The invention discloses a Hall thruster adopting a lightweight integrated
anode. The Hall thruster comprises a bottom plate, wherein an inner
magnetic core wound with an inner magnetic coil is configured at the centre of the bottom plate; a plurality of outer magnetic cores wound with outer magnetic coils are configured at the periphery of the bottom plate; the lightweight integrated
anode is arranged between the inner
magnetic core and the outer magnetic cores; a protective cover is arranged outside the
anode; and the protective cover and the anode are insulated and supported by
ceramic. An inner
ceramic ring and an outer
ceramic ring are arranged at the outlet of the lightweight integrated anode, and the inner ceramic ring and the outer ceramic ring are compacted by the outer edge of the inner
magnetic core and a
front panel separately; and all the parts are installed on the bottom plate, and an insulation sleeve sleeves the gas
pipe of the lightweight integrated anode. According to the Hall thruster disclosed by the invention, an integrated anode structure is adopted, and the flowing and distribution characteristics of a gas are improved, so that the thruster is better in
ionization effect, better in performance, lower in
thermal load, higher in the capacity of resisting to severe mechanical environments, more compact in structure, smaller in size, and lighter in weight.