The OSC² is a powerfull three-stage booster assisted space rocket that can get cargo and people in LEO but also MEO orbits. Depending on launch location and orbit type different amounts of fuel consumtion will occour. The passenger cabin comes with an integrated launch abort system. It's first stage engine provides 7,993KN of initial thrust and it's second stage engine provides 1,677KN of initial thrust. The boosters add an additional 1,334KN. The first stage is not currently reusable. This feature will likely come with the OSC^4.

__Controls:__
Yaw - Manual Vertical Axes Rotation Control (MAVEARC) 1st stage
Pitch/Roll - Second Stage Controls

__Activation Groups:__
1 - Booster separation (50,000ft)
2 - First stage separation (180,000 - 200,000ft)
3 - Second stage separation (~290,000ft)
4 - Guidechute (re-entry ~45,000ft)
5 - Parachute (10,000ft - 2,000ft)

Above measurements are in feet above ground level.