Performance enhancement of an argon-based propellant in a Hall thruster-Reference-Cited by-同舟云学术

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Performance enhancement of an argon-based propellant in a Hall thruster

Published:2019-09 Issue: Volume:167 Page:520-523
ISSN:0042-207X
Container-title:Vacuum
language:en
Short-container-title:Vacuum

Author:

Yamasaki Junko,Yokota Shigeru,Shimamura Kohei^ORCID

Funder

JSPS KAKENHI

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation

Reference17 articles.

1. Test facility concept for high power electric propulsion;Kinefuchi,2014

2. Hall thruster development for Japanese space propulsion programs;Hamada;Trans. JSASS,2017

3. Definition of Hall current ion-thruster performance;Komurasaki;J. Propul. Power,1992

4. Efficiency analysis of a Hall thruster operating with krypton and xenon;Linnell;J. Propul. Power,2006

5. Alternate propellants for PPS Hall-effect plasma thruster;Lorand,2013

Cited by 14 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. Argon admixture-driven enhanced ionization and performance of a 5 kW Hall thruster on krypton;Journal of Physics D: Applied Physics;2024-05-16

2. Numerical and experimental research on the performance of an iodine-fed Hall thruster;Vacuum;2024-04

3. Growth mechanism and characteristics of electron drift instability in Hall thruster with different propellant types;Chinese Physics B;2024-01-01

4. Review of alternative propellants in Hall thrusters;Acta Astronautica;2023-11

5. Review of closed drift thruster neutral flow dynamics;AIP Advances;2023-07-01

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