Abstract
In this paper, a new approach to planetary mission design is described which automates the search for gravity-assist trajectories. This method finds all conic solutions given a range of launch dates, a range of launch energies and a set of target planets. The new design tool is applied to the problems of finding multiple encounter trajectories to the outer planets and Venus gravity-assist trajectories to Mars. The last four-planet grand tour opportunity (until the year 2153) is identified. It requires an Earth launch in 1996 and encounters Jupiter, Uranus, Neptune, and Pluto. Venus gravity-assist trajectories to Mars for the 30 year period 1995–2024 are examined. It is shown that in many cases these trajectories require less launch energy to reach Mars than direct ballistic trajectories.
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Assistant Professor, School of Aeronautics and Astronautics
Graduate Student, School of Aeronautics and Astronautics
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Longuski, J.M., Williams, S.N. Automated design of gravity-assist trajectories to Mars and the outer planets. Celestial Mech Dyn Astr 52, 207–220 (1991). https://doi.org/10.1007/BF00048484
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DOI: https://doi.org/10.1007/BF00048484