MICRO-THRUSTER

作品数：7被引量：6H指数：2
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相关期刊：《航空动力学报》《Chinese Physics B》《Transactions of Nanjing University of Aeronautics and Astronautics》《Plasma Science and Technology》更多>>
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Precision assessment of micro-thruster performance: A comparative study of indium field emission electric propulsion thrust measurement methods with a force-feedback pendulum
《Chinese Physics B》2025年第4期132-141,共10页Bo-Song Cai Yan Shen Yuan Zhong Jian-Ping Liu Yu-Qing Wang Zhu Li Liang-Cheng Tu Shan-Qing Yang 
Project supported by the National Key Research and Development Program of China(Grant No.2020YFC2201001);the Guangdong Major Project of Basic and Applied Basic Research(Grant No.2019B030302001);the National Natural Science Foundation of China(Grant Nos.12105373,12105374,and 11927812);the Science and Technology Research Project of Jiangxi Provincial Department of Education(Grant No.GJJ2402105).
Accurate thrust assessment is crucial for characterizing the performance of micro-thrusters.This paper presents a comprehensive evaluation of the thrust generated by a needle-type indium field emission electric propul...
关键词：MICRO-THRUSTER field emission thrust stand micro-thrust measurement calibration PENDULUM 
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