Tsiklon-2A

Built & Operated By
Yuzhnoye Design Bureau
Commercial · founded 1951
Family
Tsiklon
variant 2A
Maiden Flight
27 OCT 1967
About
The Tsyklon was a Soviet-designed expendable launch system, primarily used to put Cosmos satellites into low Earth orbit. It is based on the R-36 intercontinental ballistic missile designed by Mikhail Yangel and made eight launches, with seven successes and one failure. All of its launches were conducted from LC-90 at the Baikonur Cosmodrome. It is sometimes designated Tsyklon-2A, not to be confused with the later Tsyklon-2 rocket. It was introduced in 1967 and was derived from the R-36 ICBM (NATO designation SS-9 Scarp). It was retired in 1969.
Vehicle Specifications
Height
39.7 m
Diameter
3 m
Launch Mass
182 T
Thrust
2,366 kN
Stages
2
Configuration
Expendable
Launch Record
Total Launches
8
Successful
7
Failed
1
Performance
To LEO
3,000 kg