Saturn IVB (original) (raw)

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Saturn IVB

Part of Saturn IV

LOx/LH2 propellant rocket stage. Configuration as flown on Saturn V.

Status: Flown 1967. Thrust: 1,031.98 kN (231,999 lbf). Gross mass: 119,920 kg (264,370 lb). Unfuelled mass: 13,311 kg (29,345 lb). Specific impulse: 425 s. Specific impulse sea level: 200 s. Burn time: 475 s. Height: 17.80 m (58.30 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

Cost $ : 58.290 million.

Country: USA. Engines: J-2. Launch Vehicles: Saturn C-4, Saturn C-8. Propellants: Lox/LH2.

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