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Nova GD-F-1
Part of Nova 1 stage series Family
LOx/Kerosene propellant rocket stage. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions. Recoverable stage; separation at 3,365 m/s at 89,300 m altitude; splashdown using retrorockets under 8 46 m diameter parachutes 1300 km downrange.

Status: Study 1963. Thrust: 148,031.00 kN (33,278,692 lbf). Gross mass: 9,977,000 kg (21,995,000 lb). Unfuelled mass: 680,000 kg (1,490,000 lb). Specific impulse: 335 s. Specific impulse sea level: 310 s. Burn time: 203 s. Height: 54.30 m (178.10 ft). Diameter: 18.30 m (60.00 ft). Span: 26.20 m (85.90 ft).

No Engines: 4.



Country: USA. Engines: L-7.70. Launch Vehicles: Nova GD-F. Propellants: Lox/Kerosene.

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