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Differential Sputtering Behavior of Pyrolytic Graphite and Carbon-Carbon Composite Under Xenon BombardmentA differential sputter yield measurement technique is described, which consists of a quartz crystal monitor that is swept at constant radial distance from a small target region where a high current density xenon ion beam is aimed. This apparatus has been used to characterize the sputtering behavior of various forms of carbon including polycrystalline graphite, pyrolytic graphite, and PVD-infiltrated and pyrolized carbon-carbon composites. Sputter yield data are presented for pyrolytic graphite and carbon-carbon composite over a range of xenon ion energies from 200 eV to 1 keV and angles of incidence from 0 deg (normal incidence) to 60 deg .
Document ID
20040085956
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Williams, John D.
(Colorado State Univ. Fort Collins, CO, United States)
Johnson, Mark L.
(Colorado State Univ. Fort Collins, CO, United States)
Williams, Desiree D.
(Colorado State Univ. Fort Collins, CO, United States)
Date Acquired
September 7, 2013
Publication Date
July 14, 2003
Subject Category
Nonmetallic Materials
Report/Patent Number
Boeing-819415
Meeting Information
Meeting: Joint Propulsion Conference
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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