Applications Technology Satellites Battery and Power System Design

F E Ford; B Bemis

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NASA NTRS · 19790013401

Applications Technology Satellites Battery and Power System Design

F E Ford·B Bemis

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Abstract

A summary of the ATS battery design which is onboard the Applications Technology Satellite (ATS) is provided. The 15 ampere hour nickel cadmium cells were manufactured by Gulton, 19 series connected cells per battery, and there are two batteries in each spacecraft. The operating design life was two years in a synchronous orbit, and a maximum depth of discharge of 50 percent. The design temperature for the batteries in the spacecraft was 0 to 25 C, and the charge control consisted of 1 volt versus temperature on a constant percentage voltage. Also, C/10 current limit, and a commandable trickle charge rate, using C/20 or C/60. The undervoltage was sent across a 9 cell and a 10 cell group, and it was set at one volt average per group on either group.

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F E Ford, B Bemis. 1978-01-01. Applications Technology Satellites Battery and Power System Design. https://ntrs.nasa.gov/citations/19790013401

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