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