An Experimental Investigation of Nonlinear Dissipation of Electromagnetic Waves in Inhomogeneous Collisionless Plasmas

Author(s):  
G. M. Batanov ◽  
V. A. Silin
2011 ◽  
Vol 109 (11) ◽  
pp. 114907
Author(s):  
Vijay Nalladega ◽  
Shamachary Sathish ◽  
Terry Murray ◽  
Eunsung Shin ◽  
Kumar V. Jata ◽  
...  

2013 ◽  
Vol 385-386 ◽  
pp. 1921-1926
Author(s):  
Yue Jun He ◽  
Bao Lin Ren ◽  
He Gang Xu ◽  
Wang Hua ◽  
Chun Heng Li

The water-based fog screen system for photoelectric interference, with low cost, energy-saving and environmental features, is a new type of interference material. This article describes and investigates the physical characteristics of the water-based fog screen, the principle behind the interference of visible light, infrared and other electromagnetic waves using mist, the composition of the water-based fog screen system and its significance in military applications.


1974 ◽  
Vol 27 (3) ◽  
pp. 319
Author(s):  
EL Bydder ◽  
BS Liley

The propagation properties of transverse electromagnetic waves in plasmas are discussed from the point of view of the 13-moment approximation. It is shown that additional modes, termed stress modes, should be able to propagate in a plasma even below the p


1957 ◽  
Vol 5 (2) ◽  
pp. 203-210 ◽  
Author(s):  
J. Crysdale ◽  
J. Day ◽  
W. Cook ◽  
M. Psutka ◽  
P. Robillard

2015 ◽  
Vol 64 (5) ◽  
pp. 055201
Author(s):  
Lin Min ◽  
Xu Hao-Jun ◽  
Wei Xiao-Long ◽  
Liang Hua ◽  
Zhang Yan-Hua

1997 ◽  
Vol 161 ◽  
pp. 761-776 ◽  
Author(s):  
Claudio Maccone

AbstractSETI from space is currently envisaged in three ways: i) by large space antennas orbiting the Earth that could be used for both VLBI and SETI (VSOP and RadioAstron missions), ii) by a radiotelescope inside the Saha far side Moon crater and an Earth-link antenna on the Mare Smythii near side plain. Such SETIMOON mission would require no astronaut work since a Tether, deployed in Moon orbit until the two antennas landed softly, would also be the cable connecting them. Alternatively, a data relay satellite orbiting the Earth-Moon Lagrangian pointL2would avoid the Earthlink antenna, iii) by a large space antenna put at the foci of the Sun gravitational lens: 1) for electromagnetic waves, the minimal focal distance is 550 Astronomical Units (AU) or 14 times beyond Pluto. One could use the huge radio magnifications of sources aligned to the Sun and spacecraft; 2) for gravitational waves and neutrinos, the focus lies between 22.45 and 29.59 AU (Uranus and Neptune orbits), with a flight time of less than 30 years. Two new space missions, of SETI interest if ET’s use neutrinos for communications, are proposed.


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