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Saturn IB stage
Part of S-I stage Family
LOx/Kerosene propellant rocket stage. Configuration as flown, Saturn IB.

AKA: Saturn IB. Status: Flown 1965. Thrust: 8,241.76 kN (1,852,822 lbf). Gross mass: 440,648 kg (971,462 lb). Unfuelled mass: 41,594 kg (91,699 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 155 s. Height: 24.48 m (80.31 ft). Diameter: 6.52 m (21.39 ft). Span: 6.52 m (21.39 ft).

Cost $ : 43.500 million. No Engines: 8.



Country: USA. Engines: H-1b. Launch Vehicles: Saturn B-1, Saturn A-2, Saturn IB, Saturn IB-C, Saturn IB-CE, Saturn IB-D, Uprated Saturn I. Propellants: Lox/Kerosene.

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