Graphical Method for Gravity-Assist Trajectory Design
A new analytical technique directly related to Tisserand's criterion that permits the quick identification of all viable ballistic gravity-assist sequences to a given destination is introduced. The method is best presented by a simple graphical technique. The graphical technique readily demonst...
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Veröffentlicht in: | Journal of spacecraft and rockets 2002-01, Vol.39 (1), p.9-16 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | A new analytical technique directly related to Tisserand's criterion that permits the quick identification of all viable ballistic gravity-assist sequences to a given destination is introduced. The method is best presented by a simple graphical technique. The graphical technique readily demonstrates that gravity assists via Venus, Earth, and Jupiter are tremendously effective in sequences such as Venus-Earth-Earth-Jupiter and Venus-Earth-Mars-Earth. Estimates are made for the shortest flight times for a given launch energy to each planet. This graphical technique should provide mission designers with a potent tool for finding economical gravity-assist trajectories to many targets of high scientific interest in the solar system. |
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ISSN: | 0022-4650 1533-6794 |
DOI: | 10.2514/2.3800 |