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Mage 1
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Designer: SEP. Gross Mass: 369 kg (813 lb). Empty Mass: 34 kg (74 lb). Propellants: Solid. Thrust(vac): 19.400 kN (4,361 lbf). Thrust(sl): 14.500 kN (3,260 lbf). Isp: 295 sec. Isp (sea level): 220 sec. Burn time: 50 sec. Diameter: 0.77 m (2.52 ft). Length: 1.13 m (3.70 ft). Chambers: 1. Area Ratio: 45.00. Country: France. Status: Out of production. First Flight: 1979. Last Flight: 1986. Flown: 11. Orbital circularization motor.
Mage 1 used on Rocket Stages
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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