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Nova MM T10EE-1-2
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been November 1976. Expendable stage.

Status: Study 1963. Thrust: 11,032.00 kN (2,480,092 lbf). Gross mass: 1,125,000 kg (2,480,000 lb). Unfuelled mass: 136,000 kg (299,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 393 s. Height: 23.30 m (76.40 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 2.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM T10EE-1, Nova MM T10RE-1. Propellants: Lox/LH2.

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