Diagnostics of rocket and jet engines through characteristics of the intrinsic electromagnetic field of combustion products
- Authors: Yagodnikov D.A.1, Rudinskii A.V.1,2
-
Affiliations:
- Bauman Moscow State Technical University
- Baranov Central Institute of Aviation Motors
- Issue: Vol 55, No 5 (2017)
- Pages: 808-824
- Section: Review
- URL: https://ogarev-online.ru/0018-151X/article/view/157356
- DOI: https://doi.org/10.1134/S0018151X17050200
- ID: 157356
Cite item
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
Supplementary files
