Saturn MS-IVB-2 (original) (raw)

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Saturn MS-IVB-2

Part of Saturn IV

Advanced Engines

Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters
Credit: © Mark Wade

LOx/LH2 propellant rocket stage. Douglas Studies, 1965: S-IVB with 315 k high pressure 3000 psia engine, 350,000 pounds propellant.

Status: Study 1965. Thrust: 1,401.30 kN (315,025 lbf). Gross mass: 176,600 kg (389,300 lb). Unfuelled mass: 17,800 kg (39,200 lb). Specific impulse: 447 s. Specific impulse sea level: 200 s. Burn time: 489 s. Height: 23.12 m (75.85 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

Family: Space Tugs. Country: USA. Engines: HG-3. Launch Vehicles: Saturn MLV-V-2, Saturn MLV-V-3, Saturn IB-B. Propellants: Lox/LH2.

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