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Microparticle injection effects on microwave transmission through an overly dense plasma layer

机译:微粒注入对通过过密等离子体层的微波传输的影响

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Summary form only given. Vehicles traveling at hypersonic velocities within the Earth's atmosphere, such as spacecraft during reentry and other hypersonic vehicles, are enveloped by a dense plasma layer. This plasma layer reflects and significantly attenuates GPS and S-band signals for vehicle navigation, telemetry, and voice communications, resulting in radio blackout.Injecting microparticles into a plasma discharge will reduce the free electron density via electron attachment to particles. Reducing the free electron density lowers the plasma cutoff frequency, and may allow lower frequency bands of electromagnetic signals to penetrate the plasma layer. In these studies, a linear hollow cathode produces an electron beam that is accelerated into a low pressure (50 to 150 mTorr) background of Argon gas, producing an electron beam discharge. A 170 Gauss axial magnetic field produced by two electromagnet coils in a Helmholtz configuration results in a well-collimated electron beam, producing a 2dimensional Argon plasma discharge. This discharge sheet is approximately 100 cm long by 30 cm wide by 2 cm thick, at densities as high as 1012 cm-3. The plasma sheet is intended to mimic the intense plasma layer produced and experienced by vehicles traveling at hypersonic velocities. A shaker device with fine mesh on the bottom is filled with alumina powder and fitted with a vibrating motor. When supplied with a modest voltage, the vibration drops alumina microparticles from the mesh openings, into the plasma sheet discharge, creating a dusty plasma. Varying the voltage supplied to the vibrating motor varies the flux rate and density of powder dropped into the plasma. A transmitting microwave horn is oriented normal to the dense plasma sheet while the receiving horn is mounted on a stage that can be rotated up to 180 degrees azimuthally. Results from these experiments measuring the cutoff and transmission of S-band microwaves incident on a dusty plasma layer, as well as Langmu- r probe measurements assessing microparticle effects on plasma density and transparency are reported.
机译:仅提供摘要表格。以高超音速在地球大气层中行驶的飞行器,例如重返过程中的航天器以及其他高超音速飞行器,被密集的等离子层包围。该等离子层反射并显着衰减了用于车辆导航,遥测和语音通信的GPS和S波段信号,从而导致无线电中断。将微粒注入等离子放电将通过电子附着到粒子上来降低自由电子密度。降低自由电子密度降低了等离子体截止频率,并且可以允许电磁信号的较低频带穿透等离子体层。在这些研究中,线性空心阴极产生电子束,该电子束被加速到氩气的低压(50至150 mTorr)背景下,从而产生电子束放电。两个Helmholtz构造的电磁线圈产生的170高斯轴向磁场导致准直的电子束产生二维氩气等离子体放电。该放电片长约100cm,宽30cm,厚2cm,密度高达1012cm-3。等离子片旨在模仿以高超声速行驶的车辆产生并经历的强烈等离子层。底部有细孔的振动筛装置装有氧化铝粉末,并装有振动电机。当施加适度的电压时,振动会使氧化铝微粒从筛孔掉落到等离子薄片放电中,从而产生多尘的等离子。改变提供给振动电动机的电压,会改变通入等离子体的粉末的通量率和密度。发射微波喇叭的方向垂直于致密的等离子体片,而接收喇叭则安装在可以旋转多达180度的平台上。这些实验的结果报告了测量入射在多尘等离子体层上的S波段微波的截止和传输,以及评估微粒对等离子体密度和透明度影响的Langmur探针测量结果。

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