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Accelerator Grid Tests on an Electron-Bombardment Ion RocketA systemic investigation of screen-accelerator grids was made with an ion rocket having a 10-centimert-diamter electron-bombardment ion source. Mercury ion beams of 0.03 to 0.44 ampere were operated at net accelerating voltages of 900 to 6100 volts. A multihole screen-accelerator grid set passed the greatest percent of an ideal plane diode current with a ration of between-grid spacing to individual hole diameter of approximately 1. Breakdown between the grids occurred at field strengths of 2000 to 3000 volts per millimeter for grid spacings of 1 to 3 millimeters. The accelerator impingement was about 1 percent and caused little erosion of the molybdonum grids, which indicated a grid life of the order of 10000 hours or better. The experimental work was conducted in a bell jar connected to a 5-foot-diameter by 16-foot-long vacuum tank at Lewis Research Center.
Document ID
19620000001
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
William R Kerslake
(Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 29, 2013
Publication Date
February 1, 1962
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Plasma Physics
Report/Patent Number
E-1430
NASA-TN-D-1168
Accession Number
62N10001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Electron bombardment
Electric propulsion
Ionic propulsion
Accelerator
Ion engine
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