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Ion beam sputtering in electric propulsion facilitiesExperiments were undertaken to determine sputter yields of potential ion beam target materials, to assess the impact of charge exchange on beam diagnostics in large facilities, and to examine material erosion and deposition after a 957 hr test of a 5 kW-class ion thruster. The xenon ion sputter yield of flexible graphite was lower than other graphite forms especially at high angles of incidence. Ion beam charge exchange effects were found to hamper beam probe current collection diagnostics even at pressures from 0.7 to 1.7 mPa. Estimates of the xenon ion beam envelope were made and predictions of the thickness of sputter deposited coatings in the facility were compared with measurements.
Document ID
19910022844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sovey, James S.
(NASA Lewis Research Center Cleveland, OH, United States)
Patterson, Michael J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-6420
NASA-TM-105145
AIAA PAPER 91-2117
NAS 1.15:105145
Report Number: E-6420
Report Number: NASA-TM-105145
Report Number: AIAA PAPER 91-2117
Report Number: NAS 1.15:105145
Meeting Information
Meeting: Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: June 24, 1991
End Date: June 27, 1991
Sponsors: ASEE, AIAA, SAE, ASME
Accession Number
91N32158
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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