Thermal model of LIPS-200 ring-cusp magnet field ion thruster

被引：0
|
作者：
Sun, Ming-Ming [1 ]
Zhang, Tian-Ping [1 ]
Chen, Juan-Juan [1 ]
Long, Jian-Fei [1 ]
Wu, Xian-Ming [1 ]
机构：
[1] National Key Laboratory of Vacuum and Cryogenic Technology on Physics, Lanzhou Institute of Physics, Lanzhou,730000, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2015年 / 36卷 / 08期
关键词：
19;
D O I：
10.13675/j.cnki.tjjs.2015.08.023
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1274 / 1280
相关论文
共 47 条
  • [21] Erosion processes of the discharge cathode assembly of ring-cusp gridded ion thrusters
    Gallimore, Alec D.
    Rovey, Joshua L.
    Herman, Daniel A.
    JOURNAL OF PROPULSION AND POWER, 2007, 23 (06) : 1271 - 1278
  • [22] Comparative Study of Two Types of Cusp Field Ion Thruster
    Zhao Y.-D.
    Li J.-P.
    Zhang T.-P.
    Jiang H.-C.
    Wang L.
    Guo D.-Z.
    Yang W.
    Tuijin Jishu/Journal of Propulsion Technology, 2021, 42 (11): : 2633 - 2640
  • [23] Numerical Analysis of Magnetic and Plasma Characteristics of the DC Ring Cusp Discharge Ion Thruster
    Ranasinghe, Naveen Deshan
    Wijesiriwardana, R.
    2021 12TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE), 2021, : 28 - 36
  • [24] Axial Ring-Cusp Hybrid (ARCH) plasma discharge: an approach to highly efficient miniature-scale ion sources
    Dankongkakul, Ben
    Wirz, Richard E.
    PLASMA SOURCES SCIENCE & TECHNOLOGY, 2018, 27 (12):
  • [25] Effect of a permanent-magnet-induced cusp field on a magnetic nozzle radio frequency plasma thruster
    Nakahama, Yugo
    Takahashi, Kazunori
    AIP ADVANCES, 2024, 14 (01)
  • [26] Sufficient cusp field generated by permanent magnet for compact ECR ion source
    Rashid, MH
    Bhandari, RK
    INDIAN JOURNAL OF PHYSICS, 2004, 78 (09) : 955 - 959
  • [27] The effect of magnet core size on the performance of a cylindrical Hall thruster with the near-anode cusp magnetic field
    Gao, Yuanyuan
    Wang, Weizong
    Hu, Peng
    Yu, Daren
    VACUUM, 2022, 206
  • [28] ELECTRON-CYCLOTRON-RESONANCE PLASMA GENERATION USING A PLANAR RING-CUSP MAGNETIC-FIELD AND A REENTRANT COAXIAL CAVITY
    YASUI, T
    TAHARA, H
    YOSHIKAWA, T
    JOURNAL OF VACUUM SCIENCE & TECHNOLOGY A-VACUUM SURFACES AND FILMS, 1995, 13 (04): : 2105 - 2109
  • [29] Performance and discharge characteristics of Applied-Field MPD thruster in accordance with ring magnet position
    Shin, Haewon
    Chai, Kil-Byoung
    Kim, Holak
    VACUUM, 2024, 230
  • [30] SIMPLE PERFORMANCE-MODEL FOR RING AND LINE CUSP ION THRUSTERS
    BROPHY, JR
    WILBUR, PJ
    AIAA JOURNAL, 1985, 23 (11) : 1731 - 1736
12345