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Investigation on the ion evolution in different ionization states inside the electrode channel of the micro-cathode arc thruster by time-resolved optical image and emission spectroscopy

  • Lu Wang
  • , Xi Ming Zhu*
  • , Tian Yuan Ji
  • , Hai Xing Wang
  • , Yang Zhao
  • , Hao Yan
  • , Xu Hui Liu
  • , Mao Wei Mao
  • , Li Qiu Wei
  • , Da Ren Yu
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • CAS - Beijing Institute of Control Engineering

Research output: Contribution to journal › Article › peer-review

Abstract

Micro-cathode arc thrusters (μ-CAT) hold critical applications in the national economy, serving as primary propulsion systems for orbit maintenance and formation flying missions of small satellites. Compared to steady-state thrusters (e.g., Hall thrusters or ion thrusters), the performance and lifetime of the μ-CAT depend on the ablation state of the cathode. However, it is challenging to characterize ablation-driven plasma properties due to the lack of a method to determine the time-resolved metal ion densities from cathode ablation during single-pulse discharge. In this work, we present an OES method to determine the Ti+ and Ti2+ ion densities based on ionic lines from different ionization states, and observe the “three-stage evolution” of the plasma inside the electrode channel of the micro-cathode arc thruster with capacitive discharge mode based on the high-speed imaging subsystem. The time-resolved Ti+ and Ti2+ ion densities during the interelectrode plasma and the early stage of the anode spot period are determined by synchronously triggering the power processing unit of the μ-CAT and optical emission spectroscopy subsystem. Besides, the impulse bit during a single pulse is obtained, supported by the determined ion densities and time-of-flight ion velocity monitoring method. Our method will help improve the engineering test efficiency and accelerate the design and development of the μ-CAT.

Original languageEnglish
Pages (from-to)313-327
Number of pages15
JournalActa Astronautica
Volume240
DOIs
StatePublished - Mar 2026

Keywords

  • Impulse bit
  • Micro-cathode arc thruster
  • Optical image and emission spectroscopy
  • Ti and Ti ion densities

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