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

Status: Study 1960. Thrust: 45,914.00 kN (10,321,877 lbf). Gross mass: 1,995,000 kg (4,398,000 lb). Unfuelled mass: 100,000 kg (220,000 lb). Specific impulse: 304 s. Specific impulse sea level: 265 s. Burn time: 121 s. Height: 28.00 m (91.00 ft). Diameter: 12.20 m (40.00 ft). Span: 12.20 m (40.00 ft).

No Engines: 6.



Country: USA. Engines: F-1. Launch Vehicles: Nova B, Nova D. Propellants: Lox/Kerosene.

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