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Sputtering Threshold Energies of Heavy IonsSputter erosion in ion thrusters has been measured in lifetests at discharge voltages as low as 25 V. Thruster operation at this discharge voltage results in component erosion rates sufficiently low to satisfy most mission requirements. It has been recognized that most of the internal sputtering in ion thrusters is done by doubly charged ions. Knowledge of the sputtering threshold voltage of a xenon molybdenum system would be beneficial in understanding the sputtering process as well as making more accurate calculations of the sputtering rates of ion thruster components. Sputtering threshold energies calculated from various formulations found in the literature results in values ranging from 28 to 200 eV. It is evident that some of these formulations cannot be relied upon to provide sputtering thresholds with any degree of accuracy. This paper re-examines the threshold energies measurements made in the early sixties by Askerov and Sena, and Stuart and Wehner. The threshold voltages as derived by Askerov and au have been reevaluated by using a different extrapolation method of sputter yields at low ion energies. The resulting threshold energies are in general similar to those measured by Stuart and Wehner. An empirical relationship is derived,for mercury and xenon ions for the ratio of the sputtering threshold energy to the sublimation energy as a function of the ratio of target to ion atomic mass.
Document ID
19990064093
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
Authors
Mantenieks, Maris A.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1999
Subject Category
Atomic And Molecular Physics
Report/Patent Number
IEPC-97-187
NASA/TM-1999-209273
E-11726
NAS 1.15:209273
Report Number: IEPC-97-187
Report Number: NASA/TM-1999-209273
Report Number: E-11726
Report Number: NAS 1.15:209273
Meeting Information
Meeting: International Electric Propulsion
Location: Cleveland, OH
Country: United States
Start Date: August 24, 1997
End Date: August 28, 1997
Sponsors: Electric Rocket Propulsion Society
Funding Number(s)
PROJECT: RTOP 632-1B-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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