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Vulcain 2

Snecma-led Vulcain 2 is a cryogenic liquid-oxygen/liquid-hydrogen main-stage engine for Ariane 5 ECA and Ariane 5 ES. ESA describes it as an improved Vulcain with a gas generator, oxygen and hydrogen turbopumps, a redesigned nozzle extension, and a 20% thrust increase over the original Vulcain. The Vulcain-2 technical table records 1,350 kN vacuum thrust, 433 s specific impulse, a 6.10 mixture ratio, and 1,935 kg mass.

Identity

Aliases
Vulcain 2Vulcain-2Vulcain 2 engineSnecma Vulcain 2
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
Vulcain 2
Status
retired

Details

Description
Snecma-led Vulcain 2 is a cryogenic liquid-oxygen/liquid-hydrogen main-stage engine for Ariane 5 ECA and Ariane 5 ES. ESA describes it as an improved Vulcain with a gas generator, oxygen and hydrogen turbopumps, a redesigned nozzle extension, and a 20% thrust increase over the original Vulcain. The Vulcain-2 technical table records 1,350 kN vacuum thrust, 433 s specific impulse, a 6.10 mixture ratio, and 1,935 kg mass.
Dry Mass Kg
1,935
Family
Manufacturers
Propellants
liquid hydrogenliquid oxygen
Rocket Specs
Chamber Count
1
Cycle
gas-generator
Vacuum Specific Impulse S
433
Vacuum Thrust Kn
1,350

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Assets & Meta

Creation Time
July 29, 2026 at 09:07:57 UTC
Updated Time
August 23, 2026 at 10:05:47 UTC

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Sources