Engine Model: CZ-1D-3. Designer: Fourth Academy. Gross Mass: 875 kg (1,929 lb). Propellants: Solid. Isp: 291 sec. Isp (sea level): 200 sec. Burn time: 100 sec. Diameter: 2.05 m (6.72 ft). Length: 2.20 m (7.20 ft). Chambers: 1. Country: China. Status: Out of production. First Flight: 1995. Last Flight: 2002. Flown: 3.00. Motor for proposed CZ-1D launch vehicle.
CZ-1D-3 used on Rocket Stages
- Used on stage: GF-01A. on launch vehicle: T-7.