Disclosed is artificial satellite including: a mounting structure supporting equipment-bearing walls; a launcher-adapter rigidly connected to the mounting structure; a first radiator; and at least one first system for transporting heat by a fluid, including at least one duct having a first heat-exchange section and a second heat-exchange section, the second heat-exchange section being capable of being in thermal contact with the first radiator. The first heat-exchange section is in thermal contact with at least one portion of the launcher-adapter. Also disclosed is a method for filling a tank of propellant gas of the artificial satellite.


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    Titel :

    ARTIFICIAL SATELLITE AND METHOD FOR FILLING A TANK OF PROPELLENT GAS OF SAID ARTIFICIAL SATELLITE


    Beteiligte:

    Erscheinungsdatum :

    2017-12-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Artificial satellite and method for filling a tank of propellent gas of said artificial satellite

    WALKER ANDREW NICHOLAS | Europäisches Patentamt | 2018

    Freier Zugriff

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    Choice of propellent for cold gas propulsion system for satellite

    Briscoe, H.M. | Engineering Index Backfile | 1965