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Auto Credit Based on Jayeshkhemani's MARS/CYLERO EXPLORATION SYSTEM(Drone,Rover, Satellite)

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GENERAL INFO

PERFORMANCE

  • Total Delta V: 68.5km/s
  • Total Thrust: 68.1MN
  • Engines: 12
  • Wet Mass: 3.35E+6kg
  • Dry Mass: -52,537,488kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 4 2.9km/s 35.7MN 2.9m 3.35E+6kg
2 1 3.0km/s 18.6MN 2.1m 1.2E+6kg
3 1 39.7km/s 10.4MN 4.34hours 4.21E+5kg
6 0 0m/s 0N 0s 91,899kg
7 3 22.8km/s 3.3MN 6.0m 91,899kg
8 0 0m/s 0N 0s 76,188kg

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