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Retired

Tsiklon-2A

Tsiklon-2A

🏭 Yuzhnoye Design Bureau🌐 Ukrainian📖 Wikipedia
🚀

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.

3.0 t
LEO Capacity
39.7 m
Height
8
Total Launches
87.5%
Success Rate

📷 Photo Gallery

🚀

📊 Specifications

📏Height
39.7 m
⭕Diameter
3 m
⚖️Launch Mass
182 kg
🛰️LEO Capacity
3,000 kg
🌍GTO Capacity
—
🗓️Maiden Flight
Oct 27, 1967
🚀Total Launches
8
✅Success Rate
88%
♻️Reusable
Expendable
🏭Manufacturer
Yuzhnoye Design Bureau
🌐Country
Ukrainian
📋Status
Retired