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Saturn MS-II-1-J-2T-200K
Part of Saturn II Family
LOx/LH2 propellant rocket stage. Basic Saturn II with 41 inch stretch of hydrogen tank, uprated J-2T 200k engines with 10 second increase in specific impulse.

Status: Study 1965. Thrust: 4,446.65 kN (999,646 lbf). Gross mass: 521,447 kg (1,149,593 lb). Unfuelled mass: 49,877 kg (109,959 lb). Specific impulse: 435 s. Specific impulse sea level: 300 s. Burn time: 429 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-200K. Launch Vehicles: Saturn MLV-V-1/J-2T/200K. Propellants: Lox/LH2.

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