Baikonur PU31
PU31 (Area unknown) - Launch Site: Baikonur. Launch Pads: 1. Latitude: 46.0000 N. Longitude: 63.0000 E. R-36.

  • 1965 October 1 - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1965 November 2 - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1965 December 26 - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1966 March 30 - SLI K Operational Test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1966 April 2 - SLI K Operational Test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1966 May 29 - State trials launch (41) Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).
  • 1966 June 30 - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1966 September 27 - Operational missile test Launch Vehicle: R-36. Failure. R-36 8K67
  • 1966 October 23 - Operational Test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1967 June 6 - 8F765 warhead state trials flight Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1967 June 27 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1967 September 4 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1967 October 1 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1968 February 29 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1968 June 6 - Special Test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
  • 1968 July 16 - Operational missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
  • 1968 August 14 - Operational missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
 
 
 
 
 
 
 
 
 
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