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Nova MM 1C-1
Part of Nova 1 stage series Family
LOx/Kerosene propellant rocket stage. Operational date would have been February 1973.

Status: Study 1963. Thrust: 161,710.00 kN (36,353,850 lbf). Gross mass: 8,943,000 kg (19,715,000 lb). Unfuelled mass: 590,000 kg (1,300,000 lb). Specific impulse: 304 s. Specific impulse sea level: 271 s. Burn time: 151 s. Height: 49.70 m (163.00 ft). Diameter: 21.00 m (68.00 ft). Span: 27.10 m (88.90 ft).

No Engines: 18.



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

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