Tsiklon-2A
Yuzhnoye Design Bureau
Details
Height
39.7 m
Diameter
3 m
GTO
Unknown
LEO
3,000 kg
Thrust at Liftoff
2,366 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
October 27, 1967
Description
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.