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Jupiter C-2
Part of Castor engine
Aerojet solid rocket stage. 80.00 kN (17,985 lbf) thrust. Mass 500 kg (1,102 lb).

AKA: 11xBaby Sergeant. Status: S. Thrust: 80.00 kN (17,984 lbf). Gross mass: 500 kg (1,100 lb). Unfuelled mass: 223 kg (491 lb). Burn time: 6.00 s. Height: 1.20 m (3.90 ft). Diameter: 0.89 m (2.91 ft).

No Engines: 11.



Country: USA. Launch Vehicles: Juno II (3). Propellants: Solid. Agency: JPL.

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