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Jupiter Cluster
Part of S-I stage Family
LOx/Kerosene propellant rocket stage. Masses estimated (cluster of four Jupiter IRBM stages).

Status: Study 1959. Thrust: 3,034.29 kN (682,134 lbf). Gross mass: 226,716 kg (499,823 lb). Unfuelled mass: 27,205 kg (59,976 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 172 s. Height: 18.28 m (59.97 ft). Diameter: 5.34 m (17.51 ft). Span: 5.34 m (17.51 ft).

No Engines: 4.



Country: USA. Engines: S-3. Launch Vehicles: Saturn A-2. Propellants: Lox/Kerosene.

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