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Tsyklon (Tsiklon)
Function Medium carrier rocket
Manufacturer Yuzhmash
Country of origin Soviet Union
Height 39.7 m (130.2 ft)
Diameter 3 m (9.8 ft)
Mass 182,000 kg (401,000 lb)
Stages 2
Payload to LEO 3,000 kg (6,600 lb)
Launch history
Status Retired
Launch sites Baikonur Cosmodrome, LC-90
Total launches 8
Successes 7
Failures 1
First flight 27 October 1967
Last flight 25 January 1969
Notable payloads IS-A/IS-P
First Stage - 8S671
Engines 1 RD-251
Thrust 2,640 kN (593,4090 lbf)
Specific impulse 301 sec
Burn time 120 s
Fuel N2O4/UDMH
Second Stage - 8S672
Engines 1 RD-252
Thrust 940 kN (211,410 lbf)
Specific impulse 317 s
Burn time 160 s
Fuel N2O4/UDMH

The Tsyklon (Циклон, "Cyclone", also known as Tsiklon), GRAU index 11K67, 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.

It made its maiden flight on 27 October 1967. The booster's design was kept secret and no images or film clips of the complete vehicle were released to the public until after the collapse of the Soviet Union in part because of being used exclusively for military payloads and also because it was derived from an actively serving missile system. After 1991, the plant where the R-36/Tsyklon were manufactured ended up in newly-independent Ukraine.

Tsyklon was designed by the Yuzhnoye Design Bureau and manufactured by Yuzhmash (both in Dnipropetrovsk, Ukraine). Control system was designed at NPO "Electropribor"[1] (Kharkiv, Ukraine). The last flown derivative, the Tsyklon-3 was retired in January 2009,[2] however another derivative, the Tsyklon-4, is still under development.


  • Derivatives 1
    • Tsyklon-2 1.1
    • Tsyklon-3 1.2
    • Tsyklon-4 1.3
  • See also 2
  • External links 3
  • References 4


Tsyklon-3 rocket launching a Meteor-3 weather observation satellite (Plesetsk, Aug. 15, 1991)

Two rockets were derived from the Tsyklon: the Tsyklon-2 and Tsyklon-3, known respectively as the SL-11 and SL-14 by the US DoD.[3]


The two stage Tsyklon-2 was first launched 6 August 1977 from the Baikonur Cosmodrome in Kazakhstan. The Tsyklon-2 was 39.7 metres (130 ft) long with a fueled mass of 182 tonnes. The Tsyklon-2 made its final flight in 2006.[2]


The Tsyklon-3, which featured a restartable third stage, first launched on 24 June 1977 from the Plesetsk Cosmodrome. The Tsyklon-3 is 39.27 metres (128.8 ft) long with a fueled mass of 186 to 190 tonnes. It was partially the result of an effort to reduce the number of Soviet launch vehicles in use, replacing the small R-12 derived Kosmos booster and some R-7 variants.

On 27 December 2000, a Tsyklon-3 failed in its attempt to carry six Russian satellites into orbit, plummeting to the earth. An electrical failure in the rocket's third stage was the suspected cause.

The Tsyklon-3 was retired after launching the Koronas-Foton satellite on 30 January 2009.[2]


The Tsyklon-4 is under development.

See also

External links

  • Yuzhnoye Design Office
  • Alcântara Cyclone Space


  1. ^ Krivonosov, Khartron: Computers for rocket guidance systems
  2. ^ a b c Barbosa, Rui C. (2009-01-30). "Russian Tsyklon-3 bows out with CORONAS launch". Retrieved 2009-01-30. 
  3. ^ Parsch, Andreas; Martynov, Aleksey V. (2008-07-02). "Designations of Soviet and Russian Military Aircraft and Missiles". Retrieved 2009-03-22. 

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