Tsyklon

Tsyklon (Tsiklon)
FunctionMedium carrier rocket
ManufacturerYuzhmash
Country of originSoviet Union
Size
Height39.7 m (130 ft)
Diameter3 m (9.8 ft)
Mass182 t (201 tons)
Stages2
Capacity
Payload to low Earth orbit
Mass3,000 kg (6,600 lb)
Launch history
StatusRetired
Launch sitesBaikonur Cosmodrome, LC-90
Total launches8
Success(es)7
Failure(s)1
First flight27 October 1967
Last flight25 January 1969
Type of passengers/cargoIS-A/IS-P
RORSAT
First stage – 8S671
Powered by1 RD-251
Maximum thrust2,640 kN (590,000 lbf)
Specific impulse301 s (2.95 km/s)
Burn time120 s
PropellantN2O4 / UDMH
Second stage – 8S672
Powered by1 RD-252
Maximum thrust940 kN (210,000 lbf) (211,410 lbf)
Specific impulse317 s (3.11 km/s)
Burn time160 s
PropellantN2O4 / UDMH

The Tsyklon (Ukrainian: 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] Another derivative, the Tsyklon-4, continued to be developed after the retirement of Tsyklon-3, but the Tsyklon-4 project was cancelled in 2015 due to financial concerns. Tsyklon-4 never reached launch pad. However, yet another derivative, the Cyclone-4M, a development of Tsyklon-4, continued to be developed and is still currently (2021) under development.

  1. ^ Krivonosov, Khartron: Computers for rocket guidance systems
  2. ^ Cite error: The named reference NSF-T3-retired was invoked but never defined (see the help page).

© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search