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

Status: Study 1963. Thrust: 96,379.00 kN (21,666,861 lbf). Gross mass: 4,944,000 kg (10,899,000 lb). Unfuelled mass: 317,000 kg (698,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 210 s. Height: 57.50 m (188.60 ft). Diameter: 21.30 m (69.80 ft). Span: 23.70 m (77.70 ft).

No Engines: 18.



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

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