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SICBM2
Aerojet solid rocket engine. SICBM second stage.

AKA: SICBM-2. Status: Retired 1991. Thrust: 267.00 kN (60,023 lbf). Gross mass: 5,000 kg (11,000 lb). Burn time: 44 s. Height: 3.20 m (10.40 ft). Diameter: 1.17 m (3.83 ft).

Country: USA. Launch Vehicles: SICBM. Propellants: Solid. Stages: SICBM2. Agency: Aerojet.
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