A propulsion system for the orbit control of a satellite in Earth orbit driven at a rate of displacement along an axis V tangential to the orbit comprises two propulsion modules, fixed to the satellite, and facing one another relative to the plane of the orbit, each of the propulsion modules comprising, in succession: a motorized rotation link about an axis parallel to the axis V; an offset arm; and a plate supporting two thrusters, suitable for delivering a thrust on an axis, arranged on the plate on either side of a plane P at right angles to the axis V passing through a center of mass of the satellite; each of the two thrusters being oriented in such a way that the thrust axes of the two thrusters are parallel to one another and at right angles to the axis V.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Système de propulsion en deux modules pour contrôle d'orbite et contrôle d'attitude de satellite


    Weitere Titelangaben:

    Bi-modular propulsion system for orbit and attitude control of a satellite
    Bimodulares Antriebssystem für Orbit- und Fluglageregelung eines Satelliten


    Beteiligte:
    CELERIER BRUNO (Autor:in)

    Erscheinungsdatum :

    17.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Système de propulsion pour contrôle d'orbite et contrôle d'attitude de satellite

    CELERIER BRUNO | Europäisches Patentamt | 2019

    Freier Zugriff




    Système de propulsion pour contrôle d'orbite et contrôle d'attitude de satellite

    CELERIER BRUNO | Europäisches Patentamt | 2021

    Freier Zugriff