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Cycle life test and failure model of nickel-hydrogen cells

Conference · · Proc., Intersoc. Energy Convers. Eng. Conf.; (United States)
OSTI ID:5490472
COMSAT and Air Force/Hughes design six ampere-hour individual pressure vessel nickel-hydrogen cells were charge/discharge cycled to failure. They were cycled on a low-earth-orbit cycle regime to a deep depth of discharge (80 percent of rated ampere-hour capacity). Two cells of each design were cycled. One COMSAT cell failed at cycle 1712 and the other failed at cycle 1875. For the Air Force/Hughes cells, one cell failed at cycle 2250 and the other failed at cycle 2638. All cells, of both designs, failed due to low end of discharge voltage. After cell failure, three different reconditioning tests (deep discharge, physical reorientation, and open circuit voltage stand) were conducted on all cells. A fourth reconditioning test (electrolyte addition) was conducted on one cell of each design. In addition, post-cycle cell teardown and failure analysis were performed on the one cell of each design which did not have electrolyte added after failure. These tests were conducted to evaluate failure modes. This paper presents the results of those evaluations.
Research Organization:
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio
OSTI ID:
5490472
Report Number(s):
CONF-830812-
Conference Information:
Journal Name: Proc., Intersoc. Energy Convers. Eng. Conf.; (United States) Journal Volume: 4
Country of Publication:
United States
Language:
English