Abstract: A heaterless hollow cathode with high current discharge capability for use in electric propulsion devices is presented. The heaterless hollow cathode includes a thermionic emitter insert having a tubular shape and arranged inside a hollow cathode tube. The heaterless hollow cathode further includes a propellant feed tube that longitudinally extends from an upstream region of the hollow cathode tube into an inner volume of the insert. According to one aspect, an extension of the propellant feed tube into the inner volume of the insert is in a range from one quarter to three quarters of a total longitudinal length of the insert. The propellant feed tube is made of a refractory metal that is capable of withstanding temperatures above 2200 degrees C. with negligible evaporation. According to another aspect, the refractory metal is tantalum or tungsten.