 | |
| 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 kmLEO (45.3°) | |
| Mass | 5,000 kg (11,000 lb)[4] |
| Payload to 500 kmLEO | |
| Mass | 4,600 kg (10,100 lb)[3] |
| Payload to 1200 kmLEO | |
| Mass | 3,900 kg (8,600 lb)[3] |
| Payload to 500 kmpolarLEO | |
| Mass | 3,600 kg (7,900 lb)[3] |
| Payload to 1200 kmpolarLEO | |
| Mass | 3,000 kg (6,600 lb)[3] |
| Payload to 500 kmSSO | |
| Mass | 3,450 kg (7,610 lb)[3] |
| Payload to 1000 kmSSO | |
| Mass | 3,000 kg (6,600 lb)[3] |
| Payload to180×35,768 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 |
TheCyclone-4M is aUkrainiancarrier rocket which is being developed for commercial satellite launches.
The Cyclone-4M is derived from theTsyklon-4, which started its life as an all-hypergolic three-stage-to-orbit expendable launch vehicle planned for launch from a proposed site at theAlcântara Launch Center in Brazil. However, Brazil backed out of the partnership with Ukraine in 2015, citing concerns over the project budget, the ongoing financial situation in both countries, and the future of the commercial launch market.[7] In March 2017, Canadian companyMaritime Launch Services announced plans to begin launching a modified version, the Cyclone-4M, which features aZenit-derivedLOX / RP-1 first stage in place of the originally plannedR-36 ICBM-based first- and second-stage.
In November 2021, Maritime Launch Services CEO Stephen Matier stated thatNanoracks was to be the first client to fly a payload on the Cyclone-4M.[8]
This new first-stage design would use four kerolox engines derived from theRD-120 used on the second stage of the Zenit. The standard RD-120, however, while manufactured in Ukraine, uses a number of Russian-made components which would have to be replaced with Ukrainian-made equivalents. It is also planned to fit each of these engines with a gimballing mechanism for steering (in the Zenit second stage the RD-120 is fixed to the frame while anRD-8 four-nozzle vernier engine takes care of the steering).[4] The second stage completed qualification tests in October 2019.[9]
Cyclone-4M was planned to launch from a site inCanso,Nova Scotia.[10] Construction was originally scheduled to begin in 2018.[1][11] However, repeated delays pushed the start of construction to September 2022 for the access road, and March 2023 for work to start on the first launch pad.[12] MLS completed construction on the first launch pad in 2024. However, because of the 2022Russian invasion of Ukraine, and the uncertainty it caused, MLS terminated the agreement to launch Cyclone from Spaceport Nova Scotia by third quarter 2024.[13]
Cyclone 4M will be available for $45M USD per launch.
 Ukrainian launch vehicles | ||
|---|---|---|
| Cyclone (Tsyklon) |  | |
| Zenit | ||
| Mayak | ||
| Dnipro (Dnepr) | ||
| International projects | ||
