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 :
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