Improved Control Architecture and Strategy for Iodine Ion Thruster following In-Orbit Demonstration and System-Level Radiation Testing
Concept analysis of a distributed thrust system, a novel inductive propulsion method using high energy pulse solenoids in satellite swarms for reusable interorbital freight transport
Enabling direct kinetic simulation of dense plasma plume expansion for laser ablation plasma thrusters
Simulations of Xenon Beam Ions Emitted from Electric Thrusters in Earth's Magnetosphere
Control Algorithm for 6 kW Hall Thruster
Experimental Investigation of an External Discharge Very Low Power (
Molecular Dynamics Studies of Ionic Liquid-Surface Interactions for Electrospray Thrusters
Air Ionization in Self-Neutralizing Air-Breathing Plasma Thruster
Resolving multi-dimensional plasma phenomena in Hall thrusters using the reduced-order particle-in-cell scheme
High Angle Mass Flux of an Electrospray Plume