The targeting techniques are developed which are required to determine the guidance reference release time of the space shuttle navigation system, the orbital insertion targeting values, and a time line of orbital maneuvers. An extension is made for rendezvous with a target satellite in an elliptical orbit.


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    Title :

    Space shuttle earth orbital rendezvous targeting techniques for near circular target satellite orbits


    Contributors:

    Publication date :

    1972-06-27


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :