Saturn S-IB-A

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Saturn S-IB-A

Part of S-I stage

LOx/Kerosene propellant rocket stage. Douglas Studies, 1965: S-1B with 225 k lbf H-1's.

Status: Study 1965. Thrust: 9,045.60 kN (2,033,532 lbf). Gross mass: 448,600 kg (988,900 lb). Unfuelled mass: 41,600 kg (91,700 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 128 s. Height: 24.48 m (80.31 ft). Diameter: 6.52 m (21.39 ft). Span: 6.52 m (21.39 ft).

No Engines: 8.

Country: USA. Engines: H-1c. Launch Vehicles: Saturn IB-A, Saturn IB-B. Propellants: Lox/Kerosene.

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