A new EMI test facility for electric propulsion (EP) thrusters has been developed at Aerospazio Tecnologie. The facility consists of a cylindrical dielectric vacuum tank placed in a semi-Anechoic room, connected through a gate valve to a Large Vacuum Test Facility. The electromagnetic characterisation of the facility, along with subsequent measures of the radiated emissions of a Hall effect thruster, is presented.
|Titolo:||Modeling and dielectric characterization of EMI/EMC ground test for the evaluation of the electric propulsion thruster emissions|
|Appare nelle tipologie:||4.1 Contributo in Atti di convegno|