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Tsiklon-2A

Tsiklon family · built by Yuzhnoye Design Bureau · maiden flight 1967-10-27

Profile data last updated: 2026-08-29T15:37:07.354998+00:00 | 7531-10-17

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.

Specifications

39.7 mLength
3.0 mDiameter
182 tLaunch mass
2Stages
2366 kNLiftoff thrust

Payload Capacity

3000 kgTo LEO

Lifetime Launch Record

As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.

8Total launches
7Successful
1Failed
0Upcoming

Launches Tracked on This Site

8In our archive
87.5%Success rate
Oct 27, 1967 02:21 UTCEarliest tracked
Jan 25, 1969 11:14 UTCMost recent
MissionDateStatus
Tsiklon-2A | US-AO 5 Jan 25, 1969 11:14 UTC Failure
Tsiklon-2A | I2P 2 Nov 01, 1968 00:27 UTC Success
Tsiklon-2A | I2P 1 Oct 20, 1968 04:02 UTC Success
Tsiklon-2A | I2M 2 Oct 19, 1968 04:20 UTC Success
Tsiklon-2A | I2M 1 Apr 24, 1968 16:00 UTC Success
Tsiklon-2A | US-AO 4 Mar 22, 1968 09:30 UTC Success
Tsiklon-2A | US-AO 3 Dec 27, 1967 11:28 UTC Success
Tsiklon-2A | I2-BM (Kosmos-185) Oct 27, 1967 02:21 UTC Success

Wikipedia