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Auto Credit Based on ApolloNasa17's Manned Orbiting Laboratory TITAN IIIM

well....yeah and thanks for the Gemini, CardZlol and thanks for the Titan IIIC and the MOL , ApolloNasa17. i put a KAL automated launch.

GENERAL INFO

PERFORMANCE

  • Total Delta V: 7.1km/s
  • Total Thrust: 24.0MN
  • Engines: 30
  • Wet Mass: 4.47E+5kg
  • Dry Mass: 1.22E+5kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 6 1.9km/s 9.5MN 87s 4.47E+5kg
2 0 0m/s 0N 0s 1.78E+5kg
3 2 5.1km/s 3.4MN 85s 1.16E+5kg
7 4 3m/s 111kN 2s 57,113kg
11 0 0m/s 0N 0s 3,163kg

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