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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    Title :

    Satellite electric propulsion power supply unit and system for managing the electric propulsion of a satellite


    Contributors:

    Publication date :

    2018-12-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen



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