A satellite electric propulsion power supply unit comprises: an internal source of electrical power; an external input adapted to receive an electrical power supply from an external source of electrical power; a first external output and a second external output adapted to deliver as output, respectively, a first electrical power supply and a second electrical power supply; a first selector element and a second selector element such that: the first selector element is equipped with a first internal input connected to the internal source and with two outputs: the first external output and an internal output connected to a second internal input of the second selector element; and the second selector element is equipped with an output corresponding to the second external output and with two inputs: the external input and the second internal input.


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    Titel :

    SATELLITE ELECTRIC PROPULSION POWER SUPPLY UNIT AND SYSTEM FOR MANAGING THE ELECTRIC PROPULSION OF A SATELLITE


    Beteiligte:
    GRUWE ALAIN (Autor:in) / LEDENT PHILIPPE (Autor:in)

    Erscheinungsdatum :

    13.10.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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