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
- Launch cost
- —
- LEO capacity
- 3,000 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
8
Launches with a definitive outcome
Success rate
87.5%
7 of 8
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Tsiklon-2A | US-AO 5 — Failure
- Tsiklon-2A | I2P 2 — Success
- Tsiklon-2A | I2P 1 — Success
- Tsiklon-2A | I2M 2 — Success
- Tsiklon-2A | I2M 1 — Success