Design improvements and experimental measurements of BURFIT-80 RF ion thruster

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American Institute of Aeronautics and Astronautics Inc, AIAA

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info:eu-repo/semantics/closedAccess

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BURFIT-80, a prototype radio-frequency ion thruster, is designed, built and tested at the Bogazici University Space Technologies Laboratory. This paper presents the design parameters and numerous design improvements of this thruster. Three different versions of the thruster, with the same discharge chamber inner diameter of 80 mm, have been built and tested. The latest vesion of this prototype thruster presents significant improvements of the DC electrical connections to the grids and RF electrical connections to the RF antenna. For the second version of the thruster, plume ion energy distribution measurements are conduted using an indigenously developed retarding potential analyzer, and some of the measurement results are presented.

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53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017 -- 10 July 2017 through 12 July 2017 -- Atlanta -- 195549

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Antennas; Electric connectors; Ion propulsion; Ions; Design improvements; Design parameters; Discharge chamber; Electrical connection; Ion energy distributions; Radio frequency ion thrusters; Retarding potential analyzer; Space technologies; Ion engines

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53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017

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