EMU Battery/module Service Tool Characterization Study

Palandati, C. F.

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NASA NTRS · 19840025625

EMU Battery/module Service Tool Characterization Study

Palandati, C. F.

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Abstract

The power tool which will be used to replace the attitude control system in the SMM spacecraft is being modified to operate from a self contained battery. The extravehicular mobility unit (EMU) battery, a silver zinc battery, was tested for the power tool application. The results obtained during show the EMU battery is capable of operating the power tool within the pulse current range of 2.0 to 15.0 amperes and battery temperature range of -10 to 40 degrees Celsius.

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Palandati, C. F.. 1984-09-01. EMU Battery/module Service Tool Characterization Study. https://ntrs.nasa.gov/citations/19840025625

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