Auto Credit Based on VosAerospace's Blue Origin/National Team Lunar Lander

In continuation of my Blue Origin series, here is their proposal to NASA for the 2024 Lunar Lander. It uses a three stage system, with a Transfer stage, Landing stage, and ascent stage.

Edits: RCS, better landing system.

GENERAL INFO

PERFORMANCE

  • Total Delta V: 3.6km/s
  • Total Thrust: 3.0MN
  • Engines: 6
  • Wet Mass: 1.26E+5kg
  • Dry Mass: 26,490kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 1 1.5km/s 1.9MN 79s 1.26E+5kg
3 1 1.7km/s 878kN 1.6m 69,196kg
4 1 458m/s 158kN 3.1m 69,196kg

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