Research Article
Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers
Table 13
Mission total and orbiter
to Ceres for 30-year time span and 200-year time span.
| | Single | Double | Triple |
| 30 years | | | | Total | 10.971 Km/s | 10.021 Km/s | 16.203 Km/s | Orbiter | 5.277 Km/s | 6.118 Km/s | 10.101 Km/s | 200 years | | | | Total | 10.340 Km/s | 10.365 Km/s | 13.229 Km/s | Orbiter | 5.457 Km/s | 5.934 Km/s | 8.796 Km/s |
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