| CPC F03H 1/0006 (2013.01) [B64G 1/413 (2023.08)] | 14 Claims |

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1. A plasma cathode for in space ion propulsion, comprising:
a gas flow;
a hollow emitter through which the gas flow passes;
an orifice cup, surrounding the hollow emitter and having a portion extending downstream of the hollow emitter, for containing plasma produced by the interaction of electrons from the emitter with said gas flow, said orifice cup having a discharge orifice in the portion downstream of the hollow emitter, said orifice cup containing said plasma in a substantial space between said emitter and said discharge orifice with said orifice cup electrically isolated from said emitter; and
a keeper electrode disposed downstream of said discharge orifice.
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