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- W2083977431 abstract "Inert gas tests are conducted with several magnetoelectrostatic containment discharge chamber geometries. The configurations tested include three discharge chamber lengths; three boundary magnet patterns; two different flux density magnet materials; hemispherical and conical shaped thrusters having different surface-to-volume ratios; and two and three grid ion optics. Argon mass utilizations of 60 to 79% are attained at 210 to 280 eV/ion in different test configurations. Short hemi thruster configurations are found to produce 70 to 92% xenon mass utilization at 185 to 220 eV/ion." @default.
- W2083977431 created "2016-06-24" @default.
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- W2083977431 date "1981-04-21" @default.
- W2083977431 modified "2023-09-25" @default.
- W2083977431 title "Magnetoelectrostatic thruster physical geometry tests" @default.
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- W2083977431 doi "https://doi.org/10.2514/6.1981-753" @default.
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