NASA NTRS · 20150011942
Neutralizer Hollow Cathode Simulations and Validation with Experiments
Abstract
The fidelity of electric propulsion physics-based models depends largely on the validity of their predictions over a range of operating conditions and geometries. In general, increased complexity of the physics requires more extensive comparisons with laboratory data to identify the region(s) that lie outside the validity of the model assumptions and to quantify the uncertainties within its range of application. This paper presents numerical simulations of neutralizer hollow cathodes at various operating conditions and orifice sizes. The simulations were performed using a two-dimensional axisymmetric model that solves numerically a relatively extensive system of conservation laws for the partially-ionized gas in these devices. The results for the plasma are compared directly with Langmuir probe measurements. The computed keeper voltages are also compared with the observed values. Wherever model inputs and/or specific physics of the cathode discharge are uncertain, additional sensitivity calculations have been performed to quantify the uncertainties.
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Mikellides, Ioannis G., Goebel, Dan M., Snyder, John S., Katz, Ira, Herman, Daniel A.. 2009-08-03. Neutralizer Hollow Cathode Simulations and Validation with Experiments. https://ntrs.nasa.gov/citations/20150011942
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