As development continues on the production of bismuth fueled Hall thrusters, there is a need for an accurate understanding of the nature of bismuth plasma. This includes both the ability to predict the electrical breakdown characteristics of a bismuth gas, as well as the design of tools necessary to make diagnostic measurements on a bismuth-fed electric thruster. A bismuth heat pipe apparatus capable of igniting an electrical discharge in a bismuth gas has been constructed for the purposes of such analysis. This paper will discuss the progress of using this chamber for preparing optical diagnostic techniques in a bismuth plasma, as well as measured current-voltage and Paschen curves for a bismuth gas mixed with Argon. While ion populations in the heat pipe are not yet strong enough to produce a measurable absorption or laser-induced fluorescence signal on the Bi II transition selected for thruster performance analysis, we have recorded significant effects on the electrical behavior of the argon gas due to the presence of bismuth vapor.
Nomenclature