Saturn MS-IVB-1

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Saturn MS-IVB-1

Part of Saturn IV

LOx/LH2 propellant rocket stage. Marshall studies, 1965: S-IVB structurally strengthened to handle larger payloads, otherwise unchanged.

Status: Study 1965. Thrust: 1,031.60 kN (231,913 lbf). Gross mass: 120,500 kg (265,600 lb). Unfuelled mass: 13,900 kg (30,600 lb). Specific impulse: 421 s. Specific impulse sea level: 200 s. Burn time: 475 s. Height: 18.08 m (59.31 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

Family: Space Tugs. Country: USA. Engines: J-2. Launch Vehicles: Saturn MLV-V-4(S), Saturn MLV-V-1, Saturn MLV-V-4(S)-A. Propellants: Lox/LH2.

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