Design and Analysis of Injector with Different Configurations for Liquid Rocket Engine

The performance of the rocket is determined by atomization, mixing and combustion process. Injectors are used to control these processes. Suitable method should be followed, so that increased. injector implementation in rockets determines nozzle can achieved. as simple a number small diameter holes arranged carefully constructed patterns through which fuel oxidizer travel. an improved either using superior propellant combustion, increasing mass flow rate, positioning angle hole or reducing size & orifices on plate. In here position varied for different angles injectors improve rocket. modeled Solidworks two dimensional analysis carried out ANSYS Fluent cases.