Super-Jupiter stage (original) (raw)

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Super-Jupiter stage

Part of S-I stage

E-1 Engine

E-1 Engine
Credit: © Mark Wade

LOx/Kerosene propellant rocket stage. Earliest member of what would become the Saturn family. Masses estimated.

AKA: Super-Jupiter. Status: Study 1957. Thrust: 7,538.30 kN (1,694,677 lbf). Gross mass: 317,600 kg (700,100 lb). Unfuelled mass: 19,600 kg (43,200 lb). Specific impulse: 290 s. Specific impulse sea level: 260 s. Burn time: 110 s. Height: 22.00 m (72.00 ft). Diameter: 5.23 m (17.15 ft). Span: 5.23 m (17.15 ft).

No Engines: 4.

Country: USA. Engines: E-1. Launch Vehicles: Super-Jupiter. Propellants: Lox/Kerosene.

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