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The wave-heating magnetoplasma thruster possesses many advantages such as its suitability for high power propulsion (about 100 kWe-1 MWe), high thrust density (about 4×105 N/m2), variable high thrust (about 1-100 N), and adjustable specific impulse (about 3 000-10 000 s). These advantages make the wave-heating magnetoplasma thruster well suited for a diverse range of future space missions with high-performance. Based on previous studies of the wave-heating magnetoplasma thruster both home and abroad, this work summarizes the technical status of the wave-heating magnetoplasma thruster in recent years, and analyzes the theoretical issues the present research faced in the development of the wave-heating magnetoplasma thruster, such as the so called single-pass ion cyclotron resonance heating, the plasma detachment controlling, the high-power density plasma diagnosing in strong magnetic fields, as well as many engineering difficulties, including the efficient thermal management and high-power RF power supplies. Finally, application directions of the wave-heating magnetoplasma thruster are prospected according to its performance characteristics.
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