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Shuttle ASRM
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Gross Mass: 625,000 kg (1,377,000 lb). Empty Mass: 75,000 kg (165,000 lb). Thrust (vac): 15,566.115 kN (3,499,402 lbf). Isp: 286 sec. Burn time: 133 sec. Propellants: Solid. Isp(sl): 259 sec. Diameter: 3.81 m (12.49 ft). Span: 3.81 m (12.49 ft). Length: 38.41 m (126.01 ft). Country: USA. No Engines: 1. Engine: Hercules. Status: In development. Cost $ : 250.000 million. First Flight: 1995. Other designations: Advanced Solid Rocket Motor. Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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