Near Discharge Cathode Assembly Plasma Potential Measurements in a 30-cm NSTAR-type Ion Engine Admist Beam Extraction

Author:

Herman Daniel1,Gallimore Alec1

Affiliation:

1. University of Michigan

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. Polk, J. E., etal, "An Overview of the Results from an 8200 Hour Wear Test of the NSTAR Ion Thruster," AIAA Paper #99-2446,35thAIAA/ASME/SAE/ASEEJointPropulsionConference,LosAngeles,CA,June1999.

2. Domonkos, M. T., Foster, J. E., Patterson, M. J. "Investigation of Keeper Erosion in the NSTAR Ion Thruster," IEPC Paper No. 01-308,27thInternationalElectricPropulsionConference,Pasadena,CA,Oct.2001.

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. Particle Based Plasma Simulations for an Ion Engine Discharge Chamber;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

2. Erosion Processes of the Discharge Cathode Assembly of Ring-Cusp Gridded Ion Thrusters;37th AIAA Plasmadynamics and Lasers Conference;2006-06-05

3. Hollow Cathode and Keeper-Region Plasma Measurements;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

4. Discharge Chamber Plasma Structure of a 30 cm NSTAR-type Ion Engine;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

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