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Recommended Practice for Use of ExB Probes in Electric Propulsion Testing An ExB probe is an electric propulsion plume diagnostic that has at its core a Wien filter. Ions entering the instrument experience perpendicular electric and magnetic fields, and opposing electric and magnetic forces, and are filtered based on their velocity. While the ExB probe can be used to estimate ion velocity distribution function, in the electric propulsion community, it is commonly used to measure plume current and species fractions. There are numerous probe designs, implementation and operation procedures, and data analysis approaches described and in use across the community. This paper provides recommendations and descriptions of best practices for design, implementation, and data analysis for the ExB probe, with a particular emphasis on Hall and Ion thrusters. This work contributes to the broader community goal to standardize the use of diagnostics in electric propulsion testing.
Document ID
20250008335
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Joshua L Rovey
(University of Illinois Urbana-Champaign Urbana, United States)
Toyofumi Yamauchi
(University of Illinois Urbana-Champaign Urbana, United States)
Wensheng Huang
(Glenn Research Center Cleveland, United States)
Robert E Thomas
(Glenn Research Center Cleveland, United States)
William J Hurley
(University of Michigan Ann Arbor, United States)
Shawn C Farnell
(Plasma Controls (United States) Fort Collins, United States)
Seth J Thompson
(Colorado State University Fort Collins, United States)
Cody C Farnell
(Plasma Controls (United States) Fort Collins, United States)
Casey C Farnell
(Plasma Controls (United States) Fort Collins, United States)
William P Brabston
(Georgia Institute of Technology Atlanta, United States)
Jason A Young
(The Aerospace Corporation El Segundo, United States)
Date Acquired
August 12, 2025
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
IEPC-2025-483
Meeting Information
Meeting: 39th International Electric Propulsion Conference (IEPC)
Location: London, England
Country: GB
Start Date: September 14, 2025
End Date: September 19, 2025
Sponsors: Electric Rocket Propulsion Society, American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80NSSC21K1118
WBS: 832911.01.22.06
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
electric propulsion
ExB probe
plasma plume
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