Autonomous Planning of Multigravity-Assist Trajectories with Deep Space Maneuvers Using a Differential Evolution Approach

Table 3

Solution trajectory for the Earth-Mars mission.

Mission parameter	Value
Departure date, 𝑡𝑑	02-Jun-2004 00:07:31
Departure impulse (km/s)	4.3517
DSM date	16-Aug-2004 14:23:36
DSM impulse (km/s)	0.32836
Venus swing-by date	18-Nov-2004 02:34:34
Pericenter altitude (km)	7890.1
Arrival date	16-May-2005 18:13:39
Arrival impulse (km/s)	6.0366
Mission duration (days)	348.75
Mission cost (km/s)	10.717