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Krypton charge exchange cross sections for Hall effect thruster models

机译:霍尔效应推进器模型的charge电荷交换截面

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Following discharge from a Hall effect thruster, charge exchange occurs between ions and un-ionized propellant atoms. The low-energy cations produced can disturb operation of onboard instrumentation or the thruster itself. Charge-exchange cross sections for both singly and doubly charged propellant atoms are required to model these interactions. While xenon is the most common propellant currently used in Hall effect thrusters, other propellants are being considered, in particular, krypton. We present here guided-ion beam measurements and comparisons to semiclassical calculations for Kr+?+?Kr and Kr2+?+?Kr cross sections. The measurements of symmetric Kr+?+?Kr charge exchange are in good agreement with both the calculations including spin-orbit effects and previous measurements. For the symmetric Kr2+?+?Kr reaction, we present cross section measurements for center-of-mass energies between 1?eV and 300?eV, which spans energies not previously examined experimentally. These cross section measurements compare well with a simple one-electron transfer model. Finally, cross sections for the asymmetric Kr2+?+?Kr?→?Kr+?+?Kr+ reaction show an onset near 12?eV, reaching cross sections near constant value of 1.6 ?2 with an exception near 70–80?eV.
机译:从霍尔效应推进器放电后,离子与未电离的推进剂原子之间发生电荷交换。产生的低能阳离子会干扰车载仪表或推进器本身的运行。需要对单电荷和双电荷推进剂原子的电荷交换横截面进行建模。氙气是目前在霍尔效应推进器中使用的最常见的推进剂,但其他推进剂,尤其是k也被考虑在内。我们在这里介绍离子束的测量以及与Kr + ?+?Kr和Kr 2 + ?+?Kr横截面的半经典计算的比较。对称的Kr + ?+?Kr电荷交换的测量结果与包括自旋轨道效应的计算结果和先前的测量结果都非常吻合。对于对称的Kr 2 + α+ΔKr反应,我们给出了质心能量在1?eV和300?eV之间的横截面测量值,该值跨越了以前未经实验检验的能量。这些横截面测量值与简单的单电子转移模型相比非常好。最后,非对称Kr 2 + ?+?Kr?→?Kr + ?+?Kr + 反应的横截面显示出一个接近12?eV,达到接近于1.6? 2 的恒定值的横截面,但接近70–80?eV。

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