This page no longer updated from 31 October 2001. Latest version can be found at Mage 1

Designer: SEP. Used on stages: Mage 1. Used on launch vehicles: Ariane 1. Gross Mass: 369 kg. Empty Mass: 34 kg. Propellants: Solid Thrust(vac): 1,978 kgf. Thrust(vac): 19.40 kN. Isp: 295 sec. Isp (sea level): 220 sec. Burn time: 50 sec. Diameter: 0.8 m. Length: 1.1 m. Chambers: 1. Area Ratio: 45.00. Country: France. Status: Out of Production. First Flight: 1979. Last Flight: 1986. Flown: 11. Comments: Orbital circularization motor.
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Last update 12 March 2001.
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© Mark Wade, 2001 .