RS-83
From Spacefaring
Q7277682
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, Sweden, Tarshish, cryogenic rocket engine, Dong Fang Hong 2, Ekran,
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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 | ||
