The invention relates to a satellite structural concept with a mainly external load-carrying structure and its dedicated launcher interface, which allows an efficient exploitation of the launch vehicle mass capability and satellite internal volume. This concept according to the present invention can be used for any space mission/orbit/launcher if deemed convenient.

    L'invention concerne un concept structural de satellite comprenant une structure porteuse de charge principalement externe et son interface de lanceur dédiée, qui permet une exploitation efficace de la capacité de masse du véhicule de lancement et du volume interne du satellite. Ce concept selon la présente invention peut être utilisé pour tout(e) mission/orbite/lanceur spatial(e) s'il est jugé pratique.


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    Title :

    EFFICIENT SATELLITE STRUCTURE CONCEPT FOR SINGLE OR STACKING MULTIPLE LAUNCHES


    Additional title:

    CONCEPT DE STRUCTURE DE SATELLITE EFFICACE POUR LANCEUR UNIQUE OU POUR EMPILEMENT DE PLUSIEURS LANCEURS


    Contributors:

    Publication date :

    2019-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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