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 2. on launch vehicle: Advanced Scout.

Used on stage: Mage 2. on launch vehicle: Ariane 2/3.

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