rootbrowseIAC-22C4session 66. Electric Propulsion (2)Papers2. Cathode thermal environment simulator for experimental characterization of hollow cathode inserts3. Computational Analysis and Performance Evaluation of ILIS thruster with Experimental Results4. Development of Next Generation Active Spacecraft Potential Control (ASPOC-NG) Instrument for Science Missions5. Effects of magnetic nozzle geometry on ion and electron properties6. Experimental assessment of a MEMS surface DBD plasma actuator for active flow control in air-breathing space vehicles7. Experimental validation of the use of additive manufacturing and metaheuristic inverse design to develop an electrodeless plasma thruster8. Laser-induced Fluorescence Measurements for the Characterization of the Capacitively Coupled RF-Plasma Thruster C-STAR9. Multiscale Modelling of Alternative Propellants in Magnetically Enhanced Plasma Thrusters10. Plasma diagnostics and thrust performances of the Halo thruster with permanent magnets11. Advances in the development of a low mass low power high-flow regulation valve for satellite electric propulsion