DocumentCode
386999
Title
The plasmas of rocket flight
Author
Balwanz, W.
Author_Institution
U.S. Naval Research Laboratory, Washington, DC, USA
Volume
9
fYear
1966
fDate
21-25 March 1966
Firstpage
3
Lastpage
9
Abstract
The plasmas attending a rocket in flight vary widely in charge density and size depending upon the source of the plasma and the altitude of operation. Such a plasma, i.e., a medium containing equal numbers of positive and negative charge so that it is electrically neutral in its totality, interacts with electromagnetic signals causing reflection, refraction and absorption. The solution of problems encountered in communicating through such a plasma depend upon a knowledge of its electrical properties. The complexity of the interaction requires that approximate solutions be used. A judicious application of the results of laboratory, flight and theoretical studies are required to enable the successful design of communication links. Extended theoretical and experimental studies are required to enable designs of communication systems for the space ship of the future.
Keywords
Communication systems; Electromagnetic reflection; Electromagnetic refraction; Electromagnetic wave absorption; Laboratories; Plasma applications; Plasma density; Plasma properties; Plasma sources; Rockets;
fLanguage
English
Publisher
ieee
Conference_Titel
1958 IRE International Convention Record
Conference_Location
New York, NY, USA
Type
conf
DOI
10.1109/IRECON.1961.1151013
Filename
1151013
Link To Document