Quantum-mechanical model of ion thruster for small spacecraft
https://doi.org/10.25206/2588-0373-2024-8-2-68-76
EDN: SGOLER
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.
About the Authors
V. V. FedyaninRussian Federation
Fedyanin Viktor Viktorovich - Candidate of Technical Sciences, Associate Professor of Electrical Equipment Department, SPIN-code: 1728-1697. AuthorID (SCOPUS): 57194235343. ResearcherID: O-9899-2015.
Omsk, Mira Ave., 11, 644050
V. V. Shalay
Russian Federation
Shalay Viktor Vladimirovich - Doctor of Technical Sciences, Professor, Head of Oil and Gas Engineering, Standardization and Metrology Department, OmSTU, SPIN-code: 2322-6820. AuthorID (RSCI): 9913. AuthorID (SCOPUS): 35792469000. AuthorID (SCOPUS): 56755298300. AuthorID (SCOPUS): 57190972363. ResearcherID: P-8233-2015.
Omsk, Mira Ave., 11, 644050
V. K. Fedorov
Russian Federation
Fedorov Vladimir Kuzmich - Doctor of Technical Sciences, Professor, Professor of Electrical Supply of Industrial Enterprises Department, OmSTU. SPIN-code: 2389-6978. AuthorID (RSCI): 512746. AuthorID (SCOPUS): 57194237212.
Omsk, Mira Ave., 11, 644050
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Review
For citations:
Fedyanin V.V., Shalay V.V., Fedorov V.K. Quantum-mechanical model of ion thruster for small spacecraft. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2024;8(2):68-76. (In Russ.) https://doi.org/10.25206/2588-0373-2024-8-2-68-76. EDN: SGOLER
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