Radial distribution of electrons rotation moment in hall effect and plasma-ion thrusters
The subject matter of the article is the radial distribution of electrons movement parameters inside electric propulsion thrusters with closed electrons drift. The radial magnetic field in Hall effect thrusters is the limits the axial flow of electrons because of interaction with azimuth electron cu...
Enregistré dans:
Auteur principal: | Zongshuai Guo |
---|---|
Format: | article |
Langue: | EN RU UK |
Publié: |
National Aerospace University «Kharkiv Aviation Institute»
2021
|
Sujets: | |
Accès en ligne: | https://doaj.org/article/e23db6a46b024f0aa27082f40a3e20b0 |
Tags: |
Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!
|
Documents similaires
-
Influences of Magnetic Flux Density on Discharge Characteristics of Low-Power Hall Thruster
par: Weilong Guo, et autres
Publié: (2021) -
Inductive Coupling Discharge Characteristics of a 10-cm Dual-Stage 4-Grid Radiofrequency Ion Thruster
par: Yanxu Pu, et autres
Publié: (2021) -
Performance Simulation of a 5 kW hall Thruster
par: L. Yang, et autres
Publié: (2021) -
A Conflict Risk Analysis of MAV\UAV Flight in Shared Airspace
par: ChaoYu Xia, et autres
Publié: (2021) -
Research on the Fatigue of Small Impulse Turbine Blade Based on the Numerical Simulation and Experimental Tests
par: Shijie Liu, et autres
Publié: (2021)