A primary structure (100) for a spacecraft (200) including an interface ring (10) and a predetermined number of panels defining a box arranged to close an interior volume of the spacecraft. The box is connected to the interface ring. Side panels of the box are parallel to a geometric axis (A) of the interface ring, the interface ring is temporarily fastened to a system supporting the spacecraft in a launcher. Each panel is a one-piece panel formed by machining a metal material. The side panels at the base of the box are connected to the interface ring (10) via damping inserts (60).


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    Titel :

    DAMPED MACHINED PRIMARY STRUCTURE FOR A SPACECRAFT, SATELLITE INCORPORATING THIS PRIMARY STRUCTURE AND METHOD FOR MANUFACTURING SUCH A SATELLITE


    Beteiligte:
    GACOIN FLORIAN (Autor:in) / PIERINET JEAN-MARC (Autor:in) / JOYA MIREYA (Autor:in) / PRADAL JULIEN (Autor:in) / LOPEZ-SANCHEZ SARA (Autor:in) / FABRE NICOLAS (Autor:in)

    Erscheinungsdatum :

    02.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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