Q968432: Difference between revisions
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Q968432
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{{Page|RS-68|Classes|large hydrogen-oxygen rocket engine that powers the Delta IV rocket}} | {{Page|RS-68|Classes|large hydrogen-oxygen rocket engine that powers the Delta IV rocket|}} | ||
Latest revision as of 16:07, 17 February 2025
The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown.
Wikimedia, Wikidata
Aerojet Rocketdyne, Pratt & Whitney Rocketdyne,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Tarshish, cryogenic rocket engine, Dong Fang Hong 2, Ekran, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
RS-68 Rocket Engine
RS-68 Rocket Engine at NASA's Stennis Space Center.| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | RS-68 Rocket Engine | Commons | ||
| commons | image | RS-68 Rocket Engine at NASA's Stennis Space Center. | Commons | ||
