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Tsiklon-2A

RETIRED
UKR flag — Tsiklon-2A UKR Wikipedia external-link-icon-img
Tsiklon-2A launch vehicle, operated by Yuzhnoye Design Bureau

Built & Operated By

Yuzhnoye Design Bureau

Commercial · founded 1951

Family

Tsiklon

variant 2A

Maiden Flight

27 OCT 1967

About

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.

Vehicle Specifications

Height

39.7 m

Diameter

3 m

Launch Mass

182 T

Thrust

2,366 kN

Stages

2

Configuration

Expendable

Launch Record

Total Launches

8

Successful

7

Failed

1

Performance

To LEO

3,000 kg

Version: 2.21.8

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