EMU battery/SMM power tool characterization study

Palandati, C.

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NASA NTRS · 19830013083

EMU battery/SMM power tool characterization study

Palandati, C.

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Abstract

The power tool which will be used to replace the attitude control system in the SMM spacecraft was modified to operate from a self contained battery. The extravehicular mobility unit (EMU) battery was tested for the power tool application. The results are that 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.. 1982-01-12. EMU battery/SMM power tool characterization study. https://ntrs.nasa.gov/citations/19830013083

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