Quantum-mechanical model of ion thruster for small spacecraft

Authors

DOI:

https://doi.org/10.25206/2588-0373-2024-8-2-68-76

Keywords:

models of ion and plasma thruster, mathematical modeling of the motion of charged particles, ion engine, small spacecraft, quantum mechanics, quantum mechanical model

Abstract

The article presents a quantum mechanical model of an ion thruster. The basic equations describing
the shape of the accelerated beam are considered. Detector plates demonstrating the interference
pattern in thin films are presented. A mathematical description of the relief of thin films is given using
the resulting wave function. The operation of a low-power ion engine is demonstrated. The results
of numerical solution of the model with different initial values are shown. Based on the results of
calculations, diagrams of the trajectories of charged particles are constructed.

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Author Biographies

Fedyanin Viktor Viktorovich, Omsk State Technical University, Russia, Omsk, Mira Ave., 11, 644050

Candidate of Technical Sciences, Associate Professor of Electrical Equipment Department, Omsk State Technical University (OmSTU), Omsk.

Shalay Viktor Vladimirovich, Omsk State Technical University, Russia, Omsk, Mira Ave., 11, 644050

Doctor of Technical Sciences, Professor, Head of Oil and Gas Engineering, Standardization and Metrology Department, OmSTU, Omsk.

Fedorov Vladimir Kuzmich, Omsk State Technical University, Russia, Omsk, Mira Ave., 11, 644050

Doctor of Technical Sciences, Professor, Professor of Electrical Supply of Industrial Enterprises Department, OmSTU, Omsk.

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Abstract views: 178

Published

2024-06-28

How to Cite

Fedyanin . В. В., Shalay В. В. ., & Fedorov В. К. (2024). Quantum-mechanical model of ion thruster for small spacecraft. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 8(2), 68–76. https://doi.org/10.25206/2588-0373-2024-8-2-68-76

Issue

Section

Aviation and rocket-space engineering