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Nova GD-J-2
Part of Nova 2 stage series
LOx/LH2 propellant rocket stage. Massed estimated based on tank volumes, total thrust, and first stage burnout conditions.

Status: Study 1963. Thrust: 13,346.00 kN (3,000,300 lbf). Gross mass: 1,270,000 kg (2,790,000 lb). Unfuelled mass: 91,000 kg (200,000 lb). Specific impulse: 428 s. Burn time: 365 s. Height: 38.00 m (124.00 ft). Diameter: 19.50 m (63.90 ft). Span: 19.50 m (63.90 ft).

No Engines: 2.



Country: USA. Engines: M-1. Launch Vehicles: Nova GD-J. Propellants: Lox/LH2.

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