Title :
Microwave measurements on a well-collimated dusty plasma sheet for communications blackout applications
Author :
Gillman, Eric D. ; Amatucci, Bill
Author_Institution :
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 weapons systems, 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. 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 relatively constant 170 Gauss axial magnetic field is produced by two electromagnet coils arranged in a Helmholtz configuration. This results in a well-collimated electron beam, producing a 2-dimensional Argon plasma discharge in a sheet configuration. This discharge sheet is approximately 40 cm long by 30 cm wide by 1 cm thick, and can produce electron 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. The electron beam is accelerated vertically towards a grounded beam dump electrode. This electrode is modified to include an array of six piezo buzzers modified and filled with alumina powder. When supplied with a modest voltage, the piezoelectric shakers uniformly drop dust particles into the plasma sheet discharge directly below at a constant rate, creating a dusty 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. Microwave cutoff, transmission, reflection, and scattering measurements of the plasma sheet are made in the S-band and X-band range. These measurements are relevant for applications related to communications blackout and over-the-horizon communications.
Keywords :
aircraft; dusty plasmas; electron beams; entry, descent and landing (spacecraft); microwave measurement; microwave propagation; plasma electromagnetic wave propagation; radiocommunication; space vehicles; 2D argon plasma discharge; Earth atmosphere; GPS; Helmholtz configuration; S-band range measurement; S-band signal reflection; X-band range measurement; alumina powder; argon gas; axial magnetic field; communications blackout applications; dense plasma layer; discharge sheet; dust particles; electromagnet coils; electron beam acceleration; electron beam discharge; electron density; grounded beam dump electrode; hypersonic velocity traveling vehicle; linear hollow cathode; magnetic flux density 170 gauss; microwave cutoff; microwave horn; microwave reflection; microwave scattering measurement; microwave transmission; over-the-horizon communications; piezo buzzers; piezoelectric shakers; plasma sheet discharge; pressure 50 mtorr to 150 mtorr; radio blackout; reentry; sheet configuration; signal attenuation; spacecraft; telemetry; vehicle navigation; voice communications; weapons systems; well-collimated dusty plasma sheet; well-collimated electron beam; Acceleration; Discharges (electric); Dusty plasmas; Electron beams; Microwave measurement; Vehicles;
Conference_Titel :
Radio Science Meeting (USNC-URSI NRSM), 2014 United States National Committee of URSI National
Conference_Location :
Boulder, CO
Print_ISBN :
978-1-4799-3119-4
DOI :
10.1109/USNC-URSI-NRSM.2014.6928104