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Recommended practice for use of emissive probes in electric propulsion testing

Research output: Contribution to journalReview articlepeer-review

Abstract

This article provides recommended methods for building, operating, and taking plasma potential measurements from electron-emitting probes in electric propulsion devices, including Hall thrusters, gridded ion engines, and others. The two major techniques, the floating point technique and the inflection point technique, are described in detail as well as calibration and error-reduction methods. The major heating methods are described as well as the various considerations for emissive probe construction. Special considerations for electric propulsion plasmas are addressed, including high-energy densities, ion flows, magnetic fields, and potential fluctuations. Recommendations for probe design and operation are provided.

Original languageEnglish (US)
Pages (from-to)614-637
Number of pages24
JournalJournal of Propulsion and Power
Volume33
Issue number3
DOIs
StatePublished - 2017

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Fuel Technology
  • Mechanical Engineering
  • Space and Planetary Science

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