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Nova DAC-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: 26,683.00 kN (5,998,577 lbf). Gross mass: 2,268,000 kg (5,000,000 lb). Unfuelled mass: 143,000 kg (315,000 lb). Specific impulse: 426 s. Burn time: 327 s. Height: 27.40 m (89.80 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 4.



Country: USA. Engines: M-1. Launch Vehicles: Nova-1 DAC. Propellants: Lox/LH2.

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