SICBM-2

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Model: SICBM-2. Gross Mass: 5,000 kg (11,000 lb). Thrust (vac): 267.000 kN (60,023 lbf). Burn time: 44 sec. Propellants: Solid. Diameter: 1.17 m (3.83 ft). Length: 3.20 m (10.40 ft). Country: USA. No Engines: 1. Motor: SICBM2. Status: Retired 1991. Used as: SICBM2. Release conditions: Aerojet. Used on Launch Vehicles: SICBM. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.