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Minuteman-1
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Gross Mass: 23,077 kg (50,876 lb). Empty Mass: 2,292 kg (5,052 lb). Thrust (vac): 791.300 kN (177,891 lbf). Isp: 262 sec. Burn time: 60 sec. Propellants: Solid. Isp(sl): 237 sec. Diameter: 1.67 m (5.47 ft). Span: 1.67 m (5.47 ft). Length: 7.49 m (24.57 ft). Country: USA. No Engines: 1. Engine: M55/TX-55/Tu-122. Status: In production. First Flight: 2000. Last Flight: 2006. No Launched: 5. First stage of Minuteman I. Proposed as zero stage for various Saturn variants in 1960's. Surplus motors used in ABM SDI tests in 1980's and 1990's.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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