Chinese N2O4/UDMH rocket engine. Development ended 1988. Used on CZ-1C launch vehicle.
AKA: CZ-1C-3. Status: Development ended 1988. Thrust: 107.90 kN (24,257 lbf). Specific impulse: 287 s. Specific impulse sea level: 258 s. Burn time: 164 s. Diameter: 1.80 m (5.90 ft).