Vega C
Adapted from Wikipedia · Adventurer experience
Vega C, or Vega Consolidation, is a European rocket used to launch small satellites into space. It was made by Avio and is an improved version of the original Vega rocket. Vega C can carry heavier satellites and is used for science missions and watching Earth from space.
The European Space Agency approved Vega C in December 2014. It was first run by Arianespace but will soon be managed by Avio for selling launches. Vega C can send a 2,300-kilogram spacecraft into a 700-kilometre orbit, which is much more than the original Vega.
Vega C is named after Vega, the brightest star in the constellation Lyra. It has three solid fuel stages and one liquid fuel stage, so it does not need extra boosters. Companies from many countries helped build it, including Belgium, France, the Netherlands, Spain, Switzerland, and Ukraine.
The first launch of Vega C on 13 July 2022 worked well, but the second launch on 21 December 2022 failed because of a problem with the second stage. After this, the next launch was delayed until late 2024 to fix the problem.
Specifications
Building the Vega C rocket is a team effort from many European countries. Avio from Italy leads the project and builds some parts of the rocket. Europropulsion, a partnership between Avio and ArianeGroup, makes the first stage. Airbus Netherlands B.V. from the Netherlands builds the part that connects the first and second stages. The Italian Aerospace Research Centre makes the part between the second and third stages. Beyond Gravity from Switzerland builds the protective cover for the satellite and the onboard computer that guides the rocket. SABCA from Belgium builds the systems that control the rocket’s direction.
The Vega C can carry a heavy load into space. It can lift about 2,300 kilograms to a high orbit, much more than older versions. Because it carries more, the protective cover for the satellite had to be made bigger. The new cover is wider and taller than the old one, giving almost twice as much space inside.
| Stages | Stage 1 P120C | Stage 2 Zefiro 40 | Stage 3 Zefiro 9 | Stage 4 AVUM+ |
|---|---|---|---|---|
| Height | 13.38 m (43 ft 11 in) | 8.07 m (26 ft 6 in) | 4.12 m (13 ft 6 in) | 2.04 m (6 ft 8 in) |
| Diameter | 3.4 m (11 ft 2 in) | 2.4 m (7 ft 10 in) | 1.9 m (6 ft 3 in) | 2.18 m (7 ft 2 in) |
| Propellant type | Solid (HTPB/AP/Al) | Solid (HTPB/AP/Al) | Solid (HTPB/AP/Al) | Liquid (UDMH/N2O4) |
| Gross mass | 155,027 kg (341,776 lb) | 40,477 kg (89,237 lb) | 12,000 kg (26,000 lb) | 1,436 kg (3,166 lb) |
| Propellant mass | 141,634 kg (312,250 lb) | 36,239 kg (79,893 lb) | 10,567 kg (23,296 lb) | 740 kg (1,630 lb) |
| Average thrust | 4,323 kN (972,000 lbf) | 1,304 kN (293,000 lbf) | 317 kN (71,000 lbf) | 2.45 kN (550 lbf) |
| Burn time (sec.) | 135.7 | 92.9 | 119.6 | 924.8 (up to 5 burns) |
| Specific impulse | 279 s (2.74 km/s) | 293.5 s (2.878 km/s) | 295.9 s (2.902 km/s) | 315.8 s (3.097 km/s) |
| Event | Time (sec.) | Altitude km (mi) | Velocity m/s (ft/s) |
|---|---|---|---|
| P120C ignition & lift-off | 0 | 0 | 0 |
| P120C burn-out & separation, Zefiro 40 ignition | 142 | 60 (37) | 1,885 (6,180) |
| Zefiro 40 burn-out & separation | 245 | 121 (75) | 4,555 (14,940) |
| Zefiro 9 ignition | 249 | 123 (76) | 4,550 (14,900) |
| Fairing jettisoning | 254 | 126 (78) | 4,600 (15,000) |
| Zefiro 9 separation | 417 | 190 (120) | 7,564 (24,820) |
| AVUM+ 1st ignition | 448 | 199 (124) | 7,553 (24,780) |
| AVUM+ 1st cut-off | 1,090 | 300 (190) | 7,885 (25,870) |
| AVUM+ 2nd ignition | 3,151 | 619 (385) | 7,533 (24,710) |
| AVUM+ 2nd cut-off | 3,287 | 623 (387) | 7,631 (25,040) |
| Spacecraft separation | 3,427 | 626 (389) | 7,627 (25,020) |
Future
The Vega C+ is an upgrade to the Vega C rocket. It will use a bigger first stage called the P160C instead of the P120C. This makes the rocket taller and lets it carry more weight into space. Other improvements include a better navigation system, a larger cover for the satellite, and easier production. The first Vega C+ flight is planned for 2028.
The Vega E, also called Vega Evolution, will build on the Vega C+. It will use new fuel called liquid oxygen and liquid methane. This should let the rocket carry more weight and launch several satellites into different orbits in one flight. Tests for the new engine were successful in 2022, and the first Vega E flight is expected in 2027. A special launch site is being prepared for these flights.
After 2032, the Vega Next rocket is planned. It will use an even bigger engine, which could help make the first stage of the rocket reusable.
List of launches
See also: List of Vega launches
Launch history
Future launches
This section is transcluded from List of Vega launches.
| Flight | Date / time (UTC) | Rocket | Launch site | Payload | Payload mass | Orbit | Customers | Launch outcome |
|---|---|---|---|---|---|---|---|---|
| VV21 | 13 July 2022 13:13:17 | Vega C | ELV | 350 kg (770 lb) | MEO | Success | ||
| First flight of Vega C | ||||||||
| VV22 | 21 December 2022 01:47:31 | Vega C | ELV | Pléiades Neo 5 & 6 | 1,977 kg (4,359 lb) | SSO | Airbus Defence and Space | Failure |
| Earth observation satellites. Failure due to loss of pressure of the Zefiro 40 second stage. | ||||||||
| VV25 | 5 December 2024 21:20:33 | Vega C | ELV | Sentinel-1C | 2,300 kg (5,100 lb) | SSO | ESA | Success |
| Third Sentinel-1 satellite. Return to flight for Vega C following the VV22 launch failure. | ||||||||
| VV26 | 29 April 2025 09:15 | Vega C | ELV | BIOMASS | 1,131 kg (2,493 lb) | SSO | ESA | Success |
| Earth observation satellite. Part of the Living Planet Programme. | ||||||||
| VV27 | 26 July 2025 02:03 | Vega C | ELV | CO3D × 4 + MicroCarb | 1,320 kg (2,910 lb) | SSO | CNES | Success |
| The CO3D (Constellation Optique en 3D) is an Earth observation satellite constellation providing daily 50 cm (20 in) resolution stereo imagery for global 3D mapping; MicroCarb is a microsatellite measuring atmospheric CO₂ with 1 ppm accuracy to track global sources and sinks. | ||||||||
| VV28 | 1 December 2025 17:21 | Vega C | ELV | KOMPSAT-7 (Arirang-7) | 1,810 kg (3,990 lb) | SSO | KARI | Success |
| Earth observation satellite. | ||||||||
| Date / time (UTC) | Rocket | Launch site | Payload | Orbit |
|---|---|---|---|---|
| 19 May 2026 03:52 | Vega C | ELV | SMILE | HEO |
| Solar wind Magnetosphere Ionosphere Link Explorer (SMILE) is a joint Chinese-European Earth observation satellite designed to study the magnetosphere with soft X-rays and UV. First launch to be operated by Avio without Arianespace. | ||||
| September 2026 | Vega C | ELV | Sentinel-3C | SSO |
| Third Sentinel-3 Earth observation satellite. Secondary payload is ESA's Fluorescence Explorer (FLEX) mission. | ||||
| November 2026 | Vega C | ELV | KOMPSAT-6 (Arirang-6) | SSO |
| Earth observation satellite. PLATiNO-1 as secondary payload. | ||||
| 2026 | Vega C | ELV | IRIDE × ? | LEO |
| First launch for the Italian IRIDE Earth observation satellite constellation. | ||||
| Q1 2027 | Vega C | ELV | Eagle-1 | LEO |
| Demonstrator satellite for the first European sovereign space-based quantum key distribution system. | ||||
| 1H 2027 | Vega C | ELV | CSG-4 | SSO |
| Fourth COSMO-SkyMed 2nd Generation satellite. | ||||
| November 2027 | Vega C | ELV | CO2M-A (Sentinel-7A) | SSO |
| Copernicus Anthropogenic Carbon Dioxide Monitoring. Part of the Copernicus Programme. | ||||
| Q4 2027 | Vega C | ELV | ALTIUS, FLEX | SSO |
| ALTIUS is an ozone observation satellite. FLEX is an Earth observation satellite of the Living Planet Programme. | ||||
| Q4 2027 | Vega C | ELV | FORUM | SSO |
| Earth observation satellite. Part of the Living Planet Programme. | ||||
| March 2028 | Vega C | ELV | CO2M-B (Sentinel-7B) | SSO |
| Copernicus Anthropogenic Carbon Dioxide Monitoring. Part of the Copernicus Programme. | ||||
| Q1 2028 | Vega C+ | ELV | Space Rider | LEO |
| Technology demonstration | ||||
| Q4 2028 | Vega C | ELV | CRISTAL (Sentinel-9) | Polar |
| Copernicus Polar Ice and Snow Topography Altimeter. Part of the Copernicus Programme. | ||||
| 2028 | Vega C | ELV | CHIME-A (Sentinel-10) | SSO |
| Copernicus Hyperspectral Imaging Mission. Part of the Copernicus Programme. | ||||
| 2028 | Vega C | ELV | Sentinel-3D | SSO |
| Fourth Sentinel-3 Earth observation satellite. | ||||
| 2028 | Vega C | ELV | Sentinel-2D | LEO |
| Fourth Sentinel-2 Earth observation satellite. | ||||
| Q3 2029 | Vega C | ELV | CIMR-A (Sentinel-11A) | SSO |
| Copernicus Imaging Microwave Radiometer. Part of the Copernicus Programme. | ||||
| 2029 | Vega C | ELV | ClearSpace-1 | LEO |
| Space debris removal demo. | ||||
| 2029 | Vega C | ELV | LSTM (Sentinel-8) | SSO |
| Copernicus Land Surface Temperature Monitoring. Part of the Copernicus Programme. | ||||
| 2029 | Vega C | ELV | Harmony | LEO |
| Earth Explorer 10 Mission. | ||||
| 2029 | Vega C | ELV | SBG-TIR | LEO |
| Surface Biology and Geology-Thermal Infrared. | ||||
| 2030 | Vega C | ELV | CHIME-B (Sentinel-10) | SSO |
| Copernicus Hyperspectral Imaging Mission. Part of the Copernicus Programme. | ||||
| TBD | Vega C | ELV | IRIDE × ? | LEO |
| Second launch for the Italian IRIDE Earth observation satellite constellation. | ||||
| TBD | Vega C | ELV | SHALOM | SSO |
| Joint Italian-Israeli hyperspectral imaging satellite. | ||||
| TBD | Vega C | ELV | PLATiNO-2 / MAIA | SSO |
| PLATiNO-2 will host the MAIA instrument payload. | ||||
Related articles
This article is a child-friendly adaptation of the Wikipedia article on Vega C, available under CC BY-SA 4.0.
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