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Saturn IVB (S-V)
Part of Saturn IV Family
LOx/LH2 propellant rocket stage. Saturn V version of S-IVB stage for use with upper stage.

Status: Study 1968. Thrust: 1,031.60 kN (231,913 lbf). Gross mass: 119,900 kg (264,300 lb). Unfuelled mass: 13,300 kg (29,300 lb). Specific impulse: 421 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).



Country: USA. Engines: J-2. Launch Vehicles: Saturn V 2, Saturn INT-20, Saturn V-A, Saturn V-C, Saturn V-D, Saturn V-Centaur. Propellants: Lox/LH2.

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