Saturn MS-IVB-3B

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Saturn MS-IVB-3B

Part of Saturn IV

LOx/LH2 propellant rocket stage. S-IVB with 16.5 foot stretch, 350,000 pounds propellant, 1 400,000 pound thrust toroidal engine.

Status: Study 1967. Thrust: 1,778.90 kN (399,913 lbf). Gross mass: 179,200 kg (395,000 lb). Unfuelled mass: 20,400 kg (44,900 lb). Specific impulse: 447 s. Specific impulse sea level: 200 s. Burn time: 385 s. Height: 22.82 m (74.86 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

Family: Space Tugs. Country: USA. Engines: Toroidal 400k. Launch Vehicles: Saturn V-3B. Propellants: Lox/LH2.

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