微推力器是实现空间引力波探测中无拖曳控制任务的关键. 本文在分析空间引力波探测无拖曳
控制系统对微推力器要求基础上, 通过微推进技术原理开展分析, 梳理出了满足要求的微推力器 …

Ionic liquid electrospray thrusters are capable of producing microNewton precision thrust at
a high thrust–power ratio but have yet to demonstrate lifetimes that are suitable for most …

Performance and lifetime analysis of electrospray thrusters requires accurate knowledge of
the mass and charge distributions of the plume. Mass flux and current density distributions …

Electrospray thrusters were first operated in space in 2015 as the technology demonstration
of the Colloid MicroNewton Thrusters (CMNTs), developed by Busek Co., Inc. and NASA Jet …

Electrospray thruster life and mission performance are strongly influenced by grid
impingement, the extent of which can be correlated with emission modes that occur at …

Abstract Machine learning models are applied to simulated electrospray particle data to
investigate plume dynamics from emission to final particle properties. A limited set of final …

Abstract The University of California, Los Angeles (UCLA) Plasma, Energy, & Space
Propulsion Laboratory (PESPL) presents the Discrete Electrospray Lagrangian Interaction …

View Video Presentation: https://doi. org/10.2514/6.2021-3439. vid Multimode propulsion is
the combination of two or more propulsive modes into a system that shares a single …

II. Introduction lectrospray thrusters are a highly scalable form of electric propulsion with a
wide range of specific impulse capabilities. In 2015, such thrusters first demonstrated in …

As an application of electrospray, electrospray thrusters are preferred to work in a steady
electrohydrodynamic mode to output high-precision and adjustable thrust through …