DocumentCode
951503
Title
Plasma Propulsion Devices for Space Flight
Author
Camac, M. ; Kantrowitz, A. ; Petschek, H.E.
Author_Institution
Avco Everett Research Lab., Everett, Mass.
Issue
2
fYear
1959
fDate
4/1/1959 12:00:00 AM
Firstpage
34
Lastpage
41
Abstract
An analysis of some of the more immediate space missions indicates that a large increase in payload can be achieved when electrical propulsion is used instead of chemical propulsion. For missions in the gravitational field of the Earth and to the Moon, the optimum specific impulse range for electrical propulsion is from about 1500 to 5000 seconds. Electrical propulsion with neutral plasma devices operate well in this specific impulse range as well as at higher specific impulses. Three different chambers have been described as examples of devices using neutral plasmas. Some of the factors which limit the range of efficient operation of such devices have been discussed.
Keywords
Aerospace electronics; Artificial satellites; Chemical analysis; Earth; Moon; Payloads; Plasma devices; Propulsion; Rockets; Space missions;
fLanguage
English
Journal_Title
Military Electronics, IRE Transactions on
Publisher
ieee
ISSN
0096-2511
Type
jour
DOI
10.1109/IRET-MIL.1959.5008131
Filename
5008131
Link To Document