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Nova MM-1
Part of Nova 1 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been December 1974.

Status: Study 1963. Thrust: 95,261.00 kN (21,415,524 lbf). Gross mass: 5,040,000 kg (11,110,000 lb). Unfuelled mass: 317,000 kg (698,000 lb). Specific impulse: 451 s. Specific impulse sea level: 379 s. Burn time: 215 s. Height: 49.80 m (163.30 ft). Diameter: 21.60 m (70.80 ft). Span: 23.20 m (76.10 ft).

No Engines: 18.



Country: USA. Engines: HP-1. Launch Vehicles: Nova MM 24G. Propellants: Lox/LH2.

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