Diagnostics of rocket and jet engines through characteristics of the intrinsic electromagnetic field of combustion products


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Abstract

This paper presents the feasibility of using electrophysical methods to diagnose and tune the propulsion systems of rocket and space technology items by analyzing published experimental and theoretical results on the electrophysical characteristics of combustion processes and combustor discharge of liquid- and solid-propellant rocket and air-breathing jet engines. Data on the development of emergency protection systems for propulsion engines, based on monitoring the electrophysical characteristics of the propellant, are presented.

About the authors

D. A. Yagodnikov

Bauman Moscow State Technical University

Author for correspondence.
Email: daj@bmstu.ru
Russian Federation, Moscow, 105005

A. V. Rudinskii

Bauman Moscow State Technical University; Baranov Central Institute of Aviation Motors

Email: daj@bmstu.ru
Russian Federation, Moscow, 105005; Moscow, 111116

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