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SICBM-1
Part of Castor 4 Family
Thiokol solid rocket engine.

AKA: SICBM. Status: Retired 1991. Number: 1 . Thrust: 979.00 kN (220,087 lbf). Gross mass: 11,600 kg (25,500 lb). Burn time: 40 s. Height: 7.50 m (24.60 ft). Diameter: 1.17 m (3.83 ft).



Country: USA. Launch Vehicles: SICBM. Propellants: Solid. Stages: SICBM-1. Agency: Thiokol.

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