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Nova A-3
Part of Saturn IV Family
LOx/LH2 propellant rocket stage. .

Status: Study 1960. Thrust: 313.00 kN (70,365 lbf). Gross mass: 40,000 kg (88,000 lb). Unfuelled mass: 4,000 kg (8,800 lb). Specific impulse: 427 s. Burn time: 480 s. Height: 13.10 m (42.90 ft). Diameter: 5.80 m (19.00 ft). Span: 5.80 m (19.00 ft).

No Engines: 5.



Country: USA. Engines: RL-10. Launch Vehicles: Nova A. Propellants: Lox/LH2.

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