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Nova 60-8-1
Part of Nova 1 stage series Family
Nova NASA 8 F-1
Nova NASA 8 F-1
Credit: © Mark Wade
LOx/Kerosene propellant rocket stage. Mass estimated based on total LV weight.

Status: Study 1960. Thrust: 61,928.00 kN (13,921,968 lbf). Gross mass: 3,628,000 kg (7,998,000 lb). Unfuelled mass: 227,000 kg (500,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 161 s. Height: 41.20 m (135.10 ft). Diameter: 17.40 m (57.00 ft). Span: 18.00 m (59.00 ft).

No Engines: 8.



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

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