Characterization of an ionic liquid electrospray thruster with a porous ceramic emitter  

作　　者：Chong CHEN Maolin CHEN Haohao ZHOU 陈冲;陈茂林;周浩浩(Combustion,Internal Flow and Thermal-Structure Laboratory,Northwestern Polytechnical University,Xi’an 710072,People’s Republic of China)

机构地区：[1]Combustion,Internal Flow and Thennal-Structure Laboratory,Northwestern Polytechnical University,Xi’an 710072,People’s Republic of China

出　　处：《Plasma Science and Technology》2020年第9期66-74,共9页等离子体科学和技术（英文版）

摘　　要：An ionic liquid(IL)electrospray thruster was developed for application in micro-nano satellites or gravitational wave detectors.The thruster employed a porous ceramic emitter with seven emitter strips located on its emission surface.Without any liquid-supply device,IL was delivered through porous media to emitter strips via capillary effect.Multiple emission sites then formed at the tip of each strip.A charged beam of up to 350μA(with a current density of 540μA cm^(-2))was stably produced in the negative mode.However,in the positive mode,a corona was observed which could prevent the thruster from emitting larger current.A time-of-flight mass spectrometer with significantly improved signal-to-noise ratio was built,which was used to obtain the mass distribution of the beam of the thruster.A retarding potential analysis was also performed.The test results showed that the thruster worked in the pure-ion regime,and delivered a maximum thrust of 67.1μN with specific impulses of 3952 s and 3117 s in the positive and negative modes,respectively.

关 键 词：electrospray thruster time-of-flight(TOF) retarding potential analysis(RPA) 

分 类 号：V439[航空宇航科学与技术—航空宇航推进理论与工程]