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Nova 2 F-1 Module
Part of Nova 2 stage series Family
Nova NASA 8 F-1
Nova NASA 8 F-1
Nova NASA 8 F-1 Modular
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Short Nova building block. Four used in stage 1, one in stage 2.

Status: Study 1960. Thrust: 15,121.00 kN (3,399,336 lbf). Gross mass: 1,134,000 kg (2,500,000 lb). Unfuelled mass: 77,000 kg (169,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 200 s. Height: 28.70 m (94.10 ft). Diameter: 10.10 m (33.10 ft). Span: 10.10 m (33.10 ft).

No Engines: 2.



Country: USA. Engines: F-1. Launch Vehicles: Nova 8L Mod. Propellants: Lox/Kerosene.

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