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Nova 59-4-2
Part of Nova 2 stage series Family
LOx/Kerosene propellant rocket stage. Empty Mass Estimated.

Status: Study 1959. Thrust: 7,560.00 kN (1,699,550 lbf). Gross mass: 590,000 kg (1,300,000 lb). Unfuelled mass: 45,000 kg (99,000 lb). Specific impulse: 310 s. Specific impulse sea level: 265 s. Burn time: 215 s. Height: 16.20 m (53.10 ft). Diameter: 5.20 m (17.00 ft). Span: 5.20 m (17.00 ft).



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

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