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Baikonur LC109
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Area 109 - Launch Site: Baikonur. Launch Pads: 1. Latitude: 45.9440 N. Longitude: 63.4420 E. R-36M, R-36M2. - 1974 July 4 - State trials missile test Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1974 August 30 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1974 October 23 - State trials missile test Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1974 December 25 - State trials missile test Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1975 February 26 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1975 June 7 - SLI? Operational Test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1975 August 26 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1976 September 3 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1977 May 17 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1977 November 29 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1977 December 30 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1978 February 11 - Missile accuracy test launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1978 June 14 - Joint flight trials launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1980 March 6 - DP Test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1980 July 4 - DP Test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1982 July 15 - DP Test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1982 December 23 - DP Test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1983 July 14 - Joint flight trials launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1983 October 11 - Joint flight trials launch Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1,000 km (600 mi).
- 1999 April 21 04:59 - UoSAT-12 Launch Vehicle: R-36M2. Dnepr 6703542509 Apogee: 654 km (406 mi). First launch of Russia's Dnepr launch vehicle, a converted R-36M2 ICBM. The Dnepr was launched from a silo. The third stage maneuvring bus (used on the ICBM for dispensing multiple warheads) placed UoSAT-12 into a 638 km x 652 km x 64.6 deg orbit. The third stage separated from the payload at 05:13 GMT and then made a burn into a 599 km x 1403 km x 64.6 deg orbit. UoSAT-12 was the first test of the Minibus platform, at 325 kg a larger spacecraft than earlier 50 kg Surrey UoSATs. It carried a mobile radio experiment (MERLION), a GPS receiver, and imaging cameras.
- 2000 September 26 10:05 - Tiungsat-1 Launch Vehicle: R-36M2. Dnepr 1 Apogee: 658 km (409 mi). Launch delayed from August 25/26. Customer: Astonautic Technology (M) SDN. BHD. Malaysia's first microsatellite built through a technology transfer programme with Surrey Satellite Technology Ltd Carried multi-spectral Earth imaging CCD cameras, meteorological Earth imaging CCD camera, digital store and forward communications, cosmic-ray energy deposition experiment (CEDEX)
- 2007 June 15 02:14 - TerraSAR-X Launch Vehicle: R-36M2. Dnepr Apogee: 512 km (318 mi). Scientific/commercial surveillance satellite. equipped with an X-band synthetic aperture radar with 1 meter resolution
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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