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Nova 9L-2
Part of Nova 2 stage series Family
LOx/Kerosene propellant rocket stage. Masses estimated based on total vehicle thrust, performance, and stage volumes.

Status: Study 1960. Thrust: 30,243.00 kN (6,798,896 lbf). Gross mass: 1,814,000 kg (3,999,000 lb). Unfuelled mass: 125,000 kg (275,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 164 s. Height: 35.10 m (115.10 ft). Diameter: 13.70 m (44.90 ft). Span: 13.70 m (44.90 ft).

No Engines: 4.



Country: USA. Engines: F-1. Launch Vehicles: Nova 9L. Propellants: Lox/Kerosene.

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