Performance Correlation for Electron-bombardment Ion Sources
Author : Harold R. Kaufman
Publisher :
Page : 44 pages
File Size : 28,64 MB
Release : 1965
Category : Electron bombardment conductivity
ISBN :
Author : Harold R. Kaufman
Publisher :
Page : 44 pages
File Size : 28,64 MB
Release : 1965
Category : Electron bombardment conductivity
ISBN :
Author : Allan J. Cohen
Publisher :
Page : 36 pages
File Size : 35,78 MB
Release : 1966
Category : Diffusion
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Author : Harold R. Kaufman
Publisher :
Page : 68 pages
File Size : 40,22 MB
Release : 1971
Category : Electric propulsion
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The evaluation and understanding of maximum propellant utilization, with mercury used as the propellant are presented. The primary-electron region in the ion chamber of a bombardment thruster is analyzed at maximum utilization. The results of this analysis, as well as experimental data from a range of ion-chamber configurations, show a nearly constant loss rate for unionized propellant at maximum utilization over a wide range of total propellant flow rate. The discharge loss level of 1000 eV/ion was used as a definition of maximum utilization, but the exact level of this definition has no effect on the qualitative results and little effect on the quantitative results. There are obvious design applications for the results of this investigation, but the results are particularly significant whenever efficient throttled operation is required.
Author :
Publisher :
Page : 290 pages
File Size : 26,43 MB
Release : 1971
Category :
ISBN :
Author :
Publisher :
Page : 1050 pages
File Size : 16,7 MB
Release : 1966-02
Category : Government publications
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Author : United States. Superintendent of Documents
Publisher :
Page : 1250 pages
File Size : 24,86 MB
Release : 1979
Category : United States
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Author :
Publisher :
Page : 1732 pages
File Size : 27,88 MB
Release : 1965
Category : Government publications
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Author : Walter C. Lathem
Publisher :
Page : 36 pages
File Size : 35,24 MB
Release : 1971
Category : Acceleration (Mechanics)
ISBN :
Results are presented for a theoretical analysis of the performance of two-grid accelerator systems for Kaufman thrusters. Six configurations were used to cover the range of geometries which are of immediate interest. A digital ccomputer program was used to find axially symetric solutions for a single hole of each configuration. Results are presented in terms of maximum current per hole, thrust per hole (including beam divergence effects), and maximum net-to total-voltage ratio consistent with the prevention of electron backstreaming. The results presented herein should be useful in the design of accelerator systems for a variety of applications. An analysis of the effects of charge-exchange ions on the erosion rate of the accelerator grid resulted in equations which could be used to predict the expected useful lifetime of the grid. The equations seemed consistent when theoretical results were compared with experimental results for the SERT II configuration. However, when applied to the configurations used in this analysis, limitations in the usefulness of the model were found and are presented herein.
Author :
Publisher :
Page : 1572 pages
File Size : 37,66 MB
Release : 1992
Category : Aeronautics
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1248 pages
File Size : 17,86 MB
Release : 1961
Category : Government publications
ISBN :