Pershing-2

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Model: Pershing 1A-2. Gross Mass: 2,000 kg (4,400 lb). Thrust (vac): 85.000 kN (19,108 lbf). Burn time: 39 sec. Propellants: Solid. Diameter: 1.02 m (3.34 ft). Length: 2.70 m (8.80 ft). Country: USA. No Engines: 1. Motor: TX-175. Status: Retired 1983. First Flight: 1960. Last Flight: 1983. No Launched: 423. Used as: Pershing. Release conditions: Thiokol/Martin. Model: Pershing 2-2. Gross Mass: 2,600 kg (5,700 lb). Empty Mass: 350 kg (770 lb). Thrust (vac): 134.000 kN (30,124 lbf). Burn time: 46 sec. Propellants: Solid. Diameter: 1.02 m (3.34 ft). Length: 2.80 m (9.10 ft). Country: USA. No Engines: 1. Motor: Pershing 2 St2. Status: Retired 1988. First Flight: 1982. Last Flight: 1988. No Launched: 58. Used as: Pershing. Release conditions: Thiokol/Hercules. Used on Launch Vehicles: Pershing. 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.