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Tsiklon-2A

Tsiklon familyYuzhnoye Design BureauRetired

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.

Specifications

Thrust
2,366 kN
Height
39.7 m
Diameter
3 m
Launch mass
182 t
Stages
2
LEO capacity
3,000 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

8flightswith a definitive outcome
87.5%success rate7 of 8
0success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 8

All 8 flights