Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers

Table 8

Single planet flyby results from Earth to Hylonome.

Result	Value
from Earth	[−6.706 6.666 1.961] km/s
to	[−8.356 1.634 −0.093] km/s
from	[−6.492 −5.393 1.129] km/s
to Target	[−1.913 −1.497 0.152] km/s
Total Flyby at	[1.864 −7.027 1.222] km/s
Total Flyby
Magnitude at	7.372 km/s
Maneuver at	0.000 km/s
Gravity assist benefit	7.372 km/s
Maneuver at Earth	6.856 km/s
Maneuver at target	2.434 km/s
Total	9.290 km/s
Total of orbiter	2.434 km/s