Function | Carrier rocket |
---|---|
Manufacturer |
|
Country of origin | Ukraine |
Project cost | $304M (projection, $148M spaceport included)[1] |
Cost per launch | $45M[2]-$60M[1] (projections) |
Size | |
Height | 38.7 m (127.0 ft)[3] |
Diameter | 4.0 m (13 ft)[3] |
Stages | 2 |
Capacity | |
Payload to 200 km LEO (45.3°) | |
Mass | 5,000 kg (11,000 lb)[4] |
Payload to 500 km LEO | |
Mass | 4,600 kg (10,100 lb)[3] |
Payload to 1200 km LEO | |
Mass | 3,900 kg (8,600 lb)[3] |
Payload to 500 km polar LEO | |
Mass | 3,600 kg (7,900 lb)[3] |
Payload to 1200 km polar LEO | |
Mass | 3,000 kg (6,600 lb)[3] |
Payload to 500 km SSO | |
Mass | 3,450 kg (7,610 lb)[3] |
Payload to 1000 km SSO | |
Mass | 3,000 kg (6,600 lb)[3] |
Payload to 180×35,768 km) GTO (45.2°) | |
Mass | 910 kg (2,010 lb)[4] |
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[1] |
Total launches | 0 |
First flight | 2025 (planned)[5] |
First stage | |
Diameter | 3.9 m (13 ft)[3] |
Gross mass | 260,700 kg (575,000 lb)[3] |
Propellant mass | 224,800 kg (496,000 lb)[4] |
Powered by | 4 × RD-870 engines[4] |
Maximum thrust | Sea level: 3,130 kN (319 tf) Vacuum: 3,498 kN (356.7 tf)[3] |
Specific impulse | Sea level: 298 s (2.92 km/s) Vacuum: 332 s (3.26 km/s)[6] |
Burn time | 200 seconds[6] |
Propellant | LOX / RP-1 |
Second stage | |
Diameter | 3.98 m (13.1 ft)[3] |
Gross mass | 14,000 kg (31,000 lb)[3] |
Propellant mass | 10,700 kg (24,000 lb)[4] |
Powered by | 1 × RD-861K |
Maximum thrust | 77.63 kN (7.916 tf)[3] |
Specific impulse | 325 s (3.19 km/s) |
Burn time | 450 seconds |
Propellant | N2O4 / UDMH |
The Cyclone-4M is a Ukrainian carrier rocket which is being developed for commercial satellite launches.
cbc-20170314
was invoked but never defined (see the help page).Cyclone 4M will be available for $45M USD per launch.
ZakTsyklon4m
was invoked but never defined (see the help page).