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Part of the book series: NATO ASI Series ((ASIC,volume 154))

Abstract

Some recent tests have given excellent results in the analysis of three-body systems with three equal masses. These analyses are here extended to systems of unequal masses and lead to the following.

  1. A)

    For all mass ratios the smallest mass is the most unstable and the most subject to be ejected. The largest mass is generally very stable.

  2. B)

    The bounded orbits are very rare, their region in phase space is very small, much smaller than was generally expected.

  3. C)

    The usual Lagrange and Euler three-body solutions are not only some simple solutions of the three-body problem, they have also, under many respects, a role of limit and bifurcation with respect to the other solutions.

  4. D)

    The latest tests of escape approach very near to the true limit of bounded orbits.

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References

  • Laskar, J. and Marchai, C: 1984, Celestial Mechanics 32, pp. 15–28.

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© 1985 D. Reidel Publishing Company

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Marchal, C. (1985). Three-Body Problem Some Applications of the Tests of Escape. In: Szebehely, V.G. (eds) Stability of the Solar System and Its Minor Natural and Artificial Bodies. NATO ASI Series, vol 154. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-5398-7_9

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  • DOI: https://doi.org/10.1007/978-94-009-5398-7_9

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-8883-1

  • Online ISBN: 978-94-009-5398-7

  • eBook Packages: Springer Book Archive

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