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Cyclone
The Cyclone-4 space launch system is created in cooperation between Yuzhnoye SDO, Yuzhny Machine-Building Plant, NPP Kharotron-Arkos, Ukraine, INFRAERO, Brazil, and FGUP Design Bureau of Transport Machinery, Russia. The System will provide commercial launch services into LEO, SSO, and GTO. The newest and the most powerful rocket in the Cyclone family, the Cyclone-4 is based on the flight-proven Cyclone-3 rocket.
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| Title | Value |
| Number of stages | 3 |
| Launch weight (w/o payload), tons | 195 |
| Propellant components | |
| - oxidizer | NTO |
| - fuel | UDMH |
| Propellant margin, tons | |
| - Stage 1 | 121 |
| - Stage 2 | 49 |
| - Stage 3 | 9 |
| Vacuum thrust, t | |
| - Stage 1 | 270 |
| - Stage 2 | 96 |
| - Stage 3 | 7,9 |
| Maximum axial overload, g | not higher than 6.8 |
| Inclination range (for the Alcantara launch site), deg | 2.3 to 100 |
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