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Nova MM R10R-2 stage
Part of Nova 2 stage series Family
Air/LOx/LH2 propellant rocket stage. Operational date would have been October 1980. Recoverable stage. Air-augmented plug nozzle.

AKA: Nova MM R10R-2. Status: Study 1963. Thrust: 140,539.00 kN (31,594,424 lbf). Gross mass: 8,647,000 kg (19,063,000 lb). Unfuelled mass: 1,361,000 kg (3,000,000 lb). Specific impulse: 620 s. Specific impulse sea level: 620 s. Burn time: 310 s. Height: 49.30 m (161.70 ft). Diameter: 21.30 m (69.80 ft). Span: 43.70 m (143.30 ft).

No Engines: 40.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM R10R-2. Propellants: Air/Lox/LH2.

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