Development and coupling test of active spacecraft potential control – Next generation (ASPOC-NG)
A Review of Field Emission Cathode Technologies for Electric Propulsion Systems and Instruments
Emission Performance of Ionic Liquid Electrospray Thruster for Micropropulsion
Near Time-Minimal Earth to Transfers for Low-Thrust Spacecraft
Long-Duration Test of Coaxial Low-Energy Surface Flashover Ignitor
Combined Chemical–Electric Propulsion for a Stand-Alone Mars CubeSat
Temporally and Spatially Resolved Spectroscopic Measurements of Plasma-Actuator Thermal Properties
Fault-Tolerant Station-Keeping on Libration Point Orbits
Plume Composition Measurements of a High-Emission-Density Electrospray Thruster
Colloid micro-Newton thruster development for the ST7-DRS and LISA missions
Recommended Practice for Use of Faraday Probes in Electric Propulsion Testing
Molecular Dynamics Simulations of a Liquid Gallium Electrospray Thruster
Metal Plasma Thruster for Small Satellites
Micro-Level Analysis of Marine Clay Stabilised with Polyurethane
Plasma Catalysis for Enhanced-Thrust Single Dielectric Barrier Discharge Plasma Actuators