Engine Model: Mage 2. Designer: SEP. Gross Mass: 530 kg (1,160 lb). Empty Mass: 40 kg (88 lb). Propellants: Solid. Thrust(vac): 45.500 kN (10,229 lbf). Isp: 293 sec. Burn time: 44 sec. Diameter: 0.77 m (2.52 ft). Length: 1.52 m (4.98 ft). Chambers: 1. Chamber Pressure: 48.00 bar. Area Ratio: 65.00. Country: France. First Flight: 1984. Last Flight: 1989. Flown: 17. Orbital circularization motor.
Mage 2 used on Rocket Stages
- Used on stage: Mage. on launch vehicle: Scout.