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Nova NASA-1
Part of Nova 1 stage series
Nova NASA 6 F-1
Nova NASA 6 F-1
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. .

Status: Study 1959. Thrust: 45,914.00 kN (10,321,877 lbf). Gross mass: 2,268,000 kg (5,000,000 lb). Unfuelled mass: 113,000 kg (249,000 lb). Specific impulse: 296 s. Specific impulse sea level: 257 s. Burn time: 134 s. Height: 31.40 m (103.00 ft). Diameter: 14.60 m (47.90 ft). Span: 14.60 m (47.90 ft).

No Engines: 6.



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

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