Causality analysis of vacuum chamber facility effects for Hall effect thruster operation

S Seth J. Thompson (Colorado State University 1 Department of Mechanical Engineering, , Fort Collins, Colorado 80523,) K Kentaro Hara (Stanford University 2 Department of Aeronautics and Astronautics, , Stanford, California 94305,) J Janice D. Cabrera (School of Aerospace Engineering, Georgia Institute of Technology 3 , Atlanta, Georgia 30332,) M Mitchell L. R. Walker (School of Aerospace Engineering, Georgia Institute of Technology 3 , Atlanta, Georgia 30332,) J John D. Williams

Abstract

Characterization of plasma dynamics is critical for controlling electric propulsion systems on spacecraft. Understanding the causal relations between measurement data can play an important role both in minimizing the number of diagnostics and in informing which dynamic information needs to be accounted for in a computational model. In this paper, we apply extended convergent cross mapping (eCCM) to three measured telemetry signals—cathode current, discharge voltage, and cathode-to-ground voltage—collected from a krypton-fed magnetically shielded Hall-effect thruster with base operating pressures of 6.8 and 8.5 μTorr at the 4.5 and 6 kW power levels, respectively. Data were also collected at elevated pressures, two to three times the base operating pressure. We discuss the sensitivity of the cross-mapping skill to the embedding parameters and background pressure in the vacuum chamber. We propose eCCM as a framework for characterizing dynamic relationships in the Hall-effect thruster circuit, guiding the selection of signals and the prioritization of dynamic measurements in subsequent physics-based modeling and diagnostic efforts. The results show that cross-mapping skill decreases across nearly all signal pairs for both power levels, indicating a reduction in mutual dynamic information between electrical circuit components as background pressure increases. The analysis suggests that the discharge plasma is coupled to other unmeasured components in the system as the facility pressure varies.

Article Details

Volume / Issue Vol. 140, Issue 7
Published August 21, 2026
ISSN 0021-8979
Publisher American Institute of Physics

Journal Info

Journal of Applied Physics

American Institute of Physics

ISSN: 0021-8979 Physical Sciences

Authors (5)

S

Seth J. Thompson

Colorado State University 1 Department of Mechanical Engineering, , Fort Collins, Colorado 80523,

K

Kentaro Hara

Stanford University 2 Department of Aeronautics and Astronautics, , Stanford, California 94305,

J

Janice D. Cabrera

School of Aerospace Engineering, Georgia Institute of Technology 3 , Atlanta, Georgia 30332,

M

Mitchell L. R. Walker

School of Aerospace Engineering, Georgia Institute of Technology 3 , Atlanta, Georgia 30332,

J

John D. Williams