A Docking Mechanism concept is described which is suitable for use with autonomous docking systems. The central feature of using simple cylindrical handles on one side and a type of prism seating on the other is offered as a practical method of achieving a standardized structural interface without freezing continued development of the latches, either technically or commercially. The main emphasis in docking mechanism concepts is in two directions: (1) a very simple docking mechanism, involving mainly the latch mechanism to achieve a structural link; and (2) a sophisticated Docking Mechanism, where the latch mechanism is designed for nonrigid spacecraft and the achievement of very low dynamic interactions between spacecraft during the docking process.


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    Title :

    A modular docking mechanism for in-orbit assembly and spacecraft servicing


    Contributors:
    Gampe, F. (author) / Priesett, K. (author) / Bentall, R. H. (author)


    Publication date :

    1985-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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