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Nova DAC ISI-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: 33,754.00 kN (7,588,201 lbf). Gross mass: 1,696,000 kg (3,739,000 lb). Unfuelled mass: 107,000 kg (235,000 lb). Specific impulse: 455 s. Burn time: 206 s. Height: 30.50 m (100.00 ft). Diameter: 21.30 m (69.80 ft). Span: 21.30 m (69.80 ft).

No Engines: 8.



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

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