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The Effects of Nude Faraday Probe Design and Vacuum Facility Backpressure on the Measured Ion Current Density Profile of Hall Thruster Plumes

Authors :
Alec D. Gallimore
Mitchell L. R. Walker
Richard R. Hofer
Source :
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Publication Year :
2002
Publisher :
American Institute of Aeronautics and Astronautics, 2002.

Subjects

Subjects :
Engineering
business.industry
law
Mechanical engineering
business
Faraday cage
Ion current density
Engineering physics
Hall effect thruster
law.invention

Details

Database :
OpenAIRE
Journal :
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Accession number :
edsair.doi...........396ea0e551be85f7cd4cfc241d92bcfa
Full Text :
https://doi.org/10.2514/6.2002-4253
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