DocumentCode
957557
Title
Potentialities of Electron Bombardment Ion Engines for Electric Propulsion
Author
Kerrisk, Daniel J.
Author_Institution
Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.
Issue
2
fYear
1962
fDate
6/1/1962 12:00:00 AM
Firstpage
188
Lastpage
193
Abstract
This paper discusses the expected performance of electron bombardment ion sources when used for electrostatic propulsion. Two particular sources, the duoplasmatron and the Penning Ion source, are examined in some detail and suggestions are made on how their performance for application with electric thrust devices could be improved. It is concluded that electron bombardment sources may offer some advantages over surface contact engines if ways can be found to significantly improve their propellant utilization.
Keywords
Acceleration; Apertures; Electron emission; Engines; Ion sources; Plasma accelerators; Plasma density; Propulsion; Space technology; Voltage;
fLanguage
English
Journal_Title
Space Electronics and Telemetry, IRE Transactions on
Publisher
ieee
ISSN
0096-252X
Type
jour
DOI
10.1109/IRET-SET.1962.5008831
Filename
5008831
Link To Document