Abstract
A timing condition for consecutive collision orbits in the planar, circular three-body problem has been extended to the elliptic restricted problem for μ=0. The expression developed relates eccentric anomalies at the time of collision. Some families of solutions are presented.
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Howell, K.C. Consecutive collision orbits in the limiting case μ=0 of the elliptic restricted problem. Celestial Mechanics 40, 393–407 (1987). https://doi.org/10.1007/BF01235854
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DOI: https://doi.org/10.1007/BF01235854