LIQUID PROPELLANT ROCKET ENGINE Russian patent published in 2017 - IPC F02K9/48 F02K99/00 

FIELD: engines and pumps.

SUBSTANCE: liquid propellant rocket engine contains a control unit, a chamber, a turbopump unit, containing fixed on the shaft turbine, pumps of oxidizer and fuel and a gas generator, mounted thereon and connected by means of gas duct with chamber, an ignition devices at a combustion chamber and a gas generator, an electric generator mounted on a shaft of the turbopump unit, connected by the power cables with the combustion enhancement means, wherein the microwave emitters are applied as the means of ccombustion enhancement, installed on the surface of the chamber and/or the gas generator. Microwave radiation generators can be mounted radially on the pipe-clips in the form of semi-rings. The magnetrons, klystrons tubes can be used as the microwave radiation generators. The microwave radiation generators can be connected with electric generator through the switching center.

EFFECT: improved completeness of rocket fuel components combustion and improved launch.

5 cl, 10 dwg