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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of spacecraft and rockets 2002-01, Vol.39 (1), p.9-16
Hauptverfasser: Strange, Nathan J, Longuski, James M
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
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.
ISSN:0022-4650
1533-6794
DOI:10.2514/2.3800