Numerical study of a hollow cathode neutraliser by means of a zero-dimensional plasma model-Reference-Cited by-同舟云学术

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Numerical study of a hollow cathode neutraliser by means of a zero-dimensional plasma model

Published:2020-09 Issue: Volume:174 Page:219-235
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Gurciullo Antonio^ORCID,Fabris Andrea Lucca^ORCID,Potterton Thomas

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Discharge hollow cathode design for a 4-gridded ion engine;Coletti,2010

2. Effect of cathode position on Hall-effect thruster performance and cathode coupling voltage;Sommerville,2007

3. Vacuum facility effects on Quad confinement thruster testing;Lucca Fabris,2017

4. An investigation of mercury hollow cathode phenomena;Siegfried,1978

5. Phenomenological model describing orificed, hollow cathode operation;Siegfried;AIAA J.,1983

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Establishing criteria for the transition from kinetic to fluid modeling in hollow cathode analysis;Physics of Plasmas;2024-09-01

2. Solution of Orifice Hollow Cathode Plasma Model Equations by Means of Particle Swarm Optimization;Applied Sciences;2024-07-03

3. Development of a modular hollow cathode for ground testing of plasma thrusters;Vacuum;2024-01

4. Plasma behavior of a low current orificed hollow cathode using krypton propellant for electric thruster applications;Journal of Physics D: Applied Physics;2023-08-08

5. Development of a Modular Hollow Cathode for Ground Testing of Plasma Thrusters;2023

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