← ALL ENGINES
ARIANEGROUP

Vulcain 2

RETIRED (WITH ARIANE 5)
1,359 kN (305,500 lbf)THRUST VAC (kN)
434 sISP VAC (s)
Gas GeneratorCYCLE
Liquid Hydrogen (LH₂)/LOXPROPELLANT
Jul 2026FIRST FLIGHT
ABOUT VULCAIN 2

Vulcain 2 is the European rocket engine that powered the main core of the Ariane 5 heavy-lift launcher, burning steadily for the first ten minutes of every flight to lift the rocket and its payload from the ground into space. Built in Vernon, France, it became one of the quiet workhorses of European spaceflight.

Quick facts

  • Type: Cryogenic core-stage engine (cryogenic means it burns propellants chilled to extremely low temperatures so they stay liquid).
  • Propellants: Liquid oxygen (LOX, the oxidizer that lets the fuel burn) and liquid hydrogen (LH2, the fuel).
  • Engine cycle: Gas-generator cycle.
  • Vacuum thrust: About 1,340-1,360 kN (roughly 137 tonnes-force), around 20% more than the earlier Vulcain 1.
  • Specific impulse (vacuum): About 429 seconds (a measure of how efficiently an engine turns propellant into thrust; higher is better).
  • Combustion-chamber pressure: About 117 bar.
  • Size and mass: About 3.4 m long, 2.1 m wide, dry mass around 1,800 kg.
  • Burn time: Up to about 600 seconds.
  • First successful flight: 12 February 2005 (Ariane 5 flight V521); final flight in 2023.
  • Maker: ArianeGroup (formerly Snecma / Safran), under European Space Agency (ESA) contract.

What it is and how it works

An engine like Vulcain 2 needs to push enormous amounts of propellant into its combustion chamber every second. To do that, it uses two turbopumps, which are spinning pumps driven by a small turbine. The trick is how those pumps get their power: a tiny fraction of the propellant is burned in a separate small chamber called the gas generator, and the hot gas it makes spins the turbines. This arrangement is the gas-generator cycle. The turbines then drive the pumps that force the main flow of liquid oxygen and liquid hydrogen into the big combustion chamber, where they burn to create the exhaust that produces thrust.

Because this is an “open” cycle, the gas that has spun the turbines is dumped overboard rather than fed back into the main chamber. That makes the engine simpler and tougher, at the cost of being slightly less efficient than more complex “staged-combustion” designs. The pumps work astonishingly hard: the hydrogen pump alone spins at about 34,000 rpm and delivers roughly 12 megawatts, comparable to a small power station’s output, all from a unit you could stand beside. Before the cold hydrogen is burned, it is routed around the chamber and nozzle to keep them from melting, a technique called regenerative cooling.

On Ariane 5, Vulcain 2 lights a few seconds before the two large solid boosters. This lets engineers confirm the engine is running healthily before committing to liftoff, like revving an engine and listening for trouble before releasing the brake. After the boosters drop away, Vulcain 2 burns on alone until the core stage shuts down.

Why it matters

Vulcain 2 gave Europe its own independent route to orbit on Ariane 5, one of the most reliable heavy-lift rockets ever built. As the single core-stage engine, it supplied the long, steady thrust from liftoff to orbit, while the strap-on solid boosters delivered most of the initial punch off the pad. Its extra thrust over Vulcain 1 was key to the high-performance Ariane 5 ECA, for years the leading vehicle for launching large communications satellites into geostationary orbit, often two at a time. The engine also reflects a clear philosophy: favor a simple, dependable design and reuse proven technology rather than chase maximum efficiency.

Where it is used and notable examples

  • Ariane 5 ECA: The high-performance heavy-lift variant, its core stage driven by a single Vulcain 2, used to launch large geostationary communications satellites.
  • Ariane 5 ECA+ and Ariane 5 ES: Further Vulcain 2-powered variants; Ariane 5 ES carried ESA’s Automated Transfer Vehicle (ATV) cargo ships to the International Space Station and lofted Galileo navigation satellites.
  • James Webb Space Telescope (25 December 2021): Launched by an Ariane 5 ECA whose core stage was driven by a Vulcain 2.
  • Vulcain 1: The original predecessor, first flown on Ariane 5 in 1996; Vulcain 2 increased its thrust by about 20%.

The next chapter: Vulcain 2.1

For Europe’s new Ariane 6 launcher, ArianeGroup developed an evolved version, Vulcain 2.1. It keeps the same cycle and propellants but adds cost-saving simplifications: a 3D-printed gas generator, a redesigned nozzle with far fewer parts, and ground-based ignition from burners beneath the stage instead of igniters inside the engine. It also removes the need for expensive stored helium to pressurize the oxygen tank. Vulcain 2.1 produces more than 1,370 kN of vacuum thrust at about 432 seconds of specific impulse, and first flew on Ariane 6’s maiden flight on 9 July 2024, carrying decades of proven engine heritage into Europe’s next generation of rockets.

Image: ESA
PERFORMANCE
Thrust (Sea Level)960 kN (215,800 lbf) kN
Thrust (Vacuum)1,359 kN (305,500 lbf) kN
ISP (Sea Level)318 s s
ISP (Vacuum)434 s s
Chamber Pressure11.5 MPa (1,668 psi) bar
Mass2 kg
Thrust-to-Weight68
Throttle RangeNot throttleable
Restart CapableNo
THRUST CONVERSIONS (VACUUM)
Kilonewtons1.0 kN
Pounds-force225 lbf
ENGINE CYCLE
Gas Generator
A gas generator cycle taps off a small portion of propellants to drive turbopumps via a separate combustion chamber. The turbine exhaust is dumped overboard, making it less efficient but simpler and more reliable. Used by the Merlin, F-1, and RS-27.
PROPULSION
PropellantLiquid Hydrogen (LH₂)
OxidizerLOX
Engine CycleGas Generator
Mixture Ratio6.1:1
Flow Rate~320 kg/s kg/s
PHYSICAL
Dimensions1.76 m diameter × 3.0 m length
Combustion Chambers1
Nozzle Expansion Ratio58.5:1:1
GENERAL
ManufacturerArianeGroup
CountryFrance / Europe
StatusRetired (with Ariane 5)
First FlightJuly 21, 2026
VARIANTS (3)
  • Vulcain
  • Vulcain 2
  • Vulcain 2.1
VEHICLES USING VULCAIN 2 (2)
ENGINE LINEAGE
VulcainVulcain 2Vulcain 2.1 (Ariane 6)

Related Articles