This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: SEP. Used on stages: Mage 2. Used on launch vehicles: Advanced Scout, Ariane 2/3. Gross Mass: 530 kg. Empty Mass: 40 kg. Propellants: Solid Thrust(vac): 4,638 kgf. Thrust(vac): 45.50 kN. Isp: 293 sec. Burn time: 44 sec. Diameter: 0.8 m. Length: 1.5 m. Chambers: 1. Chamber Pressure: 48.00 bar. Area Ratio: 65.00. Country: France. Status: Out of Production. First Flight: 1984. Last Flight: 1989. Flown: 17. Comments: Orbital circularization motor.
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Last update 12 March 2001.
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© Mark Wade, 2001 .