Development of direct thrust measurement system for the completely electrodeless helicon plasma thruster

被引：0
|
作者：
机构：
[1] Kuwahara, Daisuke
[2] Koyama, Yushi
[3] Otsuka, Shuhei
[4] Ishii, Takamichi
[5] Ishii, Hiroki
[6] Fujitsuka, Hiroaki
[7] Waseda, Shimpei
[8] Shinohara, Shunjiro
来源：
| 1600年 / Japan Society of Plasma Science and Nuclear Fusion Research卷 / 09期
关键词：
Pendulums;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [31] Development of an SPT-100VT Stationary Plasma Thruster with Increased Thrust
    Kim, V. P.
    Gnizdor, R. Yu.
    Grdlichko, D. P.
    Zakharchenko, V. S.
    Korkunov, M. V.
    Merkurev, D. V.
    Popov, G. A.
    Shilov, E. A.
    COSMIC RESEARCH, 2019, 57 (05) : 301 - 309
  • [32] Experimental study of a low-thrust measurement system for thruster ground tests
    Gong, Jingsong
    Hou, Lingyun
    Zhao, Wenhua
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2014, 85 (03):
  • [33] Calibration methods for the simultaneous measurement of the impulse, mass loss, and average thrust or a pulsed plasma thruster
    Yoshikawa, T.
    Tsukizaki, R.
    Kuninaka, H.
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2018, 89 (09):
  • [34] Design of a Current Measurement System in a Plasma Thruster with Rogowski Coil
    De Alessandro, R. O.
    Velez Ibarra, M. D.
    Brito, H. H.
    IEEE LATIN AMERICA TRANSACTIONS, 2013, 11 (01) : 119 - 125
  • [35] Direct thrust measurements of 2U-sized bi-directional wave plasma thruster
    Shumeiko, Andrei I.
    Telekh, Victor D.
    AIP ADVANCES, 2023, 13 (08)
  • [36] System design study of a VLEO satellite platform using the IRS RF helicon-based plasma thruster
    Herdrich, G.
    Papavramidis, K.
    Maier, P.
    Skalden, J.
    Hild, F.
    Beyer, J.
    Pfeiffer, M.
    Fugmann, M.
    Klinker, S.
    Fasoulas, S.
    Souhair, N.
    Ponti, F.
    Walther, M.
    Wiegand, A.
    Walpot, L.
    Duesmann, B.
    Borras, E. B.
    Roberts, P. C. E.
    Crisp, N. H.
    ACTA ASTRONAUTICA, 2024, 215 : 245 - 259
  • [37] Development of hot gap measurement system for the ion thruster optics
    Yuan J.
    Liang D.
    Zhou S.
    Xiao S.
    Li X.
    Yang J.
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2020, 42 (01): : 51 - 58
  • [38] Development and Testing of a Helicon Plasma Thruster Based on a Magnetically Enhanced Inductively Coupled Plasma Reactor Operating in a Multi-Mode Regime
    Andreescu, Anna-Maria Theodora
    Crunteanu, Daniel Eugeniu
    Teodorescu, Maximilian Vlad
    Danescu, Simona Nicoleta
    Cancescu, Alexandru
    Stoicescu, Adrian
    Paraschiv, Alexandru
    APPLIED SCIENCES-BASEL, 2024, 14 (18):
  • [39] Direct Measurement of Axial Momentum Imparted by an Electrothermal Radiofrequency Plasma Micro-Thruster
    Charles, Christine
    Boswell, Roderick W.
    Bish, Andrew
    Khayms, Vadim
    Scholz, Edwin F.
    FRONTIERS IN PHYSICS, 2016, 4
  • [40] Simultaneous experimental verification of indirect thrust measurement method based on Hall-effect thruster and plasma plume
    Zhang, Zhongkai
    Zhang, Zun
    Wang, Yimeng
    Zhang, Guangchuan
    Qi, Jiayun
    Liu, Jiubin
    Tang, Haibin
    Cao, Jinbin
    VACUUM, 2022, 204
12345