Back to Search Start Over

Verification of a Novel Electrospray Thruster with Magnetic Ionic liquid Propellant

Authors :
Guo Da-Wei
Cheng Mou-Sen
Li Xiao-Kang
Yang Yuntian
Source :
2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE).
Publication Year :
2021
Publisher :
IEEE, 2021.

Abstract

A new concept of magnetic ionic liquid electrospray thruster(ILET) is proposed in this paper. The thruster uses a lower working voltage with the action of an applied magnetic field, and is named as low-voltage ionic liquid electrospray thruster(LV-ILET). A jet needle is used as the emitter and the Helmholtz coil is used to apply an external magnetic field to demonstrate the working principle of the LV-ILET. The experimental results show that the stable working voltage could be reduced to 87% of that in absence of an applied magnetic field. Under the same working voltage, the applied magnetic field can significantly increase the emission current of LV-ILET. Due to the linear relationship between the thrust and the emission current, LV-ILET can either reduce the working voltage or increase the thrust with the help of the applied magnetic field and the magnetization characteristics of the propellant.

Details

Database :
OpenAIRE
Journal :
2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)
Accession number :
edsair.doi...........eb39f4895a7fdc9acc13fbe47449ee2f