Experimental Study of the Acceleration Region in a 2 kW Hall Thruster-Reference-Cited by-同舟云学术

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Experimental Study of the Acceleration Region in a 2 kW Hall Thruster

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Raitses Yevgeny¹,Staack David¹,Dorf Leonid¹,Fisch Nathaniel¹

Affiliation:

1. Princeton University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5153

Reference25 articles.

1. Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters

2. D. Manzella, D. Jacobson, R. Jankovsky, AIAAPaper No. 2001-3774,37-thJoint Propulsion Conference and Exhibit, Salt Lake City, UT.

3. Y. Raitses, J. Ashkenazy, G. Appelbaum, AIAAPaper No. 1998-3640,34-thJoint Propulsion Conference and Exhibit, July13-15, 1998,Cleveland, OH.

Cited by 4 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. Plasma in Space Propulsion;Plasma Engineering;2018

2. Plasma in Space Propulsion;Plasma Engineering;2013

3. Laser Thomson Scattering Measurements of Electron Temperature and Density in the Near-Field Plume of a Hall-Effect Thruster;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

4. Numerical Simulations of a 2kW Hall Thruster;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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