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Auto Credit Based on jcn's Interplanetary Lander & Return Module

2 stages to orbit, interplanetary transfer stage, lander & rover. Rover cover auto-ejects at <10k AGL if parachutes are armed, otherwise you can stage it manually. Lander can safely return all 5 astronauts to Droo. Crew capsule has a planetary transfer window calculator built in (AG#4).
Credit to GoldenShadowGS for the calc program.

Rover is fairly tip-proof up to 10 m/s or so (50% power). If you go faster and flip it, try using the piston to right it.

Crew Capsule AGs & Sliders =
AG1 - Running Lights
AG2 - Forward Lights
AG3 - Landing Lights
AG4 - X-fer Window Calculator
AG8 - Landing Gear
AG9 - Solar Panels
AG0 - RCS
Slider 4 - Lower Rover (pistons)

Rover AGs & Sliders =
AG1 - Head/Tail Lights
AG2 - Undercarriage Lights
AG3 - Parking Brake
AG9 - Solar Panels
Slider 1 - Piston Hinge
Slider 2 - Piston Rotator
Slider 3 - Piston Extend/Retract

Video of sample mission to Cylero and back:
https://www.simplerockets.com/Videos/View/280512

GENERAL INFO

PERFORMANCE

  • Total Delta V: 14.8km/s
  • Total Thrust: 184.5MN
  • Engines: 137
  • Wet Mass: 6.89E+6kg
  • Dry Mass: 5.98E+5kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 38 2.9km/s 118.3MN 2.0m 6.89E+6kg
2 13 2.8km/s 40.5MN 2.6m 3.12E+6kg
3 7 3.9km/s 16.7MN 3.6m 1.42E+6kg
4 4 1.8km/s 4.7MN 2.2m 4.77E+5kg
8 18 3.4km/s 1.8MN 3.1m 1.59E+5kg
9 0 0m/s 0N 0s 25,728kg

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