Operating mode investigation of a laboratory stationary plasma thruster-Reference-Cited by-同舟云学术

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Operating mode investigation of a laboratory stationary plasma thruster

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Bechu S.¹,Perot C.¹,Gascon N.¹,Lasgorceix P.¹,Hauser A.¹,Dudeck M.¹

Affiliation:

1. CNRS, Lab. d'Aerothermique, Orleans, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2567

Reference21 articles.

1. echnology of Closed-Drift Thrusters', H. R. Kauhan, AIAA-83-1398, Seattle, Wash.,June 1983.

2. RGD, 26-31July 98

3. H., Zhurin, V., Kozubsky, K., IEPC-93-093,

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1. Plasma in Space Propulsion;Plasma Engineering;2018

2. Mode Transitions in Hall-Effect Thrusters Induced by Variable Magnetic Field Strength;Journal of Propulsion and Power;2016-07

3. Effect of Segmented Electrode Length on the Performances of an Aton-Type Hall Thruster;Plasma Science and Technology;2016-04-29

4. Sheath oscillation characteristics and effect on near-wall conduction in a krypton Hall thruster;Physics of Plasmas;2014-11

5. The Performance and Wear Characterization of a High-Power High-Isp NASA Hall Thruster;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

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