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Saturn MS-II-1-J-2T-250K
Part of Saturn II Family
LOx/LH2 propellant rocket stage. Basic Saturn II with 41 inch stretch of hydrogen tank, uprated J-2T 250k engines with 25% improvement in thrust and 16 second increase in specific impulse.

Status: Study 1967. Thrust: 5,558.31 kN (1,249,558 lbf). Gross mass: 521,447 kg (1,149,593 lb). Unfuelled mass: 49,877 kg (109,959 lb). Specific impulse: 441 s. Specific impulse sea level: 290 s. Burn time: 348 s. Height: 25.88 m (84.90 ft). Diameter: 10.06 m (33.00 ft). Span: 10.06 m (33.00 ft).

No Engines: 5.



Country: USA. Engines: J-2T-250K. Launch Vehicles: Saturn MLV-V-1/J-2T/250K, Saturn MLV-V-4(S)-B. Propellants: Lox/LH2.

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