LAB / PROTOTYPE
Engineering
Size a build before committing resources.
FLIGHT PARAMETERS
RESULT
Viable configuration+35,9%thrust margin
- Minimum to lift
- 2×
- Vertical acceleration
- 3,52 m/s²
- Weight
- 176,6 kN
- Installed thrust
- 240 kN
Space Engineers 2Wiki
VS2.4 · en-US · sourced data
LAB / PROTOTYPE
Size a build before committing resources.
FLIGHT PARAMETERS
RESULT