A system (100) and method (300) for launching multiple satellites from a launch vehicle is provided. The system includes a mechanical structure (102) which has one or more mounting means (104A-F), a control unit (106) for controlling the one or more mounting means for positioning and separating the multiple satellites in the mechanical structure, an image capturing system for monitoring the positioning of each satellite in the mechanical structure. The mounting means are adapted to position the satellites in axial, inclined and radial separations at a distance to ensure that each satellite will not come in contact with each other in short duration as well as long duration of orbit evolution.

    Système (100) et procédé (300) pour lancer de multiples satellites à partir d'un véhicule de lancement. Le système comprend une structure mécanique (102) qui possède un ou plusieurs moyens de montage (104A-F), une unité de commande (106) pour commander le ou les moyens de montage pour positionner et séparer les multiples satellites dans la structure mécanique, un système de capture d'image pour surveiller le positionnement de chaque satellite dans la structure mécanique. Les moyens de montage sont conçus pour positionner les satellites dans des séparations axiales, inclinées et radiales à une distance pour s'assurer que chaque satellite ne va pas entrer en contact un autre en courte durée et longue durée d'évolution d'orbite.


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    Title :

    A SYSTEM AND METHOD FOR LAUNCHING MULTIPLE SATELLITES FROM A LAUNCH VEHICLE


    Additional title:

    SYSTÈME ET PROCÉDÉ DE LANCEMENT DE MULTIPLES SATELLITES À PARTIR D'UN VÉHICULE DE LANCEMENT


    Contributors:
    L SOWMIANARAYANAN (author) / R HUTTON (author) / B JAYAKUMAR (author) / AK ANILKUMAR (author) / DEEPAK NEGI (author) / K SIVAN (author)

    Publication date :

    2020-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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