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.


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    Titel :

    System and apparatus for deploying a satellite


    Beteiligte:
    SANTOS LUIS H (Autor:in) / HUDECK JOHN D (Autor:in)

    Erscheinungsdatum :

    2016-09-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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