Baikonur LC173
Area 173 - Launch Site: Baikonur. Launch Pads: 1. Latitude: 46.0000 N. Longitude: 63.0000 E. MR-UR-100.

  • 1972 September 15 - BI-4 test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1972 November 3 - BI-4 test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1972 December 26 - BI-4 test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1973 March 12 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1973 June 5 - State trials missile test Launch Vehicle: MR-UR-100. Failure.
  • 1973 July 9 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1973 October 2 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1973 November 4 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1973 December 27 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1974 February 26 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1974 April 28 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1974 May 31 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1974 August 28 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1974 September 27 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1974 October 23 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1975 April 23 - Operational Test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1975 June 13 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1975 August 12 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1976 March 12 - State trials flight Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1976 June 26 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1976 August 12 - Operational Test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1976 December 16 - Joint flight trials launch Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1977 March 26 - Operational Test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1977 May 25 - K? operational test launch? Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1977 June 30 - Operational Test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1978 March 26 - Operational missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1978 June 5 - Operational missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
  • 1978 August 11 - Combat training launch Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
 
 
 
 
 
 
 
 
 
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