|Function||Medium carrier rocket|
|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)|
|Payload to LEO||3,000 kg (6,600 lb)|
|Launch sites||Baikonur Cosmodrome, LC-90|
|First flight||27 October 1967|
|Last flight||25 January 1969|
|First stage – 8S671|
|Thrust||2,640 kN (593,4090 lbf)|
|Specific impulse||301 sec|
|Burn time||120 s|
4 / UDMH
|Second stage – 8S672|
|Thrust||940 kN (211,410 lbf)|
|Specific impulse||317 s|
|Burn time||160 s|
4 / 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" (Kharkiv, Ukraine). The last flown derivative, the Tsyklon-3 was retired in January 2009, however another derivative, the Tsyklon-4, is still under development.
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.
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-4 was under development as an evolution of the Tsyklon-3, but was eventually abandoned due to economic and market concerns. A derivative, the Cyclone-4M, is under development as of 2017[update] for Canadian service provider Maritime Launch Services.
- Krivonosov, Khartron: Computers for rocket guidance systems
- Barbosa, Rui C. (2009-01-30). "Russian Tsyklon-3 bows out with CORONAS launch". NASASpaceflight.com. Retrieved 2009-01-30.
- Parsch, Andreas; Martynov, Aleksey V. (2008-07-02). "Designations of Soviet and Russian Military Aircraft and Missiles". www.designation-systems.net. Retrieved 2009-03-22.