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- W2021964630 abstract "A preliminary evaluation of the performance characteristics of the 12-cm ring-cusp ion thruster with xenon propellant was made. Compared with past data, remarkable performance improvement was achieved by the modification of the magnetic field in the discharge chamber. According to numerical calculations of the magnetic field, these test results indicate a strong performance dependence on the discharge chamber boundary magnetic fields." @default.
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- W2021964630 date "1987-05-11" @default.
- W2021964630 modified "2023-09-27" @default.
- W2021964630 title "Performance characteristics of ring-cusp ion thruster" @default.
- W2021964630 doi "https://doi.org/10.2514/6.1987-1032" @default.
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