For the first time in rocket engineering, a space launch system featured a fully automated launch operations cycle, which was the result of large amount of research and development work. The Cyclone-2 is a lightweight launch vehicle for delivering payloads into low circular and elliptical Earth orbits, including open orbits.
Yuzhnoye designed the Cyclone-2 based on the 8K69 missile. The specific characteristics of the Cyclone-2 are high reliability and an automated-launch capability at any time of day in any weather.
The first launch of the Cyclone-2 occurred on August 6, 1969 from Baikonur Cosmodrome in Kazakhstan; the last one, in June 2006. The Cyclone-2 holds a unique record in rocketry: all 106 launches of this launch vehicle were successful.
Basic Specifications
|
Number of stages |
2 |
|
Dimensions, mm: Length Stage diameter Payload fairing diameter |
39 000 3 000 2 200 |
|
Launch weight (for a 3.2-ton payload), tons |
183 |
|
Propellants: Oxidizer Fuel |
NTO UDMH |
|
Vacuum thrust, tnf: Stage 1 Stage 2 |
303,2 101,5 |
|
Payload capability, tons |
1,5-5 |

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