DocumentCode
951511
Title
Plasma Propulsion Possibilities
Author
Rayle, Warren
Author_Institution
Lewis Res. Center, Natl. Aeronautics and Space Admin., Cleveland, Ohio.
Issue
2
fYear
1959
fDate
4/1/1959 12:00:00 AM
Firstpage
42
Lastpage
45
Abstract
Plasma propulsion systems are arranged in three categories according to the cyclic nature of the jet produced; 1) steady, 2) alternating or wave-accelerated, and 3) pulsed. Typical systems within each category are described with emphasis on work being done at the NASA Lewis Research Center. The criteria for evaluating the relative merits of these systems are listed and the advantages and disadvantages pointed out. Such parameters as energy efficiency and propellant utilization must be measured before conclusions can be reached as to the eventual applicability of any of these systems.
Keywords
Acceleration; Ion beams; Military aircraft; NASA; Plasma accelerators; Plasma devices; Plasma temperature; Plasma waves; Propulsion; Thermal expansion;
fLanguage
English
Journal_Title
Military Electronics, IRE Transactions on
Publisher
ieee
ISSN
0096-2511
Type
jour
DOI
10.1109/IRET-MIL.1959.5008132
Filename
5008132
Link To Document