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Space · launch vehicle

Tsiklon-2A

OKB-586 RETIRED
At a glance
Launches
8
Success rate
87.5%
7 ok · 1 failed
Payload to LEO
3,000 kg
Payload to GTO
—
Manufacturer
Yuzhnoye Design Bureau
Status
Retired
First flight
27 Oct 1967
Reusable
No
Height
39.7 m
Diameter
3 m
Launch mass
182 t
Liftoff thrust
2,366 kN
Stages
2
Launch cost
—
Booster landings
—
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.