THE ANALYSIS OF THE MUTUAL DEPENDENCE OF IMPACT IONIZATION AND ELECTRON ENERGY DISTRIBUTION IN ELECTRIC PROPULSION DEVICES

Shahram Roshanpour

Abstract


The object of this study is the set of physical processes in the non-equilibrium plasma of electric propulsion devices. The subject of the study is impact ionization, specifically the feedback effect on the electron energy spectrum. The aim of the study is to derive expressions for the impact ionization characteristics in the right-hand sides of the mathematical model equations describing electric propulsion devices based on the compromise kinetic-fluid model. The objectives of the study are: to analyze existing continuum mechanics models that incorporate the impact ionization process building upon the results presented in the author's previous works; to write an expression for the average values over the electron energy spectrum of the ionization volume coefficient and cross-section and to analyze the behavior of the calculated values taking into account the interdependence of ionization processes and the formation of the electron energy distribution. The methods used in the study include an analytical investigation of existing process models to determine their limits of applicability in rarefied plasma, as well as a theoretical analysis of the impact of ionization on the electron energy spectrum, taking into account the characteristics of plasma confined by potential barriers in a boundary bipolar layer. Calculated energy-dependent distributions above the potential barrier yielded lower values than those obtained for a Maxwellian distribution; however, higher values were observed below the ionization potential at elevated electron temperatures. Based on an analysis of the influence of the electron energy spectrum on the ionization intensity and the influence of the electromagnetic field on electron transport in energy space, a positive feedback was demonstrated: at relatively high electron temperatures, the need to transport them "upward" from the region below the ionization potential leads to an excess of electrons in this region. In turn, this surplus increases the energy-averaged ionization cross-section, further reinforcing the electron excess in the lower energy spectrum.


Keywords


electric propulsion devices, electrons energy distribution; impact ionization; potential barrier; bipolar boundary layer; angular moments model

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References


Pitaevskii, L. P. Physical Kinetics, Volume 10. Butterworth-Heinemann, 1981. 464 p.

Fitzpatrick, R. Courses Taught By Richard Fitzpatrick at University of Texas at Austin. Available et: https://farside.ph.utexas.edu/teaching.html

Fife, J. M. Hybrid-PIC Modeling and Electrostatic Probe Survey of Hall Thrusters: PhD thesis. Massachusetts Institute of Technology, Department of Aeronautics, 1998. 256 p.

Ortega, A. L., Mikellides, I. G. 2D Fluid-PIC Simulations of Hall Thrusters with Self-Consistent Resolution of the Space-Charge Regions. Plasma, 2023, vol. 6, iss. 3, pp. 550-562. DOI: 10.3390/plasma6030038.

Hofer, R. R., Katz, I., Mikellides, I., Gamero-Castano, M. Heavy Particle Velocity and Electron Mobility Modeling in Hybrid-PIC Hall Thruster Simulations. The 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006. 17 p. DOI: 10.2514/6.2006-4658.

Panelli, M., Morfei, D., Milo, B., D’Aniello, F. A., Battista, F. Axisymmetric Hybrid Plasma Model for Hall Effect Thrusters. Particles, 2021, no 4, iss 2, pp. 296-324. DOI: 10.3390/particles4020026

Guisset, S., Brull, S., Dubroca, B., d’Humières, E., Karpov, S., Potapenko, I. Asymptotic-preserving scheme for the Fokker-Planck-Landau-Maxwell system in the quasi-neutral regime. Communications in Computational Physics, 2016, vol. 19, iss. 02, pp. 301-328.

Guisset, S., Aregba, D., Brull, S., Dubroca, B. The M1 angular moments model in a velocity-adaptive frame for rarefied gas dynamics applications. Multiscale Modeling & Simulation, 2017, vol. 15, iss. 4. 30 p.

Guisset, S. Angular moments models for rarefied gas dynamics. Numerical comparisons with kinetic and Navier-Stokes equations. Kinetic and Related Models (KRM), 2020, vol. 13, iss. 4, pp. 739-758. DOI: 10.3934/krm.2020025

Guisset, S., Brull, S., d’Humières, E., Dubroca, B., Tikhonchuk, V. Classical transport theory for the collisional electronic M1 model. Physica A: Statistical Mechanics and its Applications, 2016, vol. 446. 19 p.

Nesterenko, S., Zhihao, H., Roshanpour, S. Compromise kinetic-fluid model of electrons dynamics in electric propulsion devices with closed electrons drift as an alternative to the hybrid PIC-Fluid method. Aerospace Technic and Technology, 2025, no. 1 (201), pp. 28-37. DOI: 10.32620/aktt.2025.1.03

Nesterenko, S., Huang Zhihao, Roshanpour, S. Mathematical aspects of M unlimited angular model in electric propulsion. The 2nd International scientific and practical conference "Challenges and Opportunities in Modern Scientific Research", 2025, iss. 16, pp. 208-213.

Nesterenko, S., Huang, Z., Roshanpour, S. Parameters of the bipolar boundary layer in electric propulsion thrusters with closed electron drift: M1+ angular model. The 2nd International scientific and practical conference "Modern Scientific Research: Theoretical and Practical Aspects", 2025, iss 37, pp. 462-479.

Guo, Z., Huang, Z., Peng, S. The role of impact ionization in the balance of particles, momentum and energy in plasma-ion and Hall effect thrusters. The XXXI International Scientific and Practical Conference "Trends in the development of modern scientific", Vancouver, Canada, 2021, pp. 399-440.

Loyan, A. V., Nesterenko, S. Yu., Guo Z., Huang Z. Quasi-one-dimensional mathematical model of processes in Hall effect and plasmaion thrusters. Open Information and Computer Integrated Technologies, 2021, no 92, pp. 41-54.




DOI: https://doi.org/10.32620/aktt.2026.4.05