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SLS Stage C
Part of Nova 3 stage series Family
LOx/LH2 propellant rocket stage. 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.

Status: Study 1961. Thrust: 10,673.32 kN (2,399,458 lbf). Gross mass: 825,000 kg (1,818,000 lb). Unfuelled mass: 58,000 kg (127,000 lb). Specific impulse: 428 s. Burn time: 350 s. Height: 53.00 m (173.00 ft). Diameter: 7.62 m (24.99 ft). Span: 7.62 m (24.99 ft).

No Engines: 2.



Country: USA. Engines: M-1. Launch Vehicles: SLS BC-2720. Propellants: Lox/LH2.

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