Title :
Microparticle injection effects on microwave transmission through an overly dense plasma layer
Author :
Gillman, Eric D. ; Amatucci, Bill
Author_Institution :
U.S. Naval Res. Lab., Washington, DC, USA
Abstract :
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.
Keywords :
Langmuir probes; alumina; argon; dusty plasmas; electron density; plasma boundary layers; plasma density; plasma devices; plasma magnetohydrodynamics; space vehicles; terrestrial atmosphere; 2-dimensional Argon plasma discharge; Ar; Argon gas; Earth´s atmosphere; GPS; Gauss axial magnetic field; Helmholtz configuration; Langmuir probe measurements; S-band microwave incident transmission; S-band signals; alumina microparticles; alumina powder; dense plasma sheet; discharge sheet; dusty plasma layer; electromagnet coils; electromagnetic signals; electron attachment; electron beam discharge; flux rate; free electron density; frequency bands; hypersonic vehicles; hypersonic velocities; intense plasma layer; linear hollow cathode; low pressure background; mesh openings; microparticle injection; microwave transmission; overly dense plasma layer; plasma cutoff frequency; plasma density; plasma sheet discharge; plasma transparency; powder density; pressure 50 mtorr to 150 mtorr; radio blackout; receiving horn; shaker device; size 100 cm; size 2 cm; size 30 cm; spacecraft reentry; telemetry; transmitting microwave horn; vehicle navigation; vibrating motor; voice communications; Cathodes; Electron beams; Plasmas; Vibrations;
Conference_Titel :
Plasma Sciences (ICOPS) held with 2014 IEEE International Conference on High-Power Particle Beams (BEAMS), 2014 IEEE 41st International Conference on
Conference_Location :
Washington, DC
Print_ISBN :
978-1-4799-2711-1
DOI :
10.1109/PLASMA.2014.7012471