Ionic liquid electrospray behavior in a hybrid emitter electrospray thruster

Zhang, JR; Cai, GBA; Shahzad, A; Liu, XH; Wang, WZ

Wang, WZ (corresponding author), Beihang Univ, Sch Astronaut, Adv Space Prop & Energy Lab ASPEL, Beijing 100191, Peoples R China.; Wang, WZ (corresponding author), Minist Educ, Key Lab Spacecraft Design Optimizat & Dynam Simul, Beijing 100191, Peoples R China.

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2021; 175 ():

Abstract

Electrospray thrusters are most suitable for micro-nano satellites in advantage of small size, low power consumption and high specific impulse. Howeve......

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