Thrust chamber and nozzle
- Combustion chamber
- Divergent nozzle (SWAN sandwich nozzle)
- Nozzle structural reinforcements
- Nozzle steering (gimbal) system
Gas-generator LOX/LH2 engine for the Ariane 6 core stage; sources state a laser-welded sheet-metal nozzle built by GKN Aerospace and a 3D-printed gas generator whose injection head is a nickel-based alloy. Few other materials are published.
arianegroup-vulcain-2-1 Gas-generator LOX/LH2 engine for the Ariane 6 core stage; sources state a laser-welded sheet-metal nozzle built by GKN Aerospace and a 3D-printed gas generator whose injection head is a nickel-based alloy. Few other materials are published.
Vulcain 2.1 is the single engine of the Ariane 6 core stage. It burns for about eight minutes to lift the launcher away from Earth before the Vinci upper stage takes over. Its laser-welded nozzle and 3D-printed gas generator were introduced to simplify production compared with the Ariane 5 Vulcain 2.
No photos we are allowed to show yet. If you have a photo of this product and the right to share it, send it to us.
Used in Gas generator injection head.
upgraded version of the Ariane 5 main-stage engine
version of Vulcain 2 adapted for the Ariane 6 main stage
developer of the engine, with European partners, for ESA
SWAN nozzle, built at Trollhattan, Sweden
turbine assemblies for the turbopumps
liquid oxygen turbopump
liquid oxygen turbopump responsibility moving here from Avio
valves and pressure regulators
No alloys for the nozzle sheets, chamber liner or jacket, injector, turbopump rotors, bearings, seals, valves or ducts. No standards.
What is written above is built from these numbers and quotes. Each row links to the page it was taken from. Get all of it as JSON, or ask our MCP server.
| What | Value |
|---|---|
| Vacuum thrust | More than 1370 kN |
| Vacuum thrust (eoPortal) | 1,371 kN |
| Specific impulse (vacuum) | 432 s |
| Chamber pressure | 118.8 bar |
| Mixture ratio (oxidizer to fuel) | 6.03 |
| Cycle | Gas generator, two independent turbopumps |
| Propellants | Liquid oxygen and liquid hydrogen |
| Propellant flow and burn time | Over 327 kg/s for 468 s |
| Height | 3.7 m |
| Diameter | 2.5 m |
| Mass | About 2 tonnes |
| Nozzle diameter (SWAN nozzle) | 2.5 m |
| Engines per vehicle | One, on the Ariane 6 main (core) stage |
| First hot-fire test of the Ariane 6 version | DLR P5 test facility, Lampoldshausen, reported 23 January 2018 |
| Qualification | Completed |
| First flight | Ariane 6 maiden launch, 9 July 2024 |
Each material named in the sources: where it is used here, which other products use it, and its key numbers when its material page exists.
Used in 1 partGas generator injection head
Only the gas generator injection head has a stated material (a nickel-based alloy, from a French CETIM customer sheet). The nozzle is described as laser-welded sheet metal with no alloy named. Chamber, turbopumps, igniters and valves are listed from ESA, ArianeGroup, Avio, GKN and trade sources with no material stated.
| Part | Material | Finish and standard | Made by |
|---|---|---|---|
| Combustion chamber“Two turbopumps inject hydrogen and oxygen into the combustion chamber.” | Not said | — | — |
| Divergent nozzle (SWAN sandwich nozzle)“built by laser-welding two large sheets of metal together” | Not said | — | — |
| Nozzle structural reinforcements“additively manufactured structural reinforcements” | Not said | — | — |
| Nozzle steering (gimbal) system“Its nozzle is rapidly tilted and turned during a launch to keep the rocket flying upright” | Not said | — | — |
| Part | Material | Finish and standard | Made by |
|---|---|---|---|
| Gas generator“a gas generator built using 3D printing, a simplified divergent nozzle, and an oxygen heater for tank pressurization” | Not said | — | — |
| Gas generator injection head“la conformité de cette pièce en alliage à base de nickel” | nickel-based alloy (grade not stated)nickel-based-alloy | — | — |
| Oxygen heater for tank pressurization“Additional 3D printed components include the gas generator and the Oxygen heater for tank pressurization” | Not said | — | — |
| Part | Material | Finish and standard | Made by |
|---|---|---|---|
| Liquid hydrogen turbopump“Two turbopumps inject hydrogen and oxygen into the combustion chamber.” | Not said | — | — |
| Liquid oxygen turbopump (Mk2)“the Mk2 turbopump features a host of improvements in hydraulics, balance, sealing, and turbine performance” | Not said | — | Avio |
| Liquid oxygen turbopump Dynamic Seal Package“In particular, Avio improved the Dynamic Seal Package (DSP)” | Not said | — | Avio |
| Liquid oxygen turbopump Active Balancing System“the Active Balancing System (ABS), which compensates for the axial forces generated by the turbine” | Not said | — | Avio |
| Turbine assemblies“These turbine assemblies will be manufactured at GKN Aerospace” | Not said | — | GKN Aerospace |
| Part | Material | Finish and standard | Made by |
|---|---|---|---|
| Combustion chamber ignition system (ground-based)“the combustion chamber ignition system has been moved from the engine to the launch pad” | Not said | — | — |
| Gas generator igniter and turbine pump starter“crucial components like a Thrust Chamber Igniter (TCI), Gas Generator Igniter (GGI) and a Turbine Pump Starter (TPS)” | Not said | — | — |
| Hot gas valve (electrically operated)“a new electrically-operated hot gas valve” | Not said | — | — |
| Valves and pressure regulators“In Turin, Italy, the former Microtecnica site now owned by Safran produces valves and pressure regulators” | Not said | — | Safran, Turin |
No alloys for the nozzle sheets, chamber liner or jacket, injector, turbopump rotors, bearings, seals, valves or ducts. No standards.
Collected from public pages and documents, checked 4 Nov 2026.
Published · Updated