Title :
Laboratory simulation of reentry plasma sheaths
Author_Institution :
Aerospace Corporation, El Segundo, CA, USA
fDate :
11/1/1967 12:00:00 AM
Keywords :
Plasmas; Space-vehicle reentry; Cathodes; Electrodes; Electron beams; Laboratories; Plasma density; Plasma properties; Plasma sheaths; Plasma simulation; Plasma temperature; Plasma waves;
Journal_Title :
Antennas and Propagation, IEEE Transactions on
DOI :
10.1109/TAP.1967.1139033