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Nova MM T10RR-2-1
Part of Nova 1 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been December 1976. Recoverable stage.

Status: Study 1963. Thrust: 176,686.00 kN (39,720,592 lbf). Gross mass: 9,089,000 kg (20,037,000 lb). Unfuelled mass: 680,000 kg (1,490,000 lb). Specific impulse: 304 s. Specific impulse sea level: 271 s. Burn time: 139 s. Height: 43.50 m (142.70 ft). Diameter: 21.30 m (69.80 ft). Span: 30.10 m (98.70 ft).

No Engines: 24.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM T10RR-2. Propellants: Lox/LH2.

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