Q7277682: Difference between revisions
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Q7277682
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{{Page|RS-83|Classes|proposed hydrolox rocket engine inteded to surpass the RS-68}} | {{Page|RS-83|Classes|proposed hydrolox rocket engine inteded to surpass the RS-68|}} | ||
Latest revision as of 16:04, 17 February 2025
The RS-83 was a rocket engine design for a reusable liquid hydrogen/liquid oxygen rocket larger and more powerful than any other. The RS-83 was designed to last 100 missions, and was intended for use on the first stage of a two-stage-to-orbit reusable launch vehicle.
Wikimedia, Wikidata
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-83 Prototype Engine| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | RS-83 Prototype Engine | Commons | ||
