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.
Albani, M., Puggelli, F., Toccafondi, A., Meniconi, G., Scortecci, F. (2017). Modeling and dielectric characterization of EMI/EMC ground test for the evaluation of the electric propulsion thruster emissions. In 2017 IEEE Antennas and Propagation Society International Symposium, Proceedings (pp.2599-2600). New York : Institute of Electrical and Electronics Engineers Inc. [10.1109/APUSNCURSINRSM.2017.8073342].
Modeling and dielectric characterization of EMI/EMC ground test for the evaluation of the electric propulsion thruster emissions
Albani M.;Puggelli F.;Toccafondi A.;
2017-01-01
Abstract
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.
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https://hdl.handle.net/11365/1035032