Performance of a 4 cm iodine-fueled radio frequency ion thruster-Reference-Cited by-同舟云学术

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Performance of a 4 cm iodine-fueled radio frequency ion thruster

Published:2020-05-29 Issue:9 Volume:22 Page:094006
ISSN:1009-0630
Container-title:Plasma Science and Technology
language:
Short-container-title:Plasma Sci. Technol.

Author:

YANG Jinghua,JIA Shaoxia,ZHANG Zhenhua,ZHANG Xinghua,JIN Ting,LI Long,CAI Yong,CAI Jian

Funder

National Natural Science Foundation of China

Key Laboratory of microsatellite,Chinese Academy of Sciences

Publisher

IOP Publishing

Subject

Condensed Matter Physics

Link

https://iopscience.iop.org/article/10.1088/2058-6272/ab891d/pdf

Reference14 articles.

1. Propellant alternatives for ion and Hall effect thrusters

2. Iodine propellant for electric propulsion - To be or not to be

3. Performance Evaluation of an Iodine-Vapor Hall Thruster

Cited by 11 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. Performance investigation of a low-power Hall thruster fed on iodine propellant;Plasma Science and Technology;2024-06-01

2. Development of minimalistic propulsion system for university nanosatellite;IOP Conference Series: Materials Science and Engineering;2023-09-01

3. Iodine electron cyclotron resonance plasma source for electric propulsion;Acta Physica Sinica;2023

4. Development and validation of an iodine plasma model for gridded ion thrusters;Plasma Sources Science and Technology;2022-11-01

5. Charged-particles measurements in low-pressure iodine plasmas used for electric propulsion;Plasma Sources Science and Technology;2022-08-01

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