Saturn IB-11

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Saturn IB-11

Part of S-I stage

LOx/Kerosene propellant rocket stage. 20 foot stretch of Saturn IB for use with UA1207 7 segment solid rocket strap-on units.

Status: Study 1966. Thrust: 8,241.76 kN (1,852,822 lbf). Gross mass: 505,953 kg (1,115,435 lb). Unfuelled mass: 48,545 kg (107,023 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 153 s. Height: 30.48 m (99.99 ft). Diameter: 6.52 m (21.39 ft). Span: 6.52 m (21.39 ft).

No Engines: 8.

Country: USA. Engines: H-1b. Launch Vehicles: Saturn INT-11, Saturn INT-13, Saturn INT-14. Propellants: Lox/Kerosene.

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