Non-Intrusive Plasma Diagnostics

Photo showing the X2 thruster and collection optics during a recent time-averaged LIF test.

project personnel
Zach Brown, Ethan Dale

previous personnel
Marcel Georgin, Matthew Byrne, Christopher Durot, Wensheng Huang, Tim Smith

project sponsors
Air Force Research Laboratory

There is a need to develop non-intrusive, time-resolved diagnostics to study short timescale dynamics in electric thrusters and improve modeling and simulation of the physical processes at work in thrusters. Hall effect thrusters (HETs) exhibit many high-frequency plasma oscillations. Particularly of interest is the breathing mode oscillation at tens of kilohertz, which strongly influences the ion distribution function and therefore thruster operation. The focus of this effort is on measuring how the ions evolve during the oscillation in order to better understand how the confinement of plasma is changed by the breathing mode. In addition, many other thruster concepts, such as the pulsed inductive thruster (PIT) and the field-reversed-configuration (FRC) thruster, have an explicitly pulsed nature and time-resolved diagnostics are necessary for understanding their plume dynamics. To this end, PEPL is working to develop a time-resolved laser induced fluorescence (LIF) system to measure ion velocity distribution as a function of time resolved to microsecond or smaller scales.

Traditional (time-averaged) LIF is performed at PEPL by chopping a laser on the order of kilohertz and using a lock-in amplifier to remove noise and amplify the signal. Since the signal is weak, a relatively long time constant is used and effectively averages out oscillations. The time-resolved system will modulate the laser at high-frequency using an acousto-optical modulator and acquire data with a lock-in system that has capability to acquire data with fine time resolution and either average over individual time bins only or average in the frequency domain. The details of this system are currently being investigated.

Selected Publications

  • The Use of Laser-Induced Fluorescence to Characterize Discharge Cathode Erosion in a 30cm Ring-Cusp Ion Thruster

    Williams, G. J.

    University of Michigan, Ph.D. Dissertation, 2000

  • Deconvolution of Ion Velocity Distributions from Laser-Induced Fluorescence Spectra of Xenon Electrostatic Thruster Plumes

    Smith, T. B

    University of Michigan, Ph.D. Dissertation, 2003

  • Magnetic Field Simulation and Mapping Based on Zeeman-split Laser-induced Fluorescence Spectra of Xenon in the Discharge Channel of 5-6 kW Coaxial Stationary-Plasma Hall Thrusters

    Ngom, B. B

    University of Michigan, Ph.D. Dissertation, 2009

  • Study of Hall Thruster Discharge Channel Wall Erosion via Optical Diagnostics

    Huang, W.

    University of Michigan, Ph.D. Dissertation, 2011

  • Development of a Time-Resolved Laser-Induced Fluorescence Technique for Nonperiodic Oscillations

    Durot, C.

    University of Michigan, Ph.D. Dissertation, 2016

  • Non-invasive time-resolved measurements of anomalous collision frequency in a Hall thruster

    E.T. Dale and B.A. Jorns

    Physics of Plasmas, Vol. 26, Issue 1, 013516, 2019

  • Non-invasive in situ measurement of the near-wall ion kinetic energy in a magnetically shielded Hall thruster

    Cusson, Sarah E.

    Plasma Sources Science and Technology, Vol. 28 No. 10, 21 October 2019