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Observations of single-pass ion cyclotron heating in a trans-sonic flowing plasma

机译:超声速流动等离子体中单程离子回旋加速器加热的观察

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The VAriable Specific Impulse Magnetoplasma Rocket (VASIMR (R)) is a high power electric spacecraft propulsion system, capable of I-sp/thrust modulation at constant power [F. R. Chang Diacuteaz , Proceedings of the 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 8-11 Jan. 2001]. The VASIMR (R) uses a helicon discharge to generate plasma. This plasma is energized by an rf booster stage that uses left hand polarized slow mode waves launched from the high field side of the ion cyclotron resonance. In the experiments reported in this paper, the booster uses 2-4 MHz waves with up to 50 kW of power. This process is similar to the ion cyclotron heating (ICH) in tokamaks, but in the VASIMR (R) the ions only pass through the resonance region once. The rapid absorption of ion cyclotron waves has been predicted in recent theoretical studies. These theoretical predictions have been supported with several independent measurements in this paper. The single-pass ICH produced a substantial increase in ion velocity. Pitch angle distribution studies showed that this increase took place in the resonance region where the ion cyclotron frequency was roughly equal to the frequency on the injected rf waves. Downstream of the resonance region the perpendicular velocity boost should be converted to axial flow velocity through the conservation of the first adiabatic invariant as the magnetic field decreases in the exhaust region of the VASIMR (R). This paper will review all of the single-pass ICH ion acceleration data obtained using deuterium in the first VASIMR (R) physics demonstrator machine, the VX-50. During these experiments, the available power to the helicon ionization stage increased from 3 to 20+ kW. The increased plasma density produced increased plasma loading of the ICH coupler. Starting with an initial demonstration of single-pass ion cyclotron acceleration, the experiments demonstrate significant improvements in coupler efficiency and in ion heating efficiency. In deuterium plasma, >= 80% efficient absorption of 20 kW of ICH input power was achieved. No clear evidence for power limiting instabilities in the exhaust beam has been observed.
机译:可变比冲磁极火箭(VASIMR(R))是一种高功率电动航天器推进系统,能够以恒定功率[F]进行I-sp /推力调制。 R. Chang Diacuteaz,第39届AIAA航空航天科学会议论文集和展览,内华达州里诺,2001年1月8-11日。 VASIMR(R)使用螺线管放电产生等离子体。射频增强级为该等离子体提供能量,该增强级使用从离子回旋共振的高场侧发射的左手极化慢模式波。在本文报道的实验中,助推器使用2-4 MHz的波,功率高达50 kW。此过程类似于托卡马克中的离子回旋加速器加热(IC​​H),但在VASIMR(R)中,离子仅通过一次共振区域。在最近的理论研究中已经预测了离子回旋波的快速吸收。这些理论预测得到了本文中若干独立测量的支持。单程ICH大大提高了离子速度。螺距角分布研究表明,这种增加发生在共振区域,在该区域中离子回旋加速器频率大致等于注入的rf波的频率。在VASIMR(R)的排气区域中,磁场减小时,应通过保留第一绝热不变性,将共振速度的下游垂直速度提升转换为轴向流速。本文将回顾第一台VASIMR(R)物理演示机VX-50中使用氘获得的所有单次ICH离子加速数据。在这些实验中,螺旋电离阶段的可用功率从3 kW增加到20+ kW。升高的血浆密度导致ICH耦合器的血浆负荷增加。从单程离子回旋加速器的初步演示开始,实验证明了耦合器效率和离子加热效率的显着提高。在氘等离子体中,实现了20kW ICH输入功率的> = 80%有效吸收。没有观察到明显的证据证明排气束中的功率限制不稳定性。

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