Extending service life of hall thrusters: recent progress and future challenges
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Link
http://link.springer.com/content/pdf/10.1007/s41614-019-0036-y.pdf
Reference165 articles.
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3. Ahedo E, Pablo VD (2007) Combined effects of electron partial thermalization and secondary emission in Hall thruster discharges. Phys. Plasma 14:083501. https://doi.org/10.1063/1.2749237
4. Ahedo E, Gallardo JM, Martinez-Sanchez M (2003) Effects of the radial plasma-wall interaction on the Hall thruster discharge. Phys. Plasma 10(8):3397–3409. https://doi.org/10.1063/1.1584432
5. A.L. Ortega, I.G. Mikellides, Investigations of pole erosion mechanisms in the 12.5 kW HERMeS Hall thruster using numerical simulations and ion velocity measurements. AIAA 2018-4647 (2018). https://doi.org/10.2514/6.2018-4647
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