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Baikonur LC177
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Area 177 - Launch Site: Baikonur. Launch Pads: 1. Latitude: 46.0000 N. Longitude: 63.0000 E. MR-UR-100. - 1973 April 6 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1973 June 21 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1973 July 25 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1973 October 18 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1973 December 21 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 February 4 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 March 1 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 April 3 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 April 27 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 May 28 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 June 21 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 September 14 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 October 22 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 November 12 - Operational Test mission Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1974 December 17 - State trials missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1975 July 1 - 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 May 17 - State trials flight Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1976 June 29 - Joint flight trials launch Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1976 October 26 - Joint flight trials launch Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1976 December 30 - Joint flight trials launch Launch Vehicle: MR-UR-100. Failure.
- 1977 April 14 - Joint flight trials launch Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1977 July 30 - Joint flight trials launch Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1977 October 25 - Joint flight trials launch Launch Vehicle: MR-UR-100. MR-UR-100U 15A16 Apogee: 1,000 km (600 mi).
- 1977 December 29 - Joint flight trials launch Launch Vehicle: MR-UR-100. MR-UR-100U 15A16 Apogee: 1,000 km (600 mi).
- 1978 February 27 - Operational missile test Launch Vehicle: MR-UR-100. Apogee: 1,000 km (600 mi).
- 1978 March 31 - Joint flight trials launch Launch Vehicle: MR-UR-100. MR-UR-100U 15A16 Apogee: 1,000 km (600 mi).
- 1978 June 5 - Joint flight trials launch Launch Vehicle: MR-UR-100. MR-UR-100U 15A16 Apogee: 1,000 km (600 mi).
- 1978 September 12 - Joint flight trials launch Launch Vehicle: MR-UR-100. Failure. MR-UR-100U 15A16
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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