This paper will address the trajectory correction maneuvers (TCMs) which enabled the successful completion of the circuitous VEEGA trajectory while providing for the first ever encounters with main-belt asteroids.
(abstract) Maneuver Design for Galileo Asteroid Flybys
1994-05-22
Preprint
Keine Angabe
Englisch
Mission strategy for combined comet-asteroid flybys
AIAA | 1972
|Mission Strategy for Combined Comet-Asteroid Flybys
AIAA | 1974
|Mission strategy for combined comet-asteroid flybys.
NTRS | 1972
|Optimum Trajectory for Low-thrust Multiple Trojan Asteroid Flybys
British Library Conference Proceedings | 2004
|NTRS | 1981
|