Axial Ring-Cusp Hybrid (ARCH) plasma discharge: an approach to highly efficient miniature-scale ion sources

被引:7
|
作者
Dankongkakul, Ben [1 ]
Wirz, Richard E. [2 ]
机构
[1] ERC Inc, Air Force Res Lab, Edwards AFB, CA 93524 USA
[2] Univ Calif Los Angeles, 420 Westwood Plaza, Los Angeles, CA 90064 USA
来源
PLASMA SOURCES SCIENCE & TECHNOLOGY | 2018年 / 27卷 / 12期
关键词
ion thrusters; cusp confinement; simulated discharge; ion sources; ring-cusp; CROSS-SECTIONS; CUBESATS;
D O I
10.1088/1361-6595/aae63c
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 miniaturization of conventional direct-current ion sources is predominantly restricted by efficiency limitations associated with the increased surface area-to-volume ratio of smaller-scale discharge chambers-reducing the effective confinement length of the high-energy 'primary' electrons that is necessary for efficient plasma generation. The Axial Ring-Cusp Hybrid (ARCH) plasma discharge addresses this scaling limitation by using a new approach that combines magnetic and electrostatic confinement to decouple the primary and plasma electrons loss mechanisms. Simulated ion thruster performance measurements show that the ARCH discharge may be capable of achieving a discharge loss and a propellant mass utilization of 175 eV/ion and 0.87, respectively. These estimates are supported by full internal maps of the plasma properties, including the electron energy distribution function, inside the discharge chamber. The measurements show highly effective confinement of the primary electrons, high average plasma electron temperatures of similar to 5 eV, and low plasma sheath potential relative to the anode- attributes generally found only in efficient conventional-scale discharges with good overall plasma confinement. As such, the new ARCH discharge design approach may allow miniature ion thrusters to achieve the performance and efficiency levels similar to those of highly efficient conventional ion thrusters.
引用
收藏
页数:10
相关论文
共 5 条
  • [1] Miniature ion thruster ring-cusp discharge performance and behavior
    Dankongkakul, Ben
    Wirz, Richard E.
    [J]. JOURNAL OF APPLIED PHYSICS, 2017, 122 (24)
  • [2] Plasma Structure of Miniature Ring-Cusp Ion Thruster Discharges
    Mao, Hann-Shin
    Wirz, Richard E.
    Goebel, Dan M.
    [J]. JOURNAL OF PROPULSION AND POWER, 2014, 30 (03) : 628 - 636
  • [3] Magnetic confinement in a ring-cusp ion thruster discharge plasma
    Sengupta, Anita
    [J]. JOURNAL OF APPLIED PHYSICS, 2009, 105 (09)
  • [4] REDUCTION OF PLASMA LOSS TO DISCHARGE CHAMBER WALLS IN A RING-CUSP ION-THRUSTER
    ARAKAWA, Y
    HAMATANI, C
    [J]. JOURNAL OF PROPULSION AND POWER, 1987, 3 (01) : 90 - 91
  • [5] Revealing the plasma confinement behavior of an axial ring cusp hybrid discharge in a miniature ion thruster using PIC/MCC simulation
    Liu, Wei
    Wang, Weizong
    Li, Yifei
    Xue, Shuwen
    [J]. PLASMA SOURCES SCIENCE & TECHNOLOGY, 2023, 32 (08):