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Nova MM 1B-1
Part of Nova 1 stage series Family
LOx/Kerosene propellant rocket stage. Operational date would have been December 1972.

Status: Study 1963. Thrust: 125,770.00 kN (28,274,220 lbf). Gross mass: 7,430,000 kg (16,380,000 lb). Unfuelled mass: 454,000 kg (1,000,000 lb). Specific impulse: 304 s. Specific impulse sea level: 271 s. Burn time: 162 s. Height: 46.60 m (152.80 ft). Diameter: 20.00 m (65.00 ft). Span: 25.30 m (83.00 ft).

No Engines: 14.



Country: USA. Engines: F-1A. Launch Vehicles: Nova MM 1B. Propellants: Lox/Kerosene.

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