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Nova MM 24G-2
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been December 1974.

Status: Study 1963. Thrust: 10,228.00 kN (2,299,345 lbf). Gross mass: 1,043,000 kg (2,299,000 lb). Unfuelled mass: 136,000 kg (299,000 lb). Specific impulse: 451 s. Specific impulse sea level: 379 s. Burn time: 386 s. Height: 28.80 m (94.40 ft). Diameter: 18.30 m (60.00 ft). Span: 18.30 m (60.00 ft).

No Engines: 2.



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

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