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Nova DAC 2-1
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: 102,293.00 kN (22,996,381 lbf). Gross mass: 4,943,000 kg (10,897,000 lb). Unfuelled mass: 311,000 kg (685,000 lb). Specific impulse: 410 s. Specific impulse sea level: 345 s. Burn time: 179 s. Height: 82.30 m (270.00 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 15.



Country: USA. Engines: M-1. Launch Vehicles: Nova-2 DAC. Propellants: Lox/LH2.

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