A spacecraft for the distribution of electrical energy to client craft at points situated in free space, in orbit and/or on a celestial body includes a main structure equipped with an electric thruster, with a chemical thruster and with a solar generator, a first fuel container for fuel intended for the electric thruster, and a second fuel container for fuel intended for the chemical thruster. The spacecraft is able to be modulated such that the main structure can be coupled/decoupled alternatively to/from the first container or the second container, the first container and the second container are able to be coupled/decoupled to/from one another, and the solar generator can be deployed or retracted.


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    Title :

    ENGIN SPATIAL DE DISTRIBUTION ÉLECTRIQUE, ET PROCÉDÉ ASSOCIÉ


    Additional title:

    SPACECRAFT FOR ELECTRICITY DISTRIBUTION, AND ASSOCIATED METHOD
    RAUMFAHRZEUG ZUR STROMVERTEILUNG UND ZUGEHÖRIGES VERFAHREN


    Contributors:

    Publication date :

    2024-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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