Saturn IB-15

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Saturn IB-15

Part of S-I stage

LOx/Kerosene propellant rocket stage. 10 foot stretch of Saturn IB. Not found useful in any configuration except with Minuteman first-stage strap-ons to augment thrust.

Status: Study 1966. Thrust: 8,241.76 kN (1,852,822 lbf). Gross mass: 478,103 kg (1,054,036 lb). Unfuelled mass: 45,873 kg (101,132 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 144 s. Height: 27.43 m (89.99 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-15. Propellants: Lox/Kerosene.

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