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

Status: Study 1963. Thrust: 97,840.00 kN (21,995,300 lbf). Gross mass: 4,213,000 kg (9,288,000 lb). Unfuelled mass: 194,000 kg (427,000 lb). Specific impulse: 299 s. Specific impulse sea level: 260 s. Burn time: 118 s. Height: 25.90 m (84.90 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 4.



Country: USA. Engines: 5 mlbf RP-4. Launch Vehicles: Nova-1 DAC. Propellants: Lox/Kerosene.

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