A reconfigurable power processing unit for a spacecraft including a plurality of power modules. Each of the power modules includes a first power source and a second power source. The first power source and the second power source are configured to be in series in a first state and in parallel in a second state. A plurality of contactors connect each power module to at least one of another power module in the plurality of power modules and a power processing output and are configured to control the state of the power modules.
RECONFIGURABLE POWER PROCESSING UNIT FOR SPACECRAFT OPERATIONS
REKONFIGURIERBARE LEISTUNGSVERARBEITUNGSEINHEIT FÜR DEN BETRIEB VON RAUMFAHRZEUGEN
UNITÉ DE TRAITEMENT D'ALIMENTATION RECONFIGURABLE POUR FONCTIONNEMENT D'ENGIN SPATIAL
2022-04-06
Patent
Electronic Resource
English
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