EngineAJ-60ADrag to turn · Space takes it apart1,631 kN · 44 t · cold
AJ-60A by Aerojet Rocketdyne: solid fuel rocket motor burning HTPB (retired). Thrust 1,631 kN at sea level, 1,688 kN in vacuum. 62 bar chamber pressure, 274 s specific impulse at sea level, 274 s in vacuum, 44,000 kg loaded. Figures from the database's engine record. Drawn to the published length and diameter (Wikipedia); other proportions are estimated.