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Field emission
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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
Recommended Practice for Thrust Measurement in Electric Propulsion Testing
Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing
On the cone-to-jet transition region and its significance in electrospray propulsion
Field emission electric propulsion: emission site distribution of slit emitters
Parametric Angles of Trajectory Determined Field Line Intersects
ESA Field Emission Electric Propulsion Program
Thrust Measurements of the Gaia Mission Flight-Model Cold Gas Thrusters
Compact high voltage power conditioners for Field Emission Electric Propulsion (FEEP)
High voltage vacuum insulation: new horizons
Intelligent on Board Control for Field Emission Electric Propulsion System
Microthrust Propulsion of the LISA Mission
Field Emission Electric Propulsion (FEEP) Attitude Control Capabilities
First demonstration of collision avoidance and orbit control for pico-satellites — UWE-4
Potential Modulations on SCATHA (Spacecraft Charging at High Altitude) Spacecraft
Key factors controlling the real exhaust emissions from earthwork machines
Army Pilot Emission Monitoring Program and Updating of State Emission Regulation Summary
Energy Harvesting on Spacecraft Using Electrodynamic Tethers
Small Satellite Electro-Optical System (EOS) Technological and Commercial Expansion
Globalization extension of transient luminous events from FORMOSAT-2 observation
An attitude model for the spacecraft of the ESA mission Gaia
High Power Orbit Transfer Vehicle