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
16.08.1993
Preprint
Keine Angabe
Englisch
Maneuver Design for the Galileo VEEGA Trajectory
British Library Conference Proceedings | 1993
|Maneuver Design for the Galileo VEEGA Trajectory
NTRS | 1993
|Maneuver Design for the Galileo VEEGA Trajectory (AAS 93-566)
British Library Conference Proceedings | 1993
|