Nova B-3 (original) (raw)

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Nova B-3

Part of Saturn IV

LOx/LH2 propellant rocket stage. .

Status: Study 1960. Thrust: 451.00 kN (101,388 lbf). Gross mass: 63,000 kg (138,000 lb). Unfuelled mass: 5,000 kg (11,000 lb). Specific impulse: 427 s. Burn time: 533 s. Height: 18.30 m (60.00 ft). Diameter: 6.70 m (21.90 ft). Span: 6.70 m (21.90 ft).

No Engines: 7.

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

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