The invention relates to an ejection unit for at least one satellite, in particular a picosatellite, comprising a frame that defines an inner space for receiving the satellite; and a retention device for holding the satellite in the inner space, the retention device being configured such that the satellite is releasable from the retention device.


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    Titel :

    Ejection unit for a satellite


    Beteiligte:
    BOGDANOV DIMITRIY (Autor:in) / SCHWARZ PETER (Autor:in) / GRUBER JOHANNES (Autor:in) / WIMMER PETER (Autor:in) / KRYUKOVSKIY VSEVOLOD (Autor:in)

    Erscheinungsdatum :

    2020-02-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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