Tsyklon

From Wikipedia, the free encyclopedia
Jump to: navigation, search
Tsyklon (Tsiklon)
Function Medium carrier rocket
Manufacturer Yuzhmash
Country of origin Soviet Union
Size
Height 39.7 m (130.2 ft)
Diameter 3 m (9.8 ft)
Mass 182,000 kg (401,000 lb)
Stages 2
Capacity
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
RORSAT
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.

Tsyklon was designed by the Yuzhnoe 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[edit]

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]

Tsyklon-2[edit]

The two stage Tsyklon-2 was first launched August 6, 1969, 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]

Tsyklon-3[edit]

The Tsyklon-3, which featured a restartable third stage, first launched on June 24, 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.

On December 27, 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]

Tsyklon-4[edit]

The Tsyklon-4 is under development.

See also[edit]

External links[edit]

References[edit]

  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". NASASpaceflight.com. Retrieved 2009-01-30. 
  3. ^ 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.