Auto Credit Based on NeptuneX's Poesiden heavy-RSS Triton mars orbital spacecraft

The first rover to venus desgined by neptuneX.
Happy Flying!!

GENERAL INFO

PERFORMANCE

  • Total Delta V: 35.0km/s
  • Total Thrust: 71.6MN
  • Engines: 42
  • Wet Mass: 2.6E+6kg
  • Dry Mass: 2.66E+5kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 21 3.9km/s 52.9MN 2.5m 2.6E+6kg
4 7 2.6km/s 16.0MN 40s 3.76E+5kg
6 7 1.4km/s 859kN 3.0m 1.18E+5kg
8 7 27.0km/s 1.8MN 4.9m 66,629kg

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