Acceptance test data included: voltage profiles; pressure increase or decrease; and response of the third electrode cell. A softening of the voltage profile was revealed, as well as a lowering of the discharge profile and a 10 percent loss of capacity over a 0 to 20 C temperature range.
Multimission modular spacecraft parallel battery tests
1981-03-01
Miscellaneous
No indication
English
Multimission modular spacecraft parallel battery tests
NTRS | 1977
|Multimission modular spacecraft (MMS)
AIAA | 1988
|Testing programs for the Multimission Modular Spacecraft
NTRS | 1978
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