The Gemini/Agena docking mechanisms utilize simple mechanical elements to provide a capability for initial engagement between two orbiting vehicles. The docking mechanisms then rigidize the attachment in a manner suitable for subsequent maneuver with the Agena propulsion system. Finally, the mechanisms provide a capability for disengaging and repeating the entire docking cycle. The mechanical elements used are found in daily terrestrial applications.


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    Title :

    Gemini/Agena Docking Mechanism


    Contributors:
    P H Meyer (author)

    Conference:

    1st Aerospace Mechanisms Symposium ; 1966 ; Santa Clara, CA, US



    Publication date :

    1966-05-19


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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