Research of thrust measurement for space electric propulsion

doi:10.16708/j.cnki.1000-758X.2022.0033

Abstract

Abstract: Accurate measurement of thrust is very important in the development and planning of space electric propulsion.In recent years,with the increasing of complexity and task difficulty for electric propulsion,higher requirements are put forward for the evaluation techniques and methods of thrust performance.In response to this demand,a review of the thrust measurement for space electric propulsion was presented.Measurement methods and the underlying mechanisms,technical features and applications were covered.The methods of thrust measurement can be divided into direct measurement and indirect measurement.The former mainly includes balance structure,torsional pendulum,suspension and inverted pendulum,while the latter mainly includes target and cantilever beam.The advantages and disadvantages of these measurement methods were summarized and compared,which provided a reference for developers to design the thrust measuring system.The key problems in the five segments including system design,system calibration,system response,system response measurement and calculation of thrust during the process of thrust measurement were described in detail,and the corresponding improvement methods were proposed.To serve as a reference for future thrust measurement research,suggestions were also provided by considering the development trend of electric propulsion and its demand of thrust measurement.

Key words: electric propulsion, propulsion thrust measurement, direct measurements, indirect measurement, review

ZHANG Lupeng, YANG Xin, CHANG Lei, XU Qian, ZHOU Haishan, LUO Guangnan. Research of thrust measurement for space electric propulsion[J]. Chinese Space Science and Technology, 2022, 42(3): 25-38.

0
/ / Recommend

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: http://journal26.magtechjournal.com/kjkxjs/EN/10.16708/j.cnki.1000-758X.2022.0033

http://journal26.magtechjournal.com/kjkxjs/EN/Y2022/V42/I3/25

[1]	WU Chenchen, GENG Hai, WANG Zitong, LI Detian. Development of advanced electric propulsion technology for cislunar and deep space exploration [J]. Chinese Space Science and Technology, 2023, 43(5): 13-23.
[2]	XIN Zhiping, GU Zhiru, WANG Chao, JIANG Yuanda, HU Jiusong. Digital design of power processing unit for ion electric propulsion system [J]. Chinese Space Science and Technology, 2023, 43(3): 73-80.
[3]	LIU Qi, MAO Wei, HU Peng, WEI Yanming, HU Yanlin, LI Yong, BIAN Bingxiu, LIU Xuhui. Application and development of high-precision Hall electric propulsion technology [J]. Chinese Space Science and Technology, 2023, 43(2): 1-15.
[4]	ZHANG Yuanzhe, HAN Xianwei, YANG Zhenyu, LU Haifeng, TAN Chang. Ion beam characteristics of iodine RF ion thruster optical system [J]. Chinese Space Science and Technology, 2022, 42(6): 115-124.
[5]	ZHOU Xiaotao, MA Xiaofei, LI Huanxiao. Review of flexible tensioned thin-film deployable antennas [J]. Chinese Space Science and Technology, 2022, 42(4): 77-91.
[6]	WANG Jue, WANG Min, GUO Tingting, ZHONG Xiaoqing, WEN Zheng, WEI Xin. Feasibility study of spacecraft gravity center offset compensation by intentional xenon temperature control [J]. Chinese Space Science and Technology, 2022, 42(2): 39-45.
[7]	LIU Hui, WANG Shangsheng, YU Daren, ZHAO Mingxuan, ZHENG Siyuan, CHEN Ye. Newton electric propulsion system for space gravitational wave detection [J]. Chinese Space Science and Technology, 2021, 41(5): 10-20.
[8]	HU Jianfeng, YANG Jungang, XIAO Yong, WAN Xiaoping, FENG Tao, WANG Yong, ZHENG Bing. Dynamic simulation of the deployment process of super large loop antenna belt [J]. Chinese Space Science and Technology, 2021, 41(5): 50-56.
[9]	CHEN Xinwei, GU Zuo, GAO Jun, GUO Ning, WANG Shangmin, ZHAO Yong, FENG Jie, SHI Kai, PU Yangxu, LI He. Experimental research on discharge characteristics of LHT40 low power Hall thruster [J]. Chinese Space Science and Technology, 2021, 41(5): 65-74.
[10]	YAN Nengwen, GUO Ning, WU Chenchen, GU Zengjie, YANG Zhaolun. Research on RF-ion thruster based on discharge chamber uniform model [J]. Chinese Space Science and Technology, 2021, 41(3): 1-8.
[11]	GENG Hai, SUN Mingming, LUO Junhua, LIU Jiatao. Study on the thermal radiation influence of the sputtering target on the ion thruster [J]. Chinese Space Science and Technology, 2021, 41(2): 10-18.
[12]	WU Qinqin, LIU Xinyu, DENG Hanwen, KANG Xiaoming. Research status and prospect of chemical-electrospray dual-mode propulsion system [J]. Chinese Space Science and Technology, 2021, 41(1): 1-12.
[13]	YANG Sanxiang, LIU Chao, WANG Shangmin, FENG Jie, CHEN Juanjuan, WU Chenchen, JIA Yanhui, GUO Ning, GENG Hai . Numerical study of electromagnetic acceleration mechanism for pulsed plasma thruster [J]. Chinese Space Science and Technology, 2020, 40(4): 11-21.
[14]	CHEN Jie, KANG Xiaolu, ZHAO Zhen, CHENG Jiabing, LIANG Wei. High specific impulse Hall thruster startup characteristics [J]. Chinese Space Science and Technology, 2020, 40(4): 22-28.
[15]	DUAN Chuanhui, REN Lixin, CHANG Yajie, BAI Qian, AN Ran, HUANG Yusong. All electric propulsion satellite trajectory optimization by homotopic approach [J]. Chinese Space Science and Technology, 2020, 40(2): 42-.

Research of thrust measurement for space electric propulsion

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments