A separation device for a deployable structure is configured to use the pogo-pin to supply power for severing a restraining wire. The separation device may enable the deployable structure to be elastically separated by means of an elastic force exerted thereon by a spring and may enable a deployed state of the structure to be ascertained immediately after deployment.


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    Titel :

    Separation device using pogo-pin for deployable structure of CubeSat


    Beteiligte:
    OH HYUN UNG (Autor:in) / KIM SU HYEON (Autor:in) / PARK TAE YONG (Autor:in) / SAKONG YOUNG BO (Autor:in) / KIM HONGRAE (Autor:in)

    Erscheinungsdatum :

    14.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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