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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Collision trajectories in three-body problem


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    Benedikt, E.T. (Autor:in)


    Erscheinungsdatum :

    1959


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :