Experiment Study on the Plasma Parameters Measurement in Backflow Region of Ion Thruster

The charge-exchange xenon (CEX) ion generated by ion thruster can backflow to the surface of spacecraft and threaten to the safety of spacecraft operation. In order to evaluate the effects of the induced plasma environment in backflow regions on the spacecraft, we designed a spherical single Langmuir probe of 5.8cm in diameter for measuring low-density plasma parameters in backflow region of ion thruster. In practice, the tests are performed in a two-dimensional array (40cm×60cm) composed of 20 sites. The experiment results illustrate that the electron temperature ranges from 3.71eV to 3.96eV, with the mean value of 3.82eV and the standard deviation of 0.064eV. The electron density ranges from 8.30×1012/m3 to 1.66×1013/m3, with the mean value of 1.30×1013/m3 and the standard deviation of 2.15×1012/m3. All data is analyzed according to the “ideal" plasma conditions of Maxwellian distributions.

• Tian Kai
• Yang Sheng-sheng
• Li De-tian
• Miao Yu-jun
• Xue Yu-xiong Wang Yi
• Yan Ze-dong
• Ma Ya-li
• ZHuang Jian-hong

• Langmuir Probe
• Plasma parameters
• Ion thruster
• Backflow region.

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