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Discharge Chamber Plasma Structure of a 30-cm NSTAR-Type Ion Engine

机译:30厘米NSTAR型离子发动机的放电室等离子体结构

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摘要

Single Langmuir probe measurements are presented over a two-dimensional array of locations in the near Discharge Cathode Assembly (DCA) region of a 30-cm diameter ring cusp ion thruster over a range of thruster operating conditions encompassing the high-power half of the NASA throttling table. The Langmuir probe data were analyzed with two separate methods. All data were analyzed initially assuming an electron population consisting of Maxwellian electrons only. The on-axis data were then analyzed assuming both Maxwellian and primary electrons. Discharge plasma data taken with beam extraction exhibit a broadening of the higher electron temperature plume boundary compared to similar discharge conditions without beam extraction. The opposite effect is evident with the electron/ion number density as the data without began, extraction appears to be more collimated than the corresponding data with beam extraction. Primary electron energy and number densities are presented for one operating condition giving an order of magnitude of their value and the error associated with this calculation.
机译:朗格缪尔探测器的单个测量结果显示在直径30厘米的环形尖头离子推进器的近放电阴极组件(DCA)区域中的二维位置阵列上,该推进器在包括NASA高功率一半的推进器工作条件范围内节流表。用两种单独的方法分析了Langmuir探针数据。最初假设仅由麦克斯韦电子组成的电子种群进行了分析。然后假设麦克斯韦电子和一次电子都对轴上数据进行了分析。与不使用束提取的类似放电条件相比,使用束提取获得的放电等离子体数据显示出更高的电子温度羽流边界变宽。对于电子/离子数密度,相反的效果是明显的,因为没有开始的数据,提取似乎比带有束提取的相应数据更加准直。给出了一种工作条件下的一次电子能量和数密度,给出了其值的数量级以及与此计算相关的误差。

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