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Nova GD-E-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: 26,683.00 kN (5,998,577 lbf). Gross mass: 4,535,000 kg (9,997,000 lb). Unfuelled mass: 363,000 kg (800,000 lb). Specific impulse: 428 s. Burn time: 646 s. Height: 47.90 m (157.10 ft). Diameter: 20.60 m (67.50 ft). Span: 20.60 m (67.50 ft).

No Engines: 4.



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

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