Consecutive collision orbits in the limiting case MU = 0 of the elliptic restricted problem

Details Consecutive collision orbits in the limiting case MU = 0 of the elliptic restricted problem Consecutive collision orbits in the limiting case MU = 0 of the elliptic restricted problem

Sep 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987cemec..40..393h&link_type=abstract

Celestial Mechanics (ISSN 0008-8714), vol. 40, no. 3-4, 1987, p. 393-407.

Physics

1

Collision Rates, Consecutive Events, Elliptical Orbits, Orbit Calculation, Three Body Problem, Eccentric Orbits, Hyperbolic Functions

Scientific paper

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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