Budget Amount *help |
¥4,160,000 (Direct Cost: ¥3,200,000、Indirect Cost: ¥960,000)
Fiscal Year 2019: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2018: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2017: ¥1,690,000 (Direct Cost: ¥1,300,000、Indirect Cost: ¥390,000)
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Outline of Final Research Achievements |
Hall thruster is one of the electric propulsion systems that generate a high-density plasma. It has been hypothesized that the azimuthally inhomogeneous plasma property distribution affects the magnetized electron flow. In this research, a Hall thruster was operated with an azimuthally nonuniform propellant supply, and the plasma property distribution was measured with a high-resolution probe measurement experiment. In addition, a plasma flow simulation revealed the electron flow characteristics under the azimuthal inhomogeneity.
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