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SLS Stage C
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Gross Mass: 825,000 kg (1,818,000 lb). Empty Mass: 58,000 kg (127,000 lb). Thrust (vac): 10,673.322 kN (2,399,458 lbf). Isp: 428 sec. Burn time: 350 sec. Propellants: Lox/LH2. Diameter: 7.62 m (24.99 ft). Span: 7.62 m (24.99 ft). Length: 53.00 m (173.00 ft). Country: USA. No Engines: 2. Engine: M-1. Status: Study 1961. Launch vehicle core stage for Project Lunex. Masses estimated based on optimum apportioning of B+C stage total masses. Thrust, engines estimated based on requirements.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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