Saturn S-1B-4

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Saturn S-1B-4

Part of S-I stage

LOx/Kerosene propellant rocket stage. Chrysler Studies, 1966: S-1B with 4 H-1's for use with Titan UA1205 strap-ons.

Status: Study 1966. Thrust: 4,120.70 kN (926,370 lbf). Gross mass: 444,700 kg (980,300 lb). Unfuelled mass: 37,600 kg (82,800 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 282 s. Height: 24.48 m (80.31 ft). Diameter: 6.52 m (21.39 ft). Span: 6.52 m (21.39 ft).

No Engines: 4.

Country: USA. Engines: H-1b. Launch Vehicles: Saturn INT-12. Propellants: Lox/Kerosene.

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