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Nova DAC ISI-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: 70,146.00 kN (15,769,448 lbf). Gross mass: 3,084,000 kg (6,799,000 lb). Unfuelled mass: 142,000 kg (313,000 lb). Specific impulse: 350 s. Specific impulse sea level: 320 s. Burn time: 141 s. Height: 30.50 m (100.00 ft). Diameter: 21.30 m (69.80 ft). Span: 28.00 m (91.00 ft).

No Engines: 14.



Country: USA. Engines: Chamber/single nozzle. Launch Vehicles: Nova DAC ISI. Propellants: Lox/LH2.

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