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The effect of nitrogen on xenon ion engine erosionErosion studies were performed on a 30-cm diameter J-series ion engine modified for operation on xenon propellant. The erosion rates of molybdenum and tantalum badges placed at different locations within the discharge chamber were measured as a function of the percentage of nitrogen (by mass) added to the xenon propellant. Reductions in the erosion rates of these badges of a factor of 8 to 50 were observed at nitrogen addition fractions between 0.5 to 2.0 percent. Reductions in cathode-side baffle erosion were achieved by adding nitrogen to the xenon propellant or by increasing the cathode orifice diameter. Analyses show that no significant degradation in ion engine performance should be expected at these nitrogen mass fractions. XRD, XPS and Auger analyses indicate the existence of nitrogen and nitrides in the surface of some but not all of the badges used in the tests where nitrogen was added to the xenon. Difficulty in identifying surface nitrides in the samples may be due to the existence of surface oxides and contaminants, or to the small thicknesses of the nitride layers.
Document ID
19900055512
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Garner, Charles E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Brophy, John R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pless, L. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Barnett, John W.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-2591
Accession Number
90A42567
Distribution Limits
Public
Copyright
Other

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