Experimental and Theoretical Study and Development of Electrical and Physical Methods of Monitoring and Diagnostics of Liquid- Propellant Rocket Engines

Electrical and physical characteristics of the working process of the model liquid-propellant rocket engine on the gaseous oxygen and ethyl alcohol are studied. A linear dependence of the magnetic intensity upon the pressure in the combustion chamber is obtained. The possibility of development of the contactless electrical and physical methods of diagnostics and monitoring of burning processes in power generation facilities is shown.