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.
Collision trajectories in three-body problem
J Astronautical Sciences
Journal of the Astronautical Sciences ; 6 , n 2
1959
Aufsatz (Zeitschrift)
Englisch
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