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Nova MM S10R-1 stage
Part of Nova 1 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been June 1978. SSTO; recoverable.

AKA: Nova MM S10R-1. Status: Study 1963. Thrust: 160,672.00 kN (36,120,502 lbf). Gross mass: 10,470,000 kg (23,080,000 lb). Unfuelled mass: 816,000 kg (1,798,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 263 s. Height: 69.50 m (228.00 ft). Diameter: 24.40 m (80.00 ft). Span: 32.20 m (105.60 ft).

No Engines: 24.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM S10R-1. Propellants: Lox/LH2.

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