NASA NTRS · 19790013411
Multimission modular spacecraft parallel battery tests
Abstract
An engineering evaluation of the Multimission Modular Spacecraft power supply is presented. The spacecraft has one charger with eight commandable voltage versus temperature levels. Graphs are presented which represent: (1) cell voltage limits vs. temperature; (2) charge ratio vs. temperature; (3) effect of 0.0 percent impedance unbalance at 10 C; (4) shorted cell at 10 C; and (5) discharge voltage profile at 10 C.
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Palandati, C.. 1977-01-01. Multimission modular spacecraft parallel battery tests. https://ntrs.nasa.gov/citations/19790013411
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