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Satellites from Infinity

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Introductory Orbit Dynamics

Abstract

Consider a spacecraft that has left the Earth and is flying to Jupiter. Consider it launched such that it is going to encounter Mars on its way. Precautions are taken, of course, to make sure that it does not collide with Mars. On the other hand, it is to approach Mars closely, so close as a matter of fact, that it will be under the influence of Mars for a certain period of time.

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Suggested Reading

  1. Tisserand, F. Traite de mécanique celeste, Gauthier-Villars, Paris, 1889, Vol. I, 474 pp.;

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  2. Tisserand, F. Traite de mécanique celeste, Gauthier-Villars, Paris, 1889, Vol. II, 552 pp.;

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  3. Tisserand, F. Traite de mécanique celeste, Gauthier-Villars, Paris, 1889, Vol. III, 427 pp.;

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  4. Tisserand, F. Traite de mécanique celeste, Gauthier-Villars, Paris, 1889, Vol. IV, 548 pp.

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© 1989 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig

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Rimrott, F.P.J. (1989). Satellites from Infinity. In: Introductory Orbit Dynamics. Fundamentals and Advances in the Engineering Sciences / Grundlagen und Fortschritte der Ingenieurwissenschaften. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-90338-9_10

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  • DOI: https://doi.org/10.1007/978-3-322-90338-9_10

  • Publisher Name: Vieweg+Teubner Verlag

  • Print ISBN: 978-3-322-90339-6

  • Online ISBN: 978-3-322-90338-9

  • eBook Packages: Springer Book Archive

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