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

被引:38
作者
Dale, Ethan T. [1 ]
Jorns, Benjamin A. [1 ]
机构
[1] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
关键词
ELECTRIC PROPULSION; PLASMA MEASUREMENTS; MODEL; OSCILLATIONS;
D O I
10.1063/1.5077008
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
The time-resolved cross-field electron anomalous collision frequency in a Hall thruster is inferred from minimally invasive laserbased measurements. This diagnostic is employed to characterize the relationship between the dominant low-frequency "breathing" oscillations and anomalous electron transport mechanisms. The ion Boltzmann equation combined with a generalized Ohm's law is used to infer key quantities including the ionization rate and axial electric field strength which are necessary in computing the total electron cross-field collision frequency. This is accomplished by numerically integrating functions of velocity moments of the ion velocity distribution function measured with laser-induced fluorescence, in conjunction with current density measurements at a spatial boundary. Estimates of neutral density are used to compute the classical collision frequency profile and the difference in the total collision frequency, and this quantity describes the anomalous collision frequency. This technique reveals the anticipated trends in electron transport: few collisions in the acceleration region but a collision frequency approaching the cyclotron frequency farther downstream. The time-resolved transport profiles indicate that the anomalous collision frequency fluctuates by several orders of magnitude during a breathing cycle. At troughs in the discharge current, classical collisions may dominate; at peaks in the discharge current, anomalous collisions dominate. These results show that the breathing mode and electron transport are directly correlated. This finding is discussed with regard to existing numerical models for the breathing mode and interpretations of anomalous electron transport. Published under license by AIP Publishing.
引用
收藏
页数:12
相关论文
共 41 条
  • [1] Study of stationary plasma thrusters using two-dimensional fully kinetic simulations
    Adam, JC
    Héron, A
    Laval, G
    [J]. PHYSICS OF PLASMAS, 2004, 11 (01) : 295 - 305
  • [2] [Anonymous], 2008, FUNDAMENTALS ELECT P
  • [3] Critical assessment of a two-dimensional hybrid Hall thruster model: Comparisons with experiments
    Bareilles, J
    Hagelaar, GJM
    Garrigues, L
    Boniface, C
    Boeuf, JP
    Gascon, N
    [J]. PHYSICS OF PLASMAS, 2004, 11 (06) : 3035 - 3046
  • [4] Tutorial: Physics and modeling of Hall thrusters
    Boeuf, Jean-Pierre
    [J]. JOURNAL OF APPLIED PHYSICS, 2017, 121 (01)
  • [5] Low frequency oscillations in a stationary plasma thruster
    Boeuf, JP
    Garrigues, L
    [J]. JOURNAL OF APPLIED PHYSICS, 1998, 84 (07) : 3541 - 3554
  • [6] Laser-induced fluorescence measurements of acceleration zone scaling in the 12.5 kW HERMeS Hall thruster
    Chaplin, Vernon H.
    Jorns, Benjamin A.
    Ortega, Alejandro Lopez
    Mikellides, Ioannis G.
    Conversano, Ryan W.
    Lobbia, Robert B.
    Hofer, Richard R.
    [J]. JOURNAL OF APPLIED PHYSICS, 2018, 124 (18)
  • [7] Plasma oscillations in Hall thrusters
    Choueiri, EY
    [J]. PHYSICS OF PLASMAS, 2001, 8 (04) : 1411 - 1426
  • [8] A two-dimensional (azimuthal-axial) particle-in-cell model of a Hall thruster
    Coche, P.
    Garrigues, L.
    [J]. PHYSICS OF PLASMAS, 2014, 21 (02)
  • [9] Cusson S. E., 2017, P 35 INT EL PROP C, VIEPC-2017-239
  • [10] Recommended Practice for Pressure Measurement and Calculation of Effective Pumping Speed in Electric Propulsion Testing
    Dankanich, John W.
    Walker, Mitchell
    Swiatek, Michael W.
    Yim, John T.
    [J]. JOURNAL OF PROPULSION AND POWER, 2017, 33 (03) : 668 - 680