The invention provides an integrated structure liquid-electric composite brake aircraft carrier interceptor, comprising a hub type eddy current auxiliary brake with a plurality of sets of excitation coils distributed. The hub type eddy current auxiliary brake comprises a stator, a side cover and a rotor, the stator and the rotor are co-axially arranged, the stator is located outside the rotor, theside cover covers the two ends of the stator and the two ends of the rotor, coolant flow passages which communicate mutually are formed between the rotor and the side cover and between the rotor andthe stator, and the coolant flow paths form a hydraulic auxiliary brake. The invention overcomes the defects of the existing intercepting devices and provides the novel integrated structure liquid-electric composite brake aircraft carrier interceptor with high power density, simple structure, small size, low cost, convenient control, fast response speed and adjustable torque, and an intercepting system employing the interceptor.