| Baikonur LC175/2 |
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LC175/2 Chronology 1991 December 20 - 21:31 GMT - Launch Vehicle: UR-100N. Rokot-K No. 3L Grand Prix test Agency: VKS. Apogee: 1,000 km (600 mi). 1999 October 20 - Launch Vehicle: UR-100N. Operational missile test Agency: RVSN RF. Apogee: 1,000 km (600 mi). 2000 November 1 - 10:00 GMT - Launch Vehicle: UR-100N. UR-100NU 15A35 87 Operational missile test Agency: RVSN RF. Apogee: 1,000 km (600 mi). 2001 October 26 - 12:33 GMT - Launch Vehicle: UR-100N. Operational missile test Agency: RVSN RF. Apogee: 1,000 km (600 mi). 2003 December 5 - 06:00 GMT - Launch Vehicle: UR-100N. Payload Mockup Perigee: 454 km (282 mi). Apogee: 460 km (280 mi). Inclination: 67.10 deg. Period: 93.70 min. Originally reported as an ICBM test. A Reuters story, later confirmed, claimed it was the first orbital launch of the Strela version of the rocket. 2005 October 20 - 07:30 GMT - Launch Vehicle: UR-100N. OT Kura Agency: RVSN RF. Apogee: 1,000 km (600 mi). 2006 November 9 - 11:35 GMT - Launch Vehicle: UR-100N. Operational missile test Agency: RVSN RF. Apogee: 1,000 km (600 mi). 2007 October 29 - 09:00 GMT - Launch Vehicle: UR-100N. Operational test Agency: RVSN RF. Apogee: 1,000 km (600 mi). 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. |
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