Q1785430: Difference between revisions
From Spacefaring
Q1785430
Bot: Automated import of articles *** existing text overwritten *** |
Bot: Automated import of articles *** existing text overwritten *** |
||
| Line 1: | Line 1: | ||
{{Page|Vinci|Classes|European hydrolox rocket engine | {{Page|Vinci|Classes|model of European hydrolox upper stage rocket engine|}} | ||
Latest revision as of 12:53, 2 September 2025
Vinci is a restartable, cryogenic, liquid-propellant rocket engine that powers the upper stage of Ariane 6. While development began in 1998 for the planned Ariane 5ME upgrade, funding for that programme shifted in 2014 to prioritize the development of Ariane 6, making Vinci the engine for the new launcher.
Wikimedia, Wikidata
diameter 1.84 metre, specific impulse by weight 457.2 second, height 3.22 metre, mass 280 kilogram, maximum thrust 180 kilonewton,
ArianeGroup, France,
France, ArianeGroup, cryogenic rocket engine, Dong Fang Hong 2, Ekran,
-
Location: KML, Cluster Map, Maps,
DaVinci-Oberstufentriebwerk - Vinci rocket engine (14050083338)
Maquette Vinci - Musée Safran
Vinci simple0002| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | DaVinci-Oberstufentriebwerk - Vinci rocket engine (14050083338) | Commons | ||
| commons | image | Maquette Vinci - Musée Safran | Commons | ||
| commons | image | Vinci simple0002 | Commons | ||
.jpg){kind=link}
