Abstract This paper presents the design and characterization of a miniature docking mechanism for nanosatellites. Potential applications are several, including servicing of orbital vehicles (e.g. refuelling, components replacement, deorbiting or reboosting) and assembly of large structures (e.g. telescopes, antennas). The mechanism responds to the constant demand of enabling technologies from the booming small satellites market. The developed system has a traditional probe–drogue configuration; it is equipped with a sensor to detect contact and a single servo-actuator to lock the connection. The simple, though effective, design fills a relevant gap in the field of nanosatellite technologies. Numerical simulations have been conducted to evaluate the dynamics of docking procedures and to estimate loads exchanged at contact. Experimental results validate the simulations and prove the high tolerance to angular and linear (lateral) misalignment.

    Highlights Miniature docking mechanism based on probe–drogue configuration. Compatibility with the CubeSat standard and extreme simplicity. Possibility to equip prepared, passive orbital objects. Numerical simulations of docking dynamics. Extensive laboratory validation of full docking procedure.


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    Titel :

    Miniature docking mechanism for CubeSats


    Beteiligte:

    Erschienen in:

    Acta Astronautica ; 176 ; 510-519


    Erscheinungsdatum :

    2020-06-25


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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