The present invention relates to a nano-satellite bus, characterized in that it comprises: -a mono-bloc mechanical frame (1) comprising a plurality of posts and edges (2, 2') forming the sides of the said mechanical frame; -a back panel (10) for the connection of electronic components; -at least a connector (23) with spring contacts (24), said connector (23) being connected to the back panel (10) and fixed to the mono-bloc mechanical frame (1), said spring contacts (24) being mounted as a through-hole component through one post (2) of the mono-bloc mechanical frame (1) for the connection of satellite faces. The present invention further relates to a nano-satellite comprising a nano-satellite bus comprising these.


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    Title :

    CUBESAT BUS ARCHITECTURE


    Additional title:

    CUBESAT-BUSARCHITEKTUR
    ARCHITECTURE DE BUS CUBESAT


    Contributors:

    Publication date :

    2020-04-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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