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The ion optics of a two grid electron-bombardment thrusterA detailed experimental investigation has been performed to determine the ion beam divergence of an electron-bombardment ion thruster as a function of grid geometry changes. The results show that, to a good approximation, each geometrical grid parameter independently affects one aspect of grid set performance. These observations are used to develop a graphical technique for predicting the ion beam divergence of an arbitrary ion source and grid geometry combination. The usefulness of this technique is demonstrated by comparing predicted ion beam divergence of the 30-cm diameter Engineering Model ion thruster with independent experimental determinations. Good agreement is shown between predicted and experimental results.
Document ID
19770030159
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Aston, G.
(Colorado State Univ. Fort Collins, CO, United States)
Kaufman, H. R.
(Colorado State University Fort Collins, Colo., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-1029
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Key Biscayne, FL
Start Date: November 14, 1976
End Date: November 17, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A13011
Funding Number(s)
CONTRACT_GRANT: NGR-06-002-112
Distribution Limits
Public
Copyright
Other

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