Baikonur LC67/21
Site · Russia
Original archive entry. The text, images and links below are kept as they were written.
Tsiklon, R-36M, MR-UR-100 launch complex. 67L.
Related
- Country
- Russia
- Spacecraft
- OGCh
- Launch Vehicles
- R-36 8K67, R-36O 8K69, R-36M 15A14, MR-UR-100
- Launch Sites
- Baikonur
Chronology
27 events
1963 September 28
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67. FAILURE: Failure.1963 December 3
08:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67.1963 December 13
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67. FAILURE: Failure.1964 January 16
04:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67.1964 January 25
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67. FAILURE: Failure.1964 February 19
15:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67.1964 February 27
02:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67. FAILURE: Failure.1964 May 23
04:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36 8K67. FAILURE: Failure.1965 March 5
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36O 8K69. FAILURE: Second stage propellant leak led to a fire in the silo.. Failed Stage: 2.- First attempted launch of Fractional Orbital Bombardment System booster. - . Mass: 1,700 kg (3,700 lb). Nation: Russia. Agency: RVSN. Spacecraft: OGCh. COSPAR: F19650305. A fire broke out during fuelling and the rocket exploded, seriously damaging the launch pad at Area 67..
1965 December 16
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36O 8K69.- OGCh No. 01L - . Mass: 1,700 kg (3,700 lb). Nation: Russia. Agency: RVSN. Spacecraft: OGCh. COSPAR: U651216A. Apogee: 200 km (120 mi). First suborbital test of the FOBS system. Impacted within specification CEP in target zone..
1966 February 5
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36O 8K69.- OGCh No. 02L - . Mass: 1,700 kg (3,700 lb). Nation: Russia. Agency: RVSN. Spacecraft: OGCh. COSPAR: U660205A. Apogee: 200 km (120 mi). Second suborbital test of the FOBS system..
1966 March 17
22:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36. Launch Vehicle: R-36O 8K69.- OGCh No. 03L - .
Mass: 1,700 kg (3,700 lb). Nation: Russia.
Agency: RVSN.
Spacecraft: OGCh.
COSPAR: U660316A. Apogee: 0 km (0 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.
1971 October 22
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36M. Launch Vehicle: R-36M 15A14.1971 November 3
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36M. Launch Vehicle: R-36M 15A14.1971 December 7
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: R-36M. Launch Vehicle: R-36M 15A14.1971 December 10
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. Launch Vehicle: MR-UR-100. FAILURE: Failure.1971 December 22
Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. Launch Vehicle: MR-UR-100.- BI-2 - . Nation: Kazakhstan. Agency: RVSN. Apogee: 1.00 km (0.60 mi).