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.

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cryogenic rocket engine, 
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Frameless

RS-83 Prototype Engine

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