EngineS200Drag to turn · Space takes it apart5,150 kN vac · 205 t · cold
S200 by SDSC: solid fuel rocket motor burning HTPB (active). Thrust 5,150 kN in vacuum. 70 bar chamber pressure, 274 s in vacuum, 205,000 kg loaded. Figures from the database's engine record. Drawn to the published length and diameter (Wikipedia); other proportions are estimated.