Hall Effect Thruster with an ALN chamber

被引:0
|
作者
Barral, S [1 ]
Jayet, Y
Véron, E
Mazouffre, S
Echegut, P
Dudeck, A
机构
[1] Polish Acad Sci, Inst Fundamental Technol Res, Swietokrzyska 21, PL-00049 Warsaw, Poland
[2] CNRS, Lab dAerothermique, F-45071 Orleans, France
[3] CNRS, Centre Recherche Materiaux Hautes Temperature, F-45071 Orleans, France
来源
PLASMA 2005 | 2006年 / 812卷
关键词
Hall thruster; AIN; erosion;
D O I
暂无
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 potential of AlN as a material for Hall thruster channels is assessed on the basis of actual thruster performances, computer simulations of the discharge and microscopy studies of an eroded channel. Comparison of experimental and numerical data provides further evidence that secondary electron emission (SEE) is the main phenomena responsible for wall-induced currents. The high discharge currents observed are characteristic for high SEE materials and result in a much lower thruster efficiency than with a conventional BN-SiO2 channel. The delivered thrust is also affected in the medium voltage range. With respect to erosion, scanning electron images performed after 14 hours of operation already reveal precursors of anomalous erosion patterns on the channel front side.
引用
收藏
页码:427 / +
页数:2
相关论文
共 50 条
  • [1] Technique to Collimate Ions in a Hall-Effect Thruster Discharge Chamber
    Xu, Kunning G.
    Walker, Mitchell L. R.
    JOURNAL OF PROPULSION AND POWER, 2011, 27 (03) : 564 - 572
  • [2] Role of a Conducting Vacuum Chamber in the Hall Effect Thruster Electrical Circuit
    Frieman, Jason D.
    King, Scott T.
    Walker, Mitchell L. R.
    Khayms, Vadim
    King, David
    JOURNAL OF PROPULSION AND POWER, 2014, 30 (06) : 1471 - 1479
  • [3] Preionization of buffer chamber in ATON Hall thruster
    Liu Hui
    Wu Bo-Ying
    E Peng
    Duan Ping
    ACTA PHYSICA SINICA, 2010, 59 (10) : 7203 - 7208
  • [4] Computation of neutral gas flow from a hall thruster into a vacuum chamber
    Boyd, LD
    Cai, CP
    Walker, MLR
    Gallimore, AD
    RAREFIED GAS DYNAMICS, 2003, 663 : 541 - 548
  • [5] Neutral density map of Hall thruster plume expansion in a vacuum chamber
    Walker, MLR
    Gallimore, AD
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2005, 76 (05):
  • [6] Effect of Magnetic Field in the ATON-type Hall Thruster Buffer Chamber on Discharge Current Characteristics
    Han, Ke
    Yu, Daren
    E, Peng
    Wei, Liqiu
    Ji, Yanchao
    Jiang, Binhao
    ICEMS 2008: PROCEEDINGS OF THE 11TH INTERNATIONAL CONFERENCE ON ELECTRICAL MACHINES AND SYSTEMS, VOLS 1- 8, 2008, : 940 - +
  • [7] The Effect of Pressure on the Plume Divergence in the Hall Thruster
    Cohen-Zur, Avi
    Fruchtman, Amnon
    Gany, Alon
    IEEE TRANSACTIONS ON PLASMA SCIENCE, 2008, 36 (05) : 2069 - 2081
  • [8] Optimized atom injection in a Hall effect thruster
    Garrigues, L
    Hagelaar, GJM
    Boniface, C
    Boeuf, JP
    APPLIED PHYSICS LETTERS, 2004, 85 (22) : 5460 - 5462
  • [9] Effect of the Discharge Voltage on the Performance of the Hall Thruster
    Duan Ping
    Liu Guangrui
    Bian Xingyu
    Chen Long
    Yin Yan
    Cao Anning
    PLASMA SCIENCE & TECHNOLOGY, 2016, 18 (04) : 382 - 387
  • [10] Thermal stability of the krypton Hall effect thruster
    Szelecka, Agnieszka
    Kurzyna, Jacek
    Bourdain, Loic
    NUKLEONIKA, 2017, 62 (01) : 9 - 15