Determination of collision trajectories passing through centers of celestial target bodies, is regarded as one of basic problems of Astroballistics; by applying transformation due to T.LEVI-CIVITA, it is possible to regularize collision trajectories, and to obtain conditions which position and velocity of missile must satisfy so that trajectory of missile passes through center of body; practical applicability tested on case of circumlunar trajectories.


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    Title :

    Collision trajectories in three-body problem


    Additional title:

    J Astronautical Sciences


    Contributors:


    Publication date :

    1959


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :