Preliminary Investigation of an External Discharge Plasma Thruster-Reference-Cited by-同舟云学术

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Preliminary Investigation of an External Discharge Plasma Thruster

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
language:
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Author:

Karadag Burak,Cho Shinatora,Oshio Yuya,Hamada Yushi,Funaki Ikkoh,Komurasaki Kimiya

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4951

Reference30 articles.

1. Mission advantages of constant power, variable Isp electrostatic thrusters

2. Wall material effects in stationary plasma thrusters. I. Parametric studies of an SPT-100

Cited by 5 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. Experimental investigation of an external discharge very low anode power (< 20 W) hall thruster;Journal of Electric Propulsion;2022-10-03

2. Experimental Investigation of an External Discharge Very Low Power (<20W) Hall Thruster;2022-08-17

3. Design and Application of an Argon-fed 1 A-class Plasma Bridge Neutralizer;2022 IEEE 5th International Electrical and Energy Conference (CIEEC);2022-05-27

4. Rotating spoke instabilities in a wall-less Hall thruster: simulations;Plasma Sources Science and Technology;2019-04-24

5. Thrust performance, propellant ionization, and thruster erosion of an external discharge plasma thruster;Journal of Applied Physics;2018-04-21

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