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Cargo LV Stage 1
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Gross Mass: 1,093,330 kg (2,410,380 lb). Empty Mass: 88,449 kg (194,996 lb). Thrust (vac): 10,441.061 kN (2,347,244 lbf). Isp: 452 sec. Burn time: 420 sec. Propellants: Lox/LH2. Isp(sl): 361 sec. Diameter: 8.40 m (27.50 ft). Span: 8.40 m (27.50 ft). Length: 64.27 m (210.85 ft). Country: USA. No Engines: 5. Engine: SSME. Status: Study 2005. Core vehicle proposed by NASA for Project Constellation exploration of moon and Mars. It would use shuttle external tank tooling. All masses estimated.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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