| SR118 |
home
topic index |
|
Model: Peacekeeper-1. Gross Mass: 53,400 kg (117,700 lb). Empty Mass: 4,400 kg (9,700 lb). Thrust (vac): 1,711.000 kN (384,648 lbf). Burn time: 79 sec. Propellants: Solid. Diameter: 2.35 m (7.70 ft). Length: 9.10 m (29.80 ft). Country: USA. No Engines: 1. Motor: TU-904. Status: Retired 2005. First Flight: 1994. Last Flight: 1998. No Launched: 4. Used as: MX. Other designations: SR118. Release conditions: Thiokol/UT.
Model: Taurus-0. Gross Mass: 48,960 kg (107,930 lb). Empty Mass: 4,300 kg (9,400 lb). Thrust (vac): 2,204.495 kN (495,590 lbf). Isp: 282 sec. Burn time: 56 sec. Propellants: Solid. Isp(sl): 250 sec. Diameter: 2.34 m (7.67 ft). Span: 2.34 m (7.67 ft). Length: 8.48 m (27.82 ft). Country: USA. No Engines: 1. Motor: Peacekeeper 1. Status: In production. Cost $ : 7.000 million. ICBM MX Peacekeeper ICBM 1st stage. Used for only first Taurus launch Model: SR118. Gross Mass: 53,020 kg (116,880 lb). Empty Mass: 4,211 kg (9,283 lb). Thrust (vac): 1,606.594 kN (361,177 lbf). Isp: 286 sec. Burn time: 83 sec. Propellants: Solid. Isp(sl): 229 sec. Diameter: 2.36 m (7.74 ft). Span: 2.36 m (7.74 ft). Length: 10.70 m (35.10 ft). Country: USA. No Engines: 1. Motor: Castor 120. Status: Out of production. Cost $ : 7.000 million. First Flight: 1995. Last Flight: 2004. No Launched: 25. Modification of Peackeeper ICBM first stage. Used on Launch Vehicles: 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. |