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Ion Thruster Contamination Test Facility


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Description:

  • Produces controlled contamination on material surfaces to study the effects of contamination.
  • Contamination produced by electric arc between two carbon electrodes.
  • Quantity of contamination is measured by the contamination thickness, the duration of the carbon arc, the mass loss of the electrodes, and/or monitoring electrical resistance.
  • Process occurs in vacuum inside a bell jar.

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Features:

  • The carbon arc is powered by 15 kV, 60mA, 60-Hertz alternating current, which is transformed from 120V, 60-Hertz alternating current via a neon sign transformer.
  • The pressure in the bell jar is in the range of 10-6 to 10-5 mtorr during carbon arcing, and 10-7 to 10-6 mtorr without carbon arcing.
  • The resistance of the material to be contaminated can be monitored during the arcing process.
  • The voltage to measure the resistance can be in the 1-5000V range.
  • The carbon arc can continue for more than one hour, producing more than 1000 Ĺ (Angstrom) of contamination.

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Research Projects:

  • Experimentally determine the effectiveness of the shadow shields to be used to protect ion engine’s insulators/isolators from contamination.
  • Experimentally determine the effects of contamination on materials having various surface morphologies.
  • Experimentally determine the “contamination efficiency,” or the percent of particles impacted on the surface that do not bounce away.

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Potential Uses:

  • Study of contamination effects by materials other than carbon if other materials are used as the electrode materials.

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Curator:  Sandra.A.Zolo@nasa.gov and NASA Official Responsible For Content: Sharon.K.Miller@grc.nasa.gov
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Last Updated: 08/30/2008