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Nova MM 1C-2
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been February 1973.

Status: Study 1963. Thrust: 20,015.00 kN (4,499,550 lbf). Gross mass: 2,041,000 kg (4,499,000 lb). Unfuelled mass: 163,000 kg (359,000 lb). Specific impulse: 428 s. Burn time: 387 s. Height: 49.70 m (163.00 ft). Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft).

No Engines: 3.

Country: USA. Engines: M-1. Launch Vehicles: Nova MM 1C. Propellants: Lox/LH2.



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