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Nova 59-4-1
Part of Nova 1 stage series Family
Nova NASA 4 F-1
Nova NASA 4 F-1
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Empty Mass Estimated.

Status: Study 1959. Thrust: 38,697.00 kN (8,699,431 lbf). Gross mass: 2,177,000 kg (4,799,000 lb). Unfuelled mass: 136,000 kg (299,000 lb). Specific impulse: 295 s. Specific impulse sea level: 257 s. Burn time: 150 s. Height: 23.20 m (76.10 ft). Diameter: 15.50 m (50.80 ft). Span: 15.50 m (50.80 ft).

No Engines: 5.



Country: USA. Engines: F-1. Launch Vehicles: Nova 4L. Propellants: Lox/Kerosene.

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