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.
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.