Optimization techniques are critical when investigating Earth to Mars trajectories since they have the potential of reducing the total (delta)V of a mission. A deep space maneuver (DSM) executed during the cruise may improve a trajectory by reducing the total mission V. Nonetheless, DSMs not only may improve trajectory performance (from an energetic point of view) but also open up new families of trajectories that would satisfy very specific mission requirements not achievable with ballistic trajectories. In the following pages, various specific examples showing the potential advantages of the usage of broken plane maneuvers will be introduced. These examples correspond to possible scenarios for Earth to Mars trajectories during the next decade (2010-2020).
Broken-Plane Maneuver Applications for Earth to Mars Trajectories
2007-09-24
Conference paper
No indication
English
Broken Plane MARS Trajectory Study Final Report
NTIS | 1969
Broken plane Mars trajectory study Final report
NTRS | 1969
Data return advantages of Earth-Mars-Earth trajectories.
NTRS | 1968
|Data return advantages of Earth-Mars-Earth trajectories.
AIAA | 1968
|Data return advantages of Earth-Mars-Earth trajectories
AIAA | 1967
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