С. Г. Ивахненко

ORCID: 0000-0002-5873-5806
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About
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Research Areas
  • Plasma Diagnostics and Applications
  • Ion-surface interactions and analysis
  • Metal and Thin Film Mechanics
  • Vacuum and Plasma Arcs
  • Particle accelerators and beam dynamics
  • Advanced Surface Polishing Techniques
  • Electron and X-Ray Spectroscopy Techniques
  • Advanced Machining and Optimization Techniques
  • Glass properties and applications
  • Material Science and Thermodynamics
  • Advanced Measurement and Detection Methods
  • Power Systems and Renewable Energy
  • Plasma Applications and Diagnostics
  • Real-time simulation and control systems
  • Magnetic confinement fusion research
  • Solar Thermal and Photovoltaic Systems
  • Advanced Combustion Engine Technologies
  • Surface Roughness and Optical Measurements
  • Vehicle emissions and performance
  • Ionosphere and magnetosphere dynamics
  • Field-Flow Fractionation Techniques
  • Solar and Space Plasma Dynamics
  • Electrohydrodynamics and Fluid Dynamics
  • Building Energy and Comfort Optimization
  • Welding Techniques and Residual Stresses

Bauman Moscow State Technical University
2014-2021

Murmansk State Technical University
2014-2016

The paper considers the application of Hall thruster using ambient atmospheric air for orbital station keeping. This is a relevant direction at up-to-date development stage propulsion systems. Many teams designers electric rocket thrusters evaluate different schemes particle acceleration low-earth orbit. Such technical solution allows us to abandon storage systems working agent on spacecraft board. Thus, lifetime such system orbit wouldn`t be limited by fuel range. suggests scheme device...

10.7463/1216.0852758 article EN cc-by Science and Education of the Bauman MSTU 2016-12-03

This article considers experimental demonstration of the effect azimuthal ion deflection in magnetic field.Deflection a beam field opposite polarity was shown.Theoretical dependences for values an angle deviation obtained previous works were confirmed.

10.7463/1112.0483882 article EN Science and Education of the Bauman MSTU 2012-11-03

Холловские двигатели уже 40 лет успешно эксплуатируются на космических аппаратах [1, 2, 3].Они широко используются для коррекции орбиты спутников, а также маршевых операций по изменению высоты полета.Традиционно в таких двигателях использует ксенон, ввиду его высокой атомной массы, относительно низкого потенциала ионизации, низкой химической активности и ряда других качеств.Однако ксенон имеет высокую стоимость, объясняемую малой распространенностью земле, что увеличивает затраты не только...

10.7463/1212.0483944 article RU Science and Education of the Bauman MSTU 2012-12-03

The authors consider influence of azimuthal spin ions on ion beam divergence in the engine with an anode layer.It is shown that takes form a one-sheet hyperboloid.The obtained dependences describing hyperboloid, bounding curves and asymptotes, depending geometry deviation angle.Calculation results graphic dependencies are given. Publications keywords:anode layer thruster

10.7463/1012.0483832 article EN Science and Education of the Bauman MSTU 2012-10-03

One of the most commonly used tools in ion-plasma technology is End Hall ion source, which used, particular, for etching and other processes. The ability to operate on almost any gas, a highly divergent beam generated ions energy range up several hundred electronvolts determine wide possibilities using sources science production. There are two main design schemes such actively – with floating an anode potential discharge chamber rear wall. characteristics wall have been extensively studied...

10.18127/j00338486-202411-20 article EN Radioengineering 2024-11-11

Abstract This paper considers the study of self electromagnetic emission from experimental model low-power thruster with anode layer (TAL) developed by Bauman Moscow State Technical University. The measurements were carried out during operation on krypton and xenon for three operating modes: 600 W, 800 W 1000 at a discharge voltage 300 V. Parameters generated fields measured in frequency range 1 GHz to 12 filter bandwidth MHz. receiving antenna was installed distance m exit plane,...

10.1088/1742-6596/1925/1/012081 article EN Journal of Physics Conference Series 2021-05-01

АннотацияКлючевые слова Показано, что эффект азимутального отклонения ионов в пучке ускорителя с замкнутым азимутальным дрейфом электронов можно использовать для управления формой ионного пучка и профилем распределения плотности тока по радиусу.Изменяя профиль магнитного поля вдоль оси ускорительного канала, управлять тока, придавая ему как кольцевую форму, так близкую к распределению Гаусса

10.18698/1812-3368-2017-3-24-36 article RU Herald of the Bauman Moscow State Technical University Series Natural Sciences 2017-05-01
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