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Nova MM S10E-1 stage
Part of Nova 1 stage series
LOx/LH2 propellant rocket stage. Operational date would have been October 1977. SSTO; expendable.

AKA: Nova MM S10E-1. Status: Study 1963. Thrust: 160,672.00 kN (36,120,502 lbf). Gross mass: 10,317,000 kg (22,745,000 lb). Unfuelled mass: 635,000 kg (1,399,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 264 s. Height: 65.70 m (215.50 ft). Diameter: 24.40 m (80.00 ft). Span: 26.90 m (88.20 ft).

No Engines: 24.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM S10E-1. Propellants: Lox/LH2.

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