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NUCLEAR TECHNIQUES, Volume. 47, Issue 5, 050010(2024)

Thrust measurement methods for electric propulsion based on flexible beam structure

Luoqi WANG1,2, Jinxing ZHENG2、*, Haiyang LIU2, Fei LI3, Dongdong MENG3,4, Yudong LU2, Yifan DU1,2, Zhuoyao TANG1,2, Tao WU1,2, and Jiaming SHI2
Author Affiliations
  • 1University of Science and Technology of China, Hefei 230026, China
  • 2Hefei Institutes of Physical Science, Chinese Academy of Sciences, Hefei 230031, China
  • 3State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
  • 4School of Mechanical Engineering and Energy Engineering, Beijing University of Technology, Beijing 100124, China
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    [6] LI Yifei, FU Chencong, CAI Guobiao et al. Global model co-simulation of RF ion thruster based on multi-physical field coupling[J]. Transactions of China Electrotechnical Society, 36, 3113-3123(2021).

    [7] Grubišić A N, Gabriel S B. Development of an indirect counterbalanced pendulum optical-lever thrust balance for micro- to millinewton thrust measurement[J]. Measurement Science and Technology, 21, 105101(2010).

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    [9] Xu K G, Walker M L R. High-power, null-type, inverted pendulum thrust stand[J]. The Review of Scientific Instruments, 80, 055103(2009).

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    [12] NING Zhongxi, FAN Jinrui. On line measurement method of three-wire torsion pendulum micro thrust and analysis of its uncertainty[J]. Measurement & Control Technology, 31, 45-48(2012).

    [13] YANG Juan, LIU Xianchuang, WANG Yuquan et al. Thrust measurement of an independent microwave thruster propulsion device with three-wire torsion pendulum thrust measurement system[J]. Journal of Propulsion Technology, 37, 362-371(2016).

    [14] LI Detian, ZHANG Weiwen, ZHANG Tianping et al. Ground integrated test and evaluation technology for space electric propulsion[J]. Vacuum and Cryogenics, 23, 266-273(2017).

    [15] Yanagi R, Kimura I. New type of target for the measurement of impulse bits of pulsed plasma thrusters[J]. Journal of Spacecraft and Rockets, 19, 246-249(1982).

    [16] Takao Y, Eriguchi K, Ono K. A miniature electrothermal thruster using microwave-excited microplasmas: thrust measurement and its comparison with numerical analysis[J]. Journal of Applied Physics, 101, 123307(2007).

    [17] Ding Y J, Fan H T, Ma D et al. Extending service life of Hall thrusters: recent progress and future challenges[J]. Reviews of Modern Plasma Physics, 3, 15(2019).

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    [19] Squire J P, Carter M D, Chang Diaz F R et al. Advances in duration testing of the VASIMR®VX-200SS™System[C], 4950(2016).

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    Luoqi WANG, Jinxing ZHENG, Haiyang LIU, Fei LI, Dongdong MENG, Yudong LU, Yifan DU, Zhuoyao TANG, Tao WU, Jiaming SHI. Thrust measurement methods for electric propulsion based on flexible beam structure[J]. NUCLEAR TECHNIQUES, 2024, 47(5): 050010

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    Paper Information

    Category: Research Articles

    Received: Mar. 15, 2024

    Accepted: --

    Published Online: Jul. 8, 2024

    The Author Email: ZHENG Jinxing (郑金星)

    DOI:10.11889/j.0253-3219.2024.hjs.47.050010

    Topics

    laser devices and laser physics
    Lasers and Laser Optics
    Laser physics
    laser manufacturing
    Instrumentation, Measurement and Metrology