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Nova MM S10R-2 stage
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been July 1978. SSTO; recoverable; payload 842,000 lbs.

AKA: Nova MM S10R-2. Status: Study 1963. Thrust: 160,672.00 kN (36,120,502 lbf). Gross mass: 10,502,000 kg (23,152,000 lb). Unfuelled mass: 839,000 kg (1,849,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 263 s. Height: 56.60 m (185.60 ft). Diameter: 21.30 m (69.80 ft). Span: 40.90 m (134.10 ft).

No Engines: 30.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM S10R-2. Propellants: Lox/LH2.

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