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Tsiklon · Yuzhnoye Design Bureau

Tsiklon-2A

retired
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Specifications

Status
retired
Height
39.7 m
Diameter
3 m
Mass
182,000 kg
Stages
2
Payload to LEO
3,000 kg
First flight
1967-10-27
Total launches
8
Success / Fail
7 / 1

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.

Payloads it launched · 7

COSMOS 252
MEO
COSMOS 249
MEO
COSMOS 248
LEO
COSMOS 217
Payload
COSMOS 209
LEO
COSMOS 198
LEO
COSMOS 185
LEO