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Jupiter (stage)
LOx/Kerosene propellant rocket stage. .

AKA: Jupiter. Status: Retired 1963. Thrust: 758.71 kN (170,565 lbf). Gross mass: 54,431 kg (119,999 lb). Unfuelled mass: 5,443 kg (11,999 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 182 s. Height: 18.28 m (59.97 ft). Diameter: 2.67 m (8.75 ft). Span: 2.67 m (8.75 ft).

Cost $ : 7.830 million.



Country: USA. Engines: S-3. Launch Vehicles: Jupiter IRBM, Juno II, Juno II (3). Propellants: Lox/Kerosene.

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