Modeling of plasma processes in the slowly diverging magnetic fields at the exit of an applied-field magnetoplasmadynamic thruster
Author:
Publisher
AIP Publishing
Subject
Condensed Matter Physics
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4824619
Reference21 articles.
1. Simulation and laboratory validation of magnetic nozzle effects for the high power helicon thruster
2. Plasma flow processes within magnetic nozzle configurations
3. Production of a High-Mach-Number Plasma Flow for an Advanced Plasma Space Thruster
4. The Vasimr Rocket
5. Two-dimensional supersonic plasma acceleration in a magnetic nozzle
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1. Simulation of magnetoplasmadynamic process with applied magnetic field;Acta Physica Sinica;2022
2. High-spatial-resolution image reconstruction-based method for measuring electron temperature and density of the very near field of an applied-field magnetoplasmadynamic thruster;Journal of Physics D: Applied Physics;2021-01-22
3. Application of the view factor model on the particle-in-cell and Monte Carlo collision code;Physical Review E;2020-09-16
4. Design and experimental results of a laser-ignited solid-propellant-fed magnetoplasmadynamic thruster;Review of Scientific Instruments;2020-07-01
5. Electric potential barriers in the magnetic nozzle;Physical Review E;2020-05-26
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