The invention provides a vortex
resonance multistage cusped field micro-newton-scale
ion propulsion device, belongs to the field of
plasma propulsion, and particularly relates to a vortex
resonance multistage cusped field micro-newton-scale
ion propulsion device. The device solves the problems that an existing micro-newton-scale thruster cannot meet the requirements for large-range adjustability of thrust, high-precision
thrust control and the like in major tasks such as space
gravitational wave detection and space
gravitational field detection are solved. The device comprises a
discharge cavity, a screen grid and an accelerating grid, wherein the screen grid and the accelerating grid are fixed to the open end of the
discharge cavity, a
quartz guard plate is coaxially and fixedly arrangedinside the
discharge cavity, the discharge cavity comprises an annular
wall plate and a bottom plate, the bottom plate is fixedly arranged at one end of the annular
wall plate, a plurality of incensecoil-shaped antennas are arranged on the end face, close to the
quartz guard plate, of the bottom plate, the incense coil-shaped antennas form a periodic topological structure array on the bottom plate, and multistage annular permanent magnets are arranged on the side wall of the annular
wall plate. The device is mainly used for propulsion of plasmas.