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Nova 9L-4
Part of Nova 4 stage series Family
LOx/LH2 propellant rocket stage. Masses estimated based on total vehicle thrust, performance, and stage volumes.

Status: Study 1960. Thrust: 1,775.00 kN (399,035 lbf). Gross mass: 118,000 kg (260,000 lb). Unfuelled mass: 14,000 kg (30,000 lb). Specific impulse: 420 s. Burn time: 235 s. Height: 20.70 m (67.90 ft). Diameter: 6.70 m (21.90 ft). Span: 6.70 m (21.90 ft).

No Engines: 2.



Country: USA. Engines: J-2. Launch Vehicles: Nova 9L, Nova 5S. Propellants: Lox/LH2.

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