Cyclone-4M
The Cyclone-4M is a Ukrainian carrier rocket which is being developed for commercial satellite launches.
| Function | Carrier rocket |
|---|---|
| Manufacturer |
|
| Country of origin | Ukraine |
| Project cost | $304M (projection, $148M spaceport included) |
| Cost per launch | $45M-$60M (projections) |
| Size | |
| Height | 38.7 m (127.0 ft) |
| Diameter | 4.0 m (13 ft) |
| Stages | 2 |
| Capacity | |
| Payload to 200 km LEO (45.3°) | |
| Mass | 5,000 kg (11,000 lb) |
| Payload to 500 km LEO | |
| Mass | 4,600 kg (10,100 lb) |
| Payload to 1200 km LEO | |
| Mass | 3,900 kg (8,600 lb) |
| Payload to 500 km polar LEO | |
| Mass | 3,600 kg (7,900 lb) |
| Payload to 1200 km polar LEO | |
| Mass | 3,000 kg (6,600 lb) |
| Payload to 500 km SSO | |
| Mass | 3,450 kg (7,610 lb) |
| Payload to 1000 km SSO | |
| Mass | 3,000 kg (6,600 lb) |
| Payload to 180×35,768 km) GTO (45.2°) | |
| Mass | 910 kg (2,010 lb) |
| Associated rockets | |
| Family | Zenit / Tsyklon |
| Comparable | Tsyklon-2, -3, -4, Dnepr, Soyuz-2, PSLV, Long March 4B/C |
| Launch history | |
| Status | In development |
| Launch sites | Canso, Nova Scotia, Canada |
| Total launches | 0 |
| First flight | 2025 (planned) |
| First stage | |
| Diameter | 3.9 m (13 ft) |
| Gross mass | 260,700 kg (575,000 lb) |
| Propellant mass | 224,800 kg (496,000 lb) |
| Powered by | 4 × RD-870 engines |
| Maximum thrust | Sea level: 3,130 kN (319 tf) Vacuum: 3,498 kN (356.7 tf) |
| Specific impulse | Sea level: 298 s (2.92 km/s) Vacuum: 332 s (3.26 km/s) |
| Burn time | 200 seconds |
| Propellant | LOX / RP-1 |
| Second stage | |
| Diameter | 3.98 m (13.1 ft) |
| Gross mass | 14,000 kg (31,000 lb) |
| Propellant mass | 10,700 kg (24,000 lb) |
| Powered by | 1 × RD-861K |
| Maximum thrust | 77.63 kN (7.916 tf) |
| Specific impulse | 325 s (3.19 km/s) |
| Burn time | 450 seconds |
| Propellant | N2O4 / UDMH |
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