Nova 9L-3 (original) (raw)

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Nova 9L-3

Part of Nova 3 stage series

LOx/LH2 propellant rocket stage. Masses estimated based on total vehicle thrust, performance, and stage volumes.

Status: Study 1960. Thrust: 5,334.00 kN (1,199,130 lbf). Gross mass: 363,000 kg (800,000 lb). Unfuelled mass: 36,000 kg (79,000 lb). Specific impulse: 420 s. Burn time: 250 s. Height: 21.30 m (69.80 ft). Diameter: 10.10 m (33.10 ft). Span: 10.10 m (33.10 ft).

No Engines: 6.

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

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