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.


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    Title :

    RECONFIGURABLE POWER PROCESSING UNIT FOR SPACECRAFT OPERATIONS


    Additional title:

    REKONFIGURIERBARE LEISTUNGSVERARBEITUNGSEINHEIT FÜR DEN BETRIEB VON RAUMFAHRZEUGEN
    UNITÉ DE TRAITEMENT D'ALIMENTATION RECONFIGURABLE POUR FONCTIONNEMENT D'ENGIN SPATIAL


    Contributors:

    Publication date :

    2022-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64G Raumfahrt , COSMONAUTICS



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