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Nova MM T10RR-3-1
Part of Nova 1 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been July 1977. Recoverable stage. 10% plug nozzle.

Status: Study 1963. Thrust: 109,000.00 kN (24,504,000 lbf). Gross mass: 5,517,000 kg (12,162,000 lb). Unfuelled mass: 680,000 kg (1,490,000 lb). Specific impulse: 454 s. Specific impulse sea level: 377 s. Burn time: 194 s. Height: 61.30 m (201.10 ft). Diameter: 21.30 m (69.80 ft). Span: 28.00 m (91.00 ft).

No Engines: 18.



Country: USA. Engines: CD Module. Launch Vehicles: Nova MM T10RR-3. Propellants: Lox/LH2.

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