Nova MM S10E-2 stage

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Nova MM S10E-2 stage

Part of Nova 2 stage series

LOx/LH2 propellant rocket stage. Operational date would have been November 1977. SSTO; expendable; payload 1,283,000 lbs.

AKA: Nova MM S10E-2. Status: Study 1963. Thrust: 160,672.00 kN (36,120,502 lbf). Gross mass: 10,302,000 kg (22,712,000 lb). Unfuelled mass: 639,000 kg (1,408,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 263 s. Height: 54.80 m (179.70 ft). Diameter: 21.30 m (69.80 ft). Span: 36.70 m (120.40 ft).

No Engines: 30.

Country: USA. Engines: CD Module. Launch Vehicles: Nova MM S10E-2. Propellants: Lox/LH2.

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