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Nova 9L-1
Part of Nova 1 stage series Family
Nova NASA 9 F-1
Nova NASA 9 F-1
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Masses estimated based on total vehicle thrust, performance, and stage volumes.

Status: Study 1960. Thrust: 68,048.00 kN (15,297,798 lbf). Gross mass: 2,721,000 kg (5,998,000 lb). Unfuelled mass: 181,000 kg (399,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 110 s. Height: 42.70 m (140.00 ft). Diameter: 15.20 m (49.80 ft). Span: 15.20 m (49.80 ft).

No Engines: 9.



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

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