Triple approaches in the plane isosceles equal-mass three-body problem |
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Authors: | V. V. Orlov A. V. Petrova A. I. Martynova |
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Affiliation: | (1) Sobolev Astronomical Institute, St. Petersburg State University, Bibliotechnaya pl. 2, Petrodvorets, 198904, Russia;(2) St. Petersburg Academy of Forestry Engineering, Institutskii per. 5, St. Petersburg, 194021, Russia |
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Abstract: | We analyze flyby-type triple approaches in the plane isosceles equal-mass three-body problem and in its vicinity. At the initial time, the central body lies on a straight line between the other two bodies. Triple approaches are described by two parameters: virial coefficient k and parameter $mu = dot r/sqrt {dot r^2 + dot R^2 }$ , where $dot r$ is the relative velocity of the extreme bodies and $dot R$ is the velocity of the central body relative to the center of mass of the extreme bodies. The evolution of the triple system is traceable until the first turn or escape of the central body. The ejection length increases with closeness of the triple approach (parameter k). The longest ejections and escapes occur when the extreme bodies move apart with a low velocity at the time of triple approach. We determined the domain of escapes; it corresponds to close triple approaches (k>0.8) and to μ in the range ?0.2<μ<0.7. For small deviations from the isosceles problem, the evolution does not differ qualitatively from the isosceles case. The domain of escapes decreases with increasing deviations. In general, the ejection length increases for wide approaches and decreases for close approaches. |
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Keywords: | celestial mechanics |
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