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Aestus

Aestus pressure-fed, storable-propellant liquid rocket engine for Ariane 5 EPS upper stages. ESA identifies MMH/N2O4 propellants, 27.5 kN vacuum thrust, roughly 1,100 s burn operation, and reignitable/gimballed operation; status remains retired.

Aestus
SkywalkerPL (Marcin Grzegorz Wolny) · CC BY 4.0; provide appropriate credit, a link to the license, and indicate changes; do not imply endorsement. · Source

Identity

Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
Aestus
Status
retired

Details

Description
Aestus pressure-fed, storable-propellant liquid rocket engine for Ariane 5 EPS upper stages. ESA identifies MMH/N2O4 propellants, 27.5 kN vacuum thrust, roughly 1,100 s burn operation, and reignitable/gimballed operation; status remains retired.
Propellants
monomethyl hydrazinenitrogen tetroxide
Rocket Specs
Burn Time S
1,100
Cycle
pressure-fed
Restartable
Yes
Vacuum Thrust Kn
27.5

Links

Assets & Meta

Creation Time
July 29, 2026 at 08:15:45 UTC
Updated Time
August 22, 2026 at 06:22:33 UTC

Other

Sources
Aestus - AeroVia