Study on electrons conduction paths in Hall thruster ignition processes with the cathode located inside and outside the magnetic separatrix-Reference-Cited by-同舟云学术

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Study on electrons conduction paths in Hall thruster ignition processes with the cathode located inside and outside the magnetic separatrix

Published:2019-02 Issue: Volume:155 Page:153-159
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Li Wen-Bo,Li Hong,Ding Yong-Jie,Wei Li-Qiu,Gao Qian,Yan Shi-Lin,Meng Tian-Hang,Zhu Xi-Ming,Yu Da-Ren

Funder

National Natural Science Foundation of China

Science and Technology Innovation Project of Hunan Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Optimization of a wall-less Hall thruster;Vaudolon;Appl. Phys. Lett.,2015

2. Recent progress and perspectives of space electric propulsion systems based on smart nanomaterials;Levchenko;Nat. Commun.,2018

3. A 200 W Hall thruster with hollow indented anode;Ding;Acta Astronaut.,2017

4. LaB6 hollow cathodes for ion and Hall thrusters;Goebel;J. Propul. Power,2007

5. Space micropropulsion systems for Cubesats and small satellites: from proximate targets to furthermost frontiers;Levchenko;Appl. Phys. Rev.,2018

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1. A novel optical emission spectroscopy method for diagnostics of contribution of different ionization mechanisms and flux of ions in different valences in discharge channel of a Hall thruster;Chinese Journal of Aeronautics;2024-04

2. Modeling of Ion Thruster Plume Neutralization Using Kinetic Simulations;AIAA SCITECH 2024 Forum;2024-01-04

3. Kinetic simulation of ion thruster plume neutralization in a vacuum chamber;Plasma Sources Science and Technology;2023-11-01

4. A wavelet-based method for thrust noise assessment in gravitational wave detection over wide-frequency-range;Acta Astronautica;2022-08

5. Fluid simulation on effect of background magnetic field on plasma characteristics in a Hall thruster;AIP Advances;2022-07-01

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