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Title: Maneuver Design for the Galileo VEEGA Trajectory
Authors: Potts, C.
Wilson, M.
Issue Date: 16-Aug-1993
Citation: Victoria, British Columbia
Abstract: 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.
Appears in Collections:JPL TRS 1992+

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