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 BureauStatus
RetiredFirst flight
27 Oct 1967Reusable
NoHeight
39.7 mDiameter
3 mLaunch mass
182 tLiftoff thrust
2,366 kNStages
2Launch cost
—Booster landings
—Links
WikipediaAbout
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
