An attitude model for the spacecraft of the ESA mission Gaia
A Review of Field Emission Cathode Technologies for Electric Propulsion Systems and Instruments
Army Pilot Emission Monitoring Program and Updating of State Emission Regulation Summary
Auroral kilometric radio emission in the period of quiet sun in 1996
Auroral kilometric radio emission in the period of quiet sun in 1996
Colloid micro-Newton thruster development for the ST7-DRS and LISA missions
Combined Chemical–Electric Propulsion for a Stand-Alone Mars CubeSat
Compact high voltage power conditioners for Field Emission Electric Propulsion (FEEP)
Development and coupling test of active spacecraft potential control – Next generation (ASPOC-NG)
Dual-telescope multi-channel thermal-infrared radiometer for outer planet fly-by missions
Effect of Low-Frequency Oscillation on Plasma Focusing in Krypton Hall Thruster
Emission Performance of Ionic Liquid Electrospray Thruster for Micropropulsion
Energy Harvesting on Spacecraft Using Electrodynamic Tethers
ESA Field Emission Electric Propulsion Program
Fault-Tolerant Station-Keeping on Libration Point Orbits
Features of downshifted maximum spectra during a dual-pump ionospheric heating experiment
Field emission characteristics of gold dust grains
Field emission electric propulsion: emission site distribution of slit emitters
Field Emission Electric Propulsion (FEEP) Attitude Control Capabilities
Field emission performance of multiwalled carbon nanotubes for a low-power spacecraft neutraliser
First demonstration of collision avoidance and orbit control for pico-satellites — UWE-4
Globalization extension of transient luminous events from FORMOSAT-2 observation
Ground-based and satellite DC-ULF electric field anomalies around Wenchuan M8.0 earthquake
High Power Orbit Transfer Vehicle
High voltage vacuum insulation: new horizons
Impact of surface properties on the dust grain charging
Intelligent on Board Control for Field Emission Electric Propulsion System
Iodine Electric Propulsion System Thrust Validation: From Numerical Modeling to In-Space Testing
Key factors controlling the real exhaust emissions from earthwork machines
Long-Duration Test of Coaxial Low-Energy Surface Flashover Ignitor
Metal Plasma Thruster for Small Satellites
Micro-Level Analysis of Marine Clay Stabilised with Polyurethane
Microthrust Propulsion of the LISA Mission
Molecular Dynamics Simulations of a Liquid Gallium Electrospray Thruster
Near Time-Minimal Earth to Transfers for Low-Thrust Spacecraft
On the cone-to-jet transition region and its significance in electrospray propulsion