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  • session 6
  • 6. Electric Propulsion (2)

    Papers

    2. Cathode thermal environment simulator for experimental characterization of hollow cathode inserts

    3. Computational Analysis and Performance Evaluation of ILIS thruster with Experimental Results

    4. Development of Next Generation Active Spacecraft Potential Control (ASPOC-NG) Instrument for Science Missions

    5. Effects of magnetic nozzle geometry on ion and electron properties

    6. Experimental assessment of a MEMS surface DBD plasma actuator for active flow control in air-breathing space vehicles

    7. Experimental validation of the use of additive manufacturing and metaheuristic inverse design to develop an electrodeless plasma thruster

    8. Laser-induced Fluorescence Measurements for the Characterization of the Capacitively Coupled RF-Plasma Thruster C-STAR

    9. Multiscale Modelling of Alternative Propellants in Magnetically Enhanced Plasma Thrusters

    10. Plasma diagnostics and thrust performances of the Halo thruster with permanent magnets

    11. Advances in the development of a low mass low power high-flow regulation valve for satellite electric propulsion