RS-83

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.

MainWikipediaGalleryBibliographyTableSearch

Wikimedia, Wikidata
cryogenic rocket engine, 
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, 

​

Location: KML, Cluster Map, Maps,

Frameless

RS-83 Prototype Engine

Type	Subtype	Date	Description	Notes	Source
commons	image		RS-83 Prototype Engine		Commons