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Saturn IVB C-3B
Part of Saturn IV Family
LOx/LH2 propellant rocket stage. Final common third stage design for Saturn C-3B (November 1961).

Status: Study 1961. Thrust: 889.33 kN (199,928 lbf). Gross mass: 52,144 kg (114,957 lb). Unfuelled mass: 6,801 kg (14,993 lb). Specific impulse: 420 s. Specific impulse sea level: 200 s. Burn time: 207 s. Height: 15.40 m (50.50 ft). Diameter: 5.59 m (18.33 ft). Span: 5.59 m (18.33 ft).



Country: USA. Engines: J-2. Launch Vehicles: Saturn C-3B. Propellants: Lox/LH2.

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