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Mage 1
SEP solid rocket engine. Out of production. Orbital circularization motor. First flight 1979.

Status: Out of production. Number: 11 . Thrust: 19.40 kN (4,361 lbf). Gross mass: 369 kg (813 lb). Unfuelled mass: 34 kg (74 lb). Specific impulse: 295 s. Specific impulse sea level: 220 s. Burn time: 50 s. Height: 1.13 m (3.70 ft). Diameter: 0.77 m (2.52 ft).

Thrust (sl): 14.500 kN (3,260 lbf). Thrust (sl): 1,475 kgf. Area Ratio: 45.



Country: France. Launch Vehicles: Ariane 1. Propellants: Solid. Stages: Mage 1.

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