Tsyklon

The Tsyklon, GRAU index 11K67, was a Soviet-designed expendable launch system, primarily used to put Kosmos satellites into low Earth orbit in the late-1960s. 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. It was retired in 1969.

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1967 — 1969  Wikidata
Cyclone, Cyclone-2A, Tsiklon, Tsiklon-2A, Tsyklon-2A
mass 182000 kilogram, payload mass 3000 kilogram, height 39.7 metre, diameter 3 metre, 
two-stage-to-orbit, expendable launch vehicle, Pivdenmash, Soviet Union, 
Dong Fang Hong 2, Ekran, expendable launch vehicle, 1967, 1960s, [[Tsyklon|]], 

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Location: KML, Cluster Map, Maps,

Frameless

Type	Subtype	Date	Description	Notes	Source