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Nova GD-J-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 of ballistic shape; separation at 3,420 m/s at 93,900 m altitude; splashdown using retrorockets under 7 parachutes 1340 km downrange.

Status: Study 1963. Thrust: 124,044.00 kN (27,886,200 lbf). Gross mass: 8,617,000 kg (18,997,000 lb). Unfuelled mass: 680,000 kg (1,490,000 lb). Specific impulse: 330 s. Specific impulse sea level: 310 s. Burn time: 203 s. Height: 36.60 m (120.00 ft). Diameter: 42.40 m (139.10 ft). Span: 20.10 m (65.90 ft).

No Engines: 4.



Country: USA. Engines: L-6.55. Launch Vehicles: Nova GD-J. Propellants: Lox/Kerosene.

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