This paper describes the maneuver design that achieved the necessary flyby conditions in a propellant-optimal manner while accomodating both trajectory and spacecraft operating constraints.
Maneuver Design for the Galileo VEEGA Trajectory
1993-08-16
Preprint
No indication
English
Maneuver Design for the Galileo VEEGA Trajectory
NTRS | 1993
|Maneuver Design for the Galileo VEEGA Trajectory
British Library Conference Proceedings | 1993
|Maneuver Design for the Galileo VEEGA Trajectory (AAS 93-566)
British Library Conference Proceedings | 1993
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