Overview of the electric propulsion plasma diagnostics suite for the VASIMR VX-200 testbed
ORAL
Abstract
Descriptions of the various plasma diagnostics and data analysis methods are given for instruments used in high power ($>$ 100 kW) electric propulsion testing. These include planar Langmuir probes, an articulating retarding potential analyzer, a double Langmuir probe, a multi-axis magnetometer, a high frequency electric field probe, microwave interferometer, and momentum flux targets. These diagnostics have been used to measure the efficiencies of the thruster, plasma source, ion cyclotron resonance booster, and magnetic nozzle as well as used to explore physical phenomena in the plume such as ion/electron detachment, plasma turbulence, and magnetic field line stretching. Typical plume parameters range up to 10$^{13}$ cm$^{-3}$ electron density, 1 kG applied magnetic fields, ion energies in excess of 150 eV, and cold electrons (2 -- 5 eV) with a spatial measurement range over 2 m.
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Authors
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Christopher Olsen
Ad Astra Rocket Company
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Benjamin Longmier
Ad Astra Rocket Company
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Maxwell Ballenger
Ad Astra Rocket Company
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Jared Squire
Ad Astra Rocket Company
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Tim Glover
Ad Astra Rocket Company
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Mark Carter
Ad Astra Rocket Company
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Edgar Bering
University of Houston
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Matthew Giambusso
University of Houston