Cryogenic rocket engine
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A cryogenic rocket engine is a rocket engine that uses a cryogenic fuel and oxidizer; that is, both its fuel and oxidizer are gases which have been liquefied and are stored at very low temperatures. T
Vulcain engine of Ariane 5 rocket
RL-10 is an early example of cryogenic rocket engine.
Chinese YF-77 engine used by Long March 5
CE-7.5
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The CE-7.5 is a cryogenic rocket engine developed by ISRO to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was developed as a part of the Cryogenic Upper Stage Project. It replaced
The CUS15 upper stage of GSLV-F09 powered by the CE-7.5 engine at Stage Preparation Facility