Q110273286: Difference between revisions
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Q110273286
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{{Page|Archimedes Vacuum|Classes|variant of the Archimedes engine}} | {{Page|Archimedes Vacuum|Classes|variant of the Archimedes engine|ArchimedesVac}} | ||
Latest revision as of 15:50, 17 February 2025
Archimedes is a liquid-fuel rocket engine burning liquid oxygen and liquid methane in an oxidizer-rich staged combustion cycle. It is designed by aerospace company Rocket Lab for its Neutron rocket.
Wikidata
ArchimedesVac
specific impulse by weight 320 second, maximum thrust 900 kilonewton,
Rocket Lab,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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