Dropping model structure for unmanned aerial flight test

The invention discloses a launching model structure for an unmanned aerial flight test, and the structure comprises a flight test launching model body, an airplane model, a rocket model, and a fuselage. The fuselages are connected through a central wing for reducing the gravity center and symmetrical disturbance of the flight test putting model body during flight, the hanging device is provided with a hanging frame or a hook, the hanging frame or the hook is connected to the central wing, the flight putting piece is connected to the hanging frame, the hanging frame is arranged at the central position of the central wing, and the hanging frame is connected to the hanging device. The wings are flight launching pieces used for enabling the flight test launching model body to be stably launched when the flight test launching model body is launched in a flight mode, the wings are connected to the left side and the right side of the flight test launching model body and further located on the upper side of the fusel