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Engine Model: SICBM2. Designer: Aerojet. Gross Mass: 5,000 kg (11,000 lb). Propellants: Solid. Thrust(vac): 267.000 kN (60,023 lbf). Burn time: 44 sec. Diameter: 1.17 m (3.83 ft). Length: 3.20 m (10.40 ft). Country: USA.
SICBM2 used on Rocket Stages
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