International Journal of Aerospace Engineering / 2016 / Article / Tab 16

Research Article

Multiple Gravity Assist Spacecraft Trajectories Design Based on BFS and EP_DE Algorithm

Table 16

The maximum transfer duration between random two planets.

MercuryVenusEarthMarsJupiterSaturnUranusNeptune

Mercury30060045012009000150075000120000
Venus60070560012009000150075000120000
Earth45060075015003000900750750
Mars120012001500150012000900075000120000
Jupiter900090003000120007500900090000135000
Saturn1500150090090009000300075000120000
Uranus750007500075075000900007500075000300000
Neptune120000120000750120000135000120000300000120000

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