Spacecraft rendezvous trajectory between two elliptical orbits is determined by optimization of the two impulse orbital transfer


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    Title :

    OPTIMUM TWO-IMPULSE ORBITAL TRANSFER AND RENDEZVOUS BETWEEN INCLINED ELLIPTICAL ORBITS


    Contributors:

    Publication date :

    1963-08-21


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English