Rocket engines Archives - Projects, Thesis, Dissertation, Project Reports

FLOW AND ATOMIZATION CHARACTERISTICS OF CRYOGENIC FLUID FROM A COAXIAL ROCKET INJECTOR

High thrust-to-weight ratio and consistent performance over a range of operating conditions make cryogenic rocket engines one of the best options for space propulsion. However, future space explorations and missions to moon, mars and beyond require improvements in our present knowledge of

Simulating combustion flow in a rocket chamber

Liquid propellant rocket engines are very complex machinery and require immense research time to obtain the best performance possible. Therefore its performance efficiency has to be determined based on the various losses that occur during its operation. This research aims to measure

Rocket engines

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