Yuzhnoye Design Bureau

Tsiklon-2A

2A

Retired

Overview

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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.

Manufacturer

Yuzhnoye Design Bureau

Variant

2A

Alias

N/A

Maiden Flight

October 27, 1967

Technical Specifications

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39.7 m

Length

3 m

Diameter

0 t

Launch Mass

2366 kN

Liftoff Thrust

3000 kg

LEO Capacity

GTO Capacity

Launch Record

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8

Total Launches

7

Successful

1

Failed

87.5%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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