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Serial Charging Test on High Capacity Li-Ion Cells for the Orbiter Advanced Hydraulic Power SystemAlthough it looks like module level voltage drives the cutoff for charge, the actual cutoff is due to unbalanced cell voltages that drive the module voltage up. Individual cell voltage drives the cutoff for discharge Low resistance cells are the first to reach the low-voltage cutoff Cell-to-Cell voltage differences are generally small and show similar trends for each cycle Increase for a distinct window during charge and at the end of discharge Increase in max to min cell voltage difference with time/cycles Decrease in max to min cell voltage difference during high current pulses with time/cycles Individual cell voltage trends (with respect to other cells) are very repeatable from cycle to cycle, although voltage slowly degrades with time/cycles (resistance growth) Much more difference observed near end of discharge Little change in order of cell voltage (cell with highest voltage to cell with lowest voltage) Temp sensor on the side of cell (between 2 cells) shows much greater rise during discharge than for single cell tests (18 C vs 5 C) Conclusion: Serial Charging of this string of cells is feasible as it has only a minor impact on useful capacity
Document ID
20080015797
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Jeevarajan, Judith A.
(NASA Johnson Space Center Houston, TX, United States)
Irlbeck, Brad
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
August 1, 2006
Publication Information
Publication: The 2004 NASA Aerospace Battery Workshop
Subject Category
Space Sciences (General)
Distribution Limits
Public
Copyright
Public Use Permitted.
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