Model of a Hollow Cathode Insert Plasma

Mikellides, Ioannis G.; Katz, Ira; Goebel, Dan M.; Polk, James E.

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NASA NTRS · 20070021680

Model of a Hollow Cathode Insert Plasma

Mikellides, Ioannis G.·Katz, Ira·Goebel, Dan M.·Polk, James E.

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Abstract

A 2-D axisymmetric fluid model of the plasma in the insert region of a hollow cathode is presented. The level of sophistication included in the model is motivated in part by the need to determine quantitatively plasma fluxes to the emitter surface. The ultimate goal is to assess whether plasma effects can degrade the life of impregnated inserts beyond those documented throughout the 30-50 year history of vacuum cathode technologies. Results from simulations of a 1.2-cm diameter cathode operating at a discharge current of 25 A, and a gas flow rate of 5 sccm, suggest that approximately 10 A of electron current, and 3.5 A of ion current return to the emitter surface. The total emitted electron current computed by the model is about 35 A. Comparisons with plasma measurements suggest that anomalous heating of the plasma due to two-stream instabilities is possible near the orifice region. Solution to the heavy species energy equation, with classical transport and no viscous effects, predicts heavy species temperatures as high as 2640 K.

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Mikellides, Ioannis G., Katz, Ira, Goebel, Dan M., Polk, James E.. 2004-07-12. Model of a Hollow Cathode Insert Plasma. https://ntrs.nasa.gov/citations/20070021680

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