Nova MM T10RR-2-2

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Nova MM T10RR-2-2

Part of Nova 2 stage series

LOx/LH2 propellant rocket stage. Operational date would have been December 1976. Recoverable stage.

Status: Study 1963. Thrust: 20,015.00 kN (4,499,550 lbf). Gross mass: 2,041,000 kg (4,499,000 lb). Unfuelled mass: 181,000 kg (399,000 lb). Specific impulse: 455 s. Burn time: 408 s. Height: 24.40 m (80.00 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

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

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