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Mage 2
SEP solid rocket engine. Orbital circularization motor for Advanced Scout, Ariane 2/3. First flight 1984.

Status: First flight 1984. Number: 17 . Thrust: 45.50 kN (10,229 lbf). Gross mass: 530 kg (1,160 lb). Unfuelled mass: 40 kg (88 lb). Specific impulse: 293 s. Burn time: 44 s. Height: 1.52 m (4.98 ft). Diameter: 0.77 m (2.52 ft).

Chamber Pressure: 48.00 bar. Area Ratio: 65.



Country: France. Launch Vehicles: Ariane 2/3, Ariane 3, Advanced Scout. Propellants: Solid. Stages: Mage 2.

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