 W. However, these calculations were made only at the cell components' level, and the transient nature of the heat accumulation and dissipation was not considered. A simple transient model based on the lumped-heat-capacity concept was developed to predict the time-dependent cell temperature at different discharge rates. The overall objective was to examine the influence of cell design variable from the heat removal point of view under normal discharge conditions and to make recommendations to build more efficient lithium cells.
Document ID
19870001647
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cho, Y. I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Halpert, G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Deligiannis, E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 13, 2013
Publication Date
September 1, 1986
Publication Information
Publication: NASA. Goddard Space Flight Center The 1985 Goddard Space Flight Center Battery Workshop (date)
Subject Category
Electronics And Electrical Engineering
Accession Number
87N11080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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