Discharge Chamber Performance of the NEXIS Ion Thruster-Reference-Cited by-同舟云学术

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Discharge Chamber Performance of the NEXIS Ion Thruster

Published:2004-06-21 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Goebel Dan¹,Polk J.¹,Sengupta A.¹

Affiliation:

1. Jet Propulsion Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3813

Reference15 articles.

1. Simulated ion thruster operation without beam extraction

2. 4J.Brophy,"NASA'sDeepSpace1IonEngine",Rev.Sci.Instrum.73(2002)p.1071-1078

3. 5JohnR.Beattie,"XIPSKeepsSatellitesonTrack",TheIndustrialPhysicist,June1998.

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2. Systematic low-thrust trajectory design to Mars based on a full Ephemeris modeling;Advances in Space Research;2019-12

3. Axial Ring-Cusp Hybrid (ARCH) plasma discharge: an approach to highly efficient miniature-scale ion sources;Plasma Sources Science and Technology;2018-12-21

4. Ion engine grids: Function, main parameters, issues, configurations, geometries, materials and fabrication methods;Chinese Journal of Aeronautics;2018-08

5. Design of Miniature Ring-Cusp Ion Thrusters via Analysis of Discharge EEDF and Plasma Parameter Mapping;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

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