The invention relates to a foldable coaxial reverse propeller unmanned aerial vehicle and a striking method. The unmanned aerial vehicle comprises a data chain antenna, an upper rotor wing, an upper rotor wing propeller clamp, a driving module, a lower rotor wing propeller clamp, a lower rotor wing, a power and flight control module, an image load, a terminal-sensitive bullet, and a terminal-sensitive bullet sensor. The upper rotor wing and the lower rotor wing are connected with the driving module through the upper rotor wing propeller clamp and the lower rotor wing propeller clamp respectively, and the upper rotor wing and the lower rotor wing are driven to rotate under the driving of the driving module to produce lift force; the power and flight control module provides power for the driving module, and the data chain antenna is electrically connected to the power and flight control module to realize the data and instruction transmission between the power and flight control module and a ground control station; and the image load is installed on the outer side of the power and flight control module to be used for collecting an image of an attack target, and the terminal-sensitivebullet and the sensor used for sensitive attack targets are installed at the bottom of the unmanned aerial vehicle. According to the unmanned aerial vehicle and the striking method, the terminal-sensitive bullet is adopted for striking, so that the requirement of a flying platform on the bullet throwing precision is reduced, and low cost is realized.