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Saturn II-SL
Part of Saturn II
LOx/LH2 propellant rocket stage. Saturn II modified with reduced expansion ratio J-2 engines for use a first stage (sea level launch). Requires solid rocket motor augmentation to get off the ground.

Status: Study 1966. Thrust: 5,500.77 kN (1,236,621 lbf). Gross mass: 490,952 kg (1,082,363 lb). Unfuelled mass: 44,240 kg (97,530 lb). Specific impulse: 390 s. Specific impulse sea level: 275 s. Burn time: 310 s. Height: 24.84 m (81.49 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 5.



Country: USA. Engines: J-2-SL. Launch Vehicles: Saturn INT-19. Propellants: Lox/LH2.

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