CZ-1C-3

home topic index

Engine Model: CZ-1C-3. Propellants: N2O4/UDMH. Thrust(vac): 107.900 kN (24,257 lbf). Thrust(sl): 97.000 kN (21,806 lbf). Isp: 287 sec. Isp (sea level): 258 sec. Burn time: 164 sec. Diameter: 1.80 m (5.90 ft). Chambers: 1. Country: China. Status: Development ended 1988. CZ-1C-3 used on Rocket Stages Used on stage: CZ-1C-3. on launch vehicle: CZ-1. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.