Low Power Cylindrical Hall Thruster Performance and Plume Properties-Reference-Cited by-同舟云学术

Low Power Cylindrical Hall Thruster Performance and Plume Properties

Published:2008-07-21 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Diamant Kevin,Pollard James,Raitses Yevgeny,Fisch Nathaniel

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. 2Hruby,V.,Monheiser,J.,Pote,B.,Rostler,P.,Kolencik,J.,andFreeman,C."DevelopmentofLowPowerHallThrusters," AIAA 99-3534,30th Plasmadynamics andLasers Conference, Norfolk, VA, 28 June - 1July, 1999.

2. 3Warner, N.Z. and Martinez-Sanchez, M. "Design and Preliminary Testing of a Miniaturized TAL Hall Thruster," AIAA 2006-4994, 42nd Joint Propulsion Conference, Sacramento, CA,9-12July 2006.

3. 4Battista, F., DeMarco, E., Misuri, T., and Andrenucci, M. "A Review of the Hall Thruster Scaling Methodology," IEPC 2007-313, 30thInternationalElectric PropulsionConference, Florence, Italy,17-20September2007.

4. 5Belikov, M., Gorshkov, O., Dyshlyuk, E., Lovtzov, A., and Shagayda, A. "Development of Low-Power Hall Thruster with Lifetime up to 3000 Hours," IEPC 2007-129, 30thInternational Electric Propulsion Conference, Florence, Italy,17-20September 2007.

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