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Nova MM T10RR-3-2
Part of Nova 2 stage series Family
LOx/LH2 propellant rocket stage. Operational date would have been July 1977. Recoverable stage.

Status: Study 1963. Thrust: 12,052.00 kN (2,709,397 lbf). Gross mass: 1,229,000 kg (2,709,000 lb). Unfuelled mass: 136,000 kg (299,000 lb). Specific impulse: 454 s. Burn time: 397 s. Height: 21.80 m (71.50 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 T10RR-3. Propellants: Lox/LH2.

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