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Vinci

ArianeGroup's Vinci is the Ariane 6 upper-stage cryogenic LOX/LH2 engine. ArianeGroup describes its expander cycle, approximately 180 kN thrust, multiple-ignition capability, and upper-stage flexibility for clustered payload insertion; ESA records 18 tonnes vacuum thrust and 465 s specific impulse and notes a final restart for controlled upper-stage disposal. ArianeGroup's flight-model production and integration work support active status.

Identity

Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
Vinci
Status
active

Details

Description
ArianeGroup's Vinci is the Ariane 6 upper-stage cryogenic LOX/LH2 engine. ArianeGroup describes its expander cycle, approximately 180 kN thrust, multiple-ignition capability, and upper-stage flexibility for clustered payload insertion; ESA records 18 tonnes vacuum thrust and 465 s specific impulse and notes a final restart for controlled upper-stage disposal. ArianeGroup's flight-model production and integration work support active status.
Propellants
liquid hydrogenliquid oxygen
Rocket Specs
Cycle
expander
Restartable
Yes
Vacuum Specific Impulse S
465
Vacuum Thrust Kn
180

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Creation Time
August 1, 2026 at 08:05:17 UTC
Updated Time
August 15, 2026 at 04:05:47 UTC

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