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Model: Nova MM R10R-2. Gross Mass: 8,647,000 kg (19,063,000 lb). Empty Mass: 1,361,000 kg (3,000,000 lb). Thrust (vac): 140,539.000 kN (31,594,424 lbf). Isp: 620 sec. Burn time: 310 sec. Propellants: Air/Lox/LH2. Isp(sl): 620 sec. Diameter: 21.30 m (69.80 ft). Span: 43.70 m (143.30 ft). Length: 49.30 m (161.70 ft). Country: USA. No Engines: 40. Motor: CD Module. Status: Study 1963.

Operational date would have been October 1980. Recoverable stage. Air-augmented plug nozzle.

Model: Nova MM R10E-2. Gross Mass: 8,474,000 kg (18,681,000 lb). Empty Mass: 1,188,000 kg (2,619,000 lb). Thrust (vac): 140,539.000 kN (31,594,424 lbf). Isp: 620 sec. Burn time: 310 sec. Propellants: Air/Lox/LH2. Isp(sl): 620 sec. Diameter: 21.30 m (69.80 ft). Span: 43.70 m (143.30 ft). Length: 49.10 m (161.00 ft). Country: USA. No Engines: 40. Motor: CD Module. Status: Study 1963.

Operational date would have been October 1980. Expendable stage. Air-augmented plug nozzle.

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