|
Baikonur LC142
|
|
Area 142 - Launch Site: Baikonur. Launch Pads: 1. Latitude: 46.0000 N. Longitude: 63.0000 E. R-36. - 1968 October 28 - Operational missile test Launch Vehicle: R-36. Failure. R-36 8K67
- 1968 December 4 - Operational missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1969 March 29 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1969 October 24 - RVSN Command operational test mission Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1969 November 4 - OS-67 No. 1L Test mission Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1969 December 12 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1970 January 21 - State trials missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1970 January 30 - State trials missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1970 February 18 - State trials missile test Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1970 April 11 - State trials missile test Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1970 April 27 - State trials missile test Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1970 September 12 - OS state trials flight Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1970 October 8 - Palma-4 Operational Test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1970 October 29 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1970 December 12 - RVSN Command operational test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1971 June 26 - Operational missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1971 September 9 - Combat training launch Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1971 December 2 - OS state trials flight Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1972 July 14 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1972 September 15 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1973 January 24 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1975 January 27 - Svilets Test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1975 February 27 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1975 June 25 - OS-67 Test mission Launch Vehicle: R-36. R-36 8K67 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 - 2007 except where otherwise noted.
|
|
|
|