NASA NTRS · 20060039619
(abstract) Maneuver Design for Galileo Asteroid Flybys
Abstract
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.
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Wilson, Michael G., Potts, Christopher L.. 1994-05-22. (abstract) Maneuver Design for Galileo Asteroid Flybys. https://ntrs.nasa.gov/citations/20060039619
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