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Baikonur LC161
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Area 161 - Launch Site: Baikonur. Launch Pads: 1. Latitude: 46.0380 N. Longitude: 63.0770 E. R-36, R-36-O. - 1967 March 22 - OGCh Launch Vehicle: R-36-O. Failure. R-36O 8K69 N22500 No. 08L
- 1967 May 17 16:05 - Cosmos 160 Launch Vehicle: R-36-O. R-36O 8K69 Ya22500 No. 09L Apogee: 177 km (109 mi). Fractional Orbital Bombardment system test.
- 1967 July 31 16:45 - Cosmos 170 Launch Vehicle: R-36-O. R-36O 8K69 Ya22500 No. 12L Apogee: 199 km (123 mi). Fractional Orbital Bombardment system test.
- 1967 September 19 14:45 - Cosmos 178 Launch Vehicle: R-36-O. R-36O 8K69 Ya22500 No. 14L Apogee: 258 km (160 mi). Fractional Orbital Bombardment system test.
- 1967 October 18 13:30 - Cosmos 183 Launch Vehicle: R-36-O. R-36O 8K69 Ya22500 No. 16L Apogee: 306 km (190 mi). Fractional Orbital Bombardment system test.
- 1968 May 28 - OGCh Launch Vehicle: R-36-O. R-36O 8K69 Ya22501m No. 19L Probable suborbital test of Fractional Orbital Bombardment System.
- 1968 October 2 13:35 - Cosmos 244 Launch Vehicle: R-36-O. R-36O 8K69 V22501 No. 10T Apogee: 158 km (98 mi). Fractional Orbital Bombardment System test.
- 1969 April 18 - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1969 June 27 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1969 October 23 - RVSN Command operational test mission Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1969 Dec 19? - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1970 January 17 - 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 9 - State trials missile test Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1970 February 20 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1970 March 29 - State trials missile test Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1970 April 15 - State trials missile test Launch Vehicle: R-36. R-36 8K67P Apogee: 1,000 km (600 mi).
- 1970 October 12 - Palma-4 Operational Test mission Launch Vehicle: R-36. Failure. R-36 8K67
- 1970 December 11 - RVSN Command operational test mission Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1971 February 17 - Operational missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).
- 1971 October 2 - Combat training launch Launch Vehicle: R-36. R-36 8K67M Apogee: 1,000 km (600 mi).
- 1972 April 12 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1972 May 26 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1972 August 24 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1973 March 9 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1973 May 23 - State trials missile test Launch Vehicle: R-36. R-36 8K67MA Apogee: 1,000 km (600 mi).
- 1973 July 21 - State trials missile test Launch Vehicle: R-36. Failure. R-36 8K67PM
- 1973 October 8 - State trials missile test Launch Vehicle: R-36. Failure. R-36 8K67PM
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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