DocumentCode
2500157
Title
Plasma antenna with mercury filling used for aerospace vehicles
Author
Ovsyanikov, V.V. ; Ol´shevs´kiy, O.L. ; Popel´, V.M. ; Romanenko, Y.D. ; Moroz, S.N.
Author_Institution
Dniepropetrovsk Nat. Univ. named after O. Gonchar, Dniepropetrovsk, Ukraine
fYear
2012
fDate
17-21 Sept. 2012
Firstpage
167
Lastpage
169
Abstract
Results of account the effect of mercury vapor on the specific conductivity and relative permittivity of the plasma antenna are shown. The influence of mercury vapor on the efficiency of the plasma antenna is described.
Keywords
aircraft antennas; permittivity; plasma devices; aerospace vehicles; mercury filling; mercury vapor; plasma antenna; relative permittivity; specific conductivity; Antennas; Conductivity; Mercury (metals); Permittivity; Plasmas; Ultra wideband technology; Vehicles; Plasma antenna; aerospace vehicles antennas; conductivity and relative permeability of plasma; mercury vapor; the efficiency of antenna;
fLanguage
English
Publisher
ieee
Conference_Titel
Ultrawideband and Ultrashort Impulse Signals (UWBUSIS), 2012 6th International Conference on
Conference_Location
Sevastopol
Print_ISBN
978-1-4673-1940-9
Type
conf
DOI
10.1109/UWBUSIS.2012.6379768
Filename
6379768
Link To Document