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Nova 59-4-3
Part of Nova 4 stage series Family
LOx/LH2 propellant rocket stage. Empty Mass Estimated.

Status: Study 1959. Thrust: 1,421.00 kN (319,453 lbf). Gross mass: 168,000 kg (370,000 lb). Unfuelled mass: 18,000 kg (39,000 lb). Specific impulse: 420 s. Specific impulse sea level: 306 s. Burn time: 426 s. Height: 14.00 m (45.00 ft). Diameter: 5.20 m (17.00 ft). Span: 5.20 m (17.00 ft).

No Engines: 4.



Country: USA. Engines: LH2-80k. Launch Vehicles: Nova 4L. Propellants: Lox/LH2.

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