Busek proposes to develop radio frequency discharge, gridded micro-ion thruster that produces sub-mN thrust precisely adjustable over a wide dynamic thrust range. Such propulsion is needed to augment and overlap the present micro Newton propulsion such as colloid thruster. The RF was selected to eliminate the internal cathode of the DC discharge ion thrusters. This cathode could be a life limiting component and consumes propellant. Two types of neutralizers are candidates for the proposed thruster and include Busek's carbon nanotube field emission cathode similar to that developed for the ST7 DRS mission and already demonstrated RF discharge cathode which consumes much less flow than comparable hollow cathode. The performance of the proposed RF micro-ion thruster is expected to approach that of the NASA JPL MiXI which represents the state of the art in small ion thrusters with DC discharge. In Phase 1 the RF micro-ion thruster will be build and tested and second generation laboratory device will be designed. MIT, our subcontractor, will initiate the development the RF thruster numerical model to support the experimental effort. In Phase 2 the thruster system will be constructed and demonstrated including the optimized thruster, neutralizer, key parts of the PPU and the feed system.