International Journal of Aerospace Engineering / 2016 / Article / Tab 15

Research Article

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

Table 15

The minimum transfer duration between random two planets.

MercuryVenusEarthMarsJupiterSaturnUranusNeptune

Mercury1025255020010010002500
Venus25501515025020015003000
Earth251550200200505050
Mars5015020015050050025002500
Jupiter200250200500100050025002500
Saturn10020050500500250500500
Uranus100015005025002500500500020000
Neptune2500300050250025005002000010000

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