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How is redundancy of power supply from converters done in satellites? can anyone explain with complete details.Is it possible to get the actual design from power system of any mini-satellites ? Is the redundancy of converters actually done?

i want to know how redundancy is maintained for the converter in a satellite.it's the most crucial part as the failure of a converter is highly possible and how is this problem tackled? by saying converter i mean dc/dc converter

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