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Ion species fractions in the far-field plume of a high-specific impulse Hall thruster

Publication ,  Conference
Hofer, RR; Gallimore, AD
Published in: 39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit
January 1, 2003

An ExB probe was used to measure the ion species fractions of Xe+, Xe2+, and Xe3+ in the farfield plume of the NASA-173Mv2 laboratory-model Hall thruster. The thruster was operated at a constant xenon flow rate of 10 mg/s and discharge voltages of 300-900 V. The ExB probe was placed two meters downstream of the thruster exit plane on the thruster centerline. At a discharge voltage of 300 V, the species fractions of Xe2+ and Xe3+ were lower, but still consistent with, previous Hall thruster studies using other mass analyzers. Over discharge voltages of 300-900 V, the Xe2+ species fractions increased from 0.04 to 0.12 and the Xe3+ species fraction increased from 0.01 to 0.02. © 2003 by the American Institute of Aeronautics and Astronautics, Inc.

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Published In

39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit

DOI

Publication Date

January 1, 2003
 

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Hofer, R. R., & Gallimore, A. D. (2003). Ion species fractions in the far-field plume of a high-specific impulse Hall thruster. In 39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit. https://doi.org/10.2514/6.2003-5001
Hofer, R. R., and A. D. Gallimore. “Ion species fractions in the far-field plume of a high-specific impulse Hall thruster.” In 39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit, 2003. https://doi.org/10.2514/6.2003-5001.
Hofer RR, Gallimore AD. Ion species fractions in the far-field plume of a high-specific impulse Hall thruster. In: 39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit. 2003.
Hofer, R. R., and A. D. Gallimore. “Ion species fractions in the far-field plume of a high-specific impulse Hall thruster.” 39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit, 2003. Scopus, doi:10.2514/6.2003-5001.
Hofer RR, Gallimore AD. Ion species fractions in the far-field plume of a high-specific impulse Hall thruster. 39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit. 2003.

Published In

39th AIAA ASME SAE ASEE Joint Propulsion Conference and Exhibit

DOI

Publication Date

January 1, 2003