A space-debris capturing device (3) includes a harpoon (31, 41, 41') driven into target debris (X) as space debris to be removed. The harpoon (31, 41, 41') includes a first harpoon part (43) having a large diameter, and a second harpoon part (44) having a diameter smaller than the diameter of the first harpoon part (43) and protruding from a leading surface (43a) in the direction of the drive of the first harpoon part (43) into the target debris (X).


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    Titel :

    УСТРОЙСТВО ЗАХВАТА КОСМИЧЕСКОГО МУСОРА И УСТРОЙСТВО УДАЛЕНИЯ КОСМИЧЕСКОГО МУСОРА


    Erscheinungsdatum :

    20.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS