Q16840: Difference between revisions
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Q16840
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{{Page|Aestus|Classes|European rocket engine}} | {{Page|Aestus|Classes|European rocket engine|Astrium Aestus}} | ||
Latest revision as of 15:53, 17 February 2025
Aestus is a hypergolic liquid rocket engine used on an upper stage of Ariane 5 family rockets for the orbital insertion. It features unique design of 132 coaxial injection elements causing swirl mixing of the MMH propellants with nitrogen tetroxide oxidizer. The pressure-fed engine allows for multiple re-ignitions.
1997 — 2018
Wikimedia, Wikidata
Astrium Aestus
Astrium,
Sikh Confederacy, 1990s, Republic of Haiti, 1997, pressure-fed engine, Ekran, Dong Fang Hong 2, Astrium, Tarshish, Ashkenaz, Reman, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Chinland, Calvinist Republic of Ghent,
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Location: KML, Cluster Map, Maps,
ILA 2018, Schönefeld (1X7A5210)
Aestus
Ariane 5 EPS Upper Stage| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | ILA 2018, Schönefeld (1X7A5210) | Commons | ||
| commons | image | Aestus | Commons | ||
| commons | image | Ariane 5 EPS Upper Stage | Commons | ||
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