A frictionless satellite constraint system is provided. The constraint system includes at least one clamp bar configured to restrain a satellite within the constraint system in an axial direction. The constraint system also includes a plurality of pins configured to restrain the satellite within the constraint system in a lateral direction.


    Access

    Download


    Export, share and cite



    Title :

    System and apparatus for deploying a satellite


    Contributors:

    Publication date :

    2016-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    System and Apparatus for Deploying a Satellite

    Santos, Luis H. / Hudeck, John D. | NTRS | 2016


    STRUCTURE DEPLOYING SYSTEM AND SATELLITE COMPRISING THE SAME

    European Patent Office | 2021

    Free access

    METHOD FOR DEPLOYING A SATELLITE CONSTELLATION

    MARCHANDISE FRÉDÉRIC / SIMONTACCHI PAMELA / MATHIEU PERRINE | European Patent Office | 2017

    Free access

    Deploying Connexion by BoeingSM Satellite Services

    Laase, Ed / Richards, William | AIAA | 2003


    STRUCTURE DEPLOYING SYSTEM AND SATELLITE COMPRISING THE SAME

    SHIN JAE SUNG / KIM DAE YEOUG / LEE JONG WON et al. | European Patent Office | 2021

    Free access