SM-3

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Model: SM-3-3. Gross Mass: 100 kg (220 lb). Thrust (vac): 7.000 kN (1,574 lbf). Burn time: 15 sec. Propellants: Solid. Diameter: 0.33 m (1.08 ft). Length: 0.90 m (2.95 ft). Country: USA. No Engines: 1. Motor: SM3 TSRM. Status: Active. First Flight: 1992. Last Flight: 2007. No Launched: 21. Used as: SM3.TSRM. Other designations: SM-3 TSRM. Release conditions: Thiokol/TE. Used on Launch Vehicles: Standard-ER. Terrier. 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.