Single launch complex consisting of 2 launch pads.

• 1963 September 28 - State trials launch (1) Launch Vehicle: R-36. Failure. Exploded at launch - pad damaged.. R-36 8K67P G22500-02L

• 1963 December 3 - State trials missile test Launch Vehicle: R-36. R-36 8K67P G22500-04L Apogee: 1,000 km (600 mi).

• 1963 December 13 - State trials missile test Launch Vehicle: R-36. Failure. R-36 8K67P

• 1964 January 16 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 January 25 - State trials missile test Launch Vehicle: R-36. Failure.

• 1964 February 19 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 February 27 - State trials missile test Launch Vehicle: R-36. Failure.

• 1964 April 26 - State trials missile test Launch Vehicle: R-36. Failure.

• 1964 May 23 - State trials missile test Launch Vehicle: R-36. Failure.

• 1964 May 30 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 June 24 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 July 1 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 August 5 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 August 11 - State trials missile test Launch Vehicle: R-36. Failure.

• 1964 September 8 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 September 25 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi). Demonstration launch witnessed by Khrushchev.

• 1964 October 10 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 October 29 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1964 December 15 - State trials missile test Launch Vehicle: R-36. Apogee: 1,000 km (600 mi).

• 1965 January 30 - State trials missile test Launch Vehicle: R-36. R-36 8K67 Apogee: 1,000 km (600 mi).

• 1965 March 5 - First attempted launch of Fractional Orbital Bombardment System booster. Launch Vehicle: R-36-O. Second stage propellant leak led to a fire in the silo.. R-36O 8K69 A fire broke out during fuelling and the rocket exploded, seriously damaging the launch pad at Area 67.

• 1965 December 16 - OGCh No. 01L Launch Vehicle: R-36-O. R-36O 8K69 U22502 No. 1L Apogee: 200 km (120 mi). First suborbital test of the FOBS system. Impacted within specification CEP in target zone.

• 1966 February 5 - OGCh No. 02L Launch Vehicle: R-36-O. R-36O 8K69 U22502 No. 02L Apogee: 200 km (120 mi). Second suborbital test of the FOBS system.

• 1966 March 17 22:00 - OGCh No. 03L Launch Vehicle: R-36-O. R-36O 8K69 U22502 No. 03L Apogee: 0 km ( mi). Last of three suborbital flight tests of the FOBS system. The second stage of the booster placed the third stage and dummy warhead on a depressed trajectory with a range of 8500 km but an altitude of only 220 km (versus 800 to 1200 km for an optimum ballistic trajectory). The third stage than executed a 180 degree turn and its engines were fired to further brake the warhead to an impact on the Kamchatka peninsula. The second stage meanwhile continued on to reentry over the Pacific Ocean.

• 1966 May 20 19:00 - OGCh No. 04L Launch Vehicle: R-36-O. R-36O 8K69 U22502 No. 04L Possible suborbital test of FOBS booster or failed FOBS test. Not mentioned as FOBS-related in contemporary CIA assessments.

• 1971 October 22 - BI-2 Silo tests Test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1.00 km (0.60 mi).

• 1971 November 3 - BI-2 test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1.00 km (0.60 mi).

• 1971 December 7 - BI-2 test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 1.00 km (0.60 mi).

• 1971 December 10 - BI-2 test mission Launch Vehicle: MR-UR-100. Failure.

• 1971 December 29 - BI-3 test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 10 km (6 mi).

• 1972 February 21 - BI-2 test mission Launch Vehicle: MR-UR-100. Apogee: 1.00 km (0.60 mi).

• 1972 March 6 - BI-3 test mission Launch Vehicle: R-36M. Failure. Exploded over silo, destroying it.. R-36M 15A14 Apogee: 10 km (6 mi).

• 1972 March 21 - BI-2 test mission Launch Vehicle: MR-UR-100. Apogee: 1.00 km (0.60 mi).

• 1972 April 29 - BI-3 test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 10 km (6 mi).

• 1972 May 6 - BI-3 test mission Launch Vehicle: MR-UR-100. Apogee: 10 km (6 mi).

• 1972 May 24 - BI-3 test mission Launch Vehicle: MR-UR-100. Apogee: 10 km (6 mi).

• 1972 June 8 - BI-3 test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 10 km (6 mi).

• 1972 June 15 - BI-3 test mission Launch Vehicle: MR-UR-100. Apogee: 10 km (6 mi).

• 1972 August 18 - BI-3 test mission Launch Vehicle: R-36M. R-36M 15A14 Apogee: 10 km (6 mi).

• 1972 December 22 - BI-2 test mission Launch Vehicle: MR-UR-100. Apogee: 1.00 km (0.60 mi).