The files introduce a revolutionary design for an unmanned aerial vehicle provided by a missile for aerial targets. The drone has a propeller for propulsion which can be driven electrically by electric motors. That design can be integrated with solar cells at the area of the wing span and the support which is provided to hold the vertical stabilizers. The wing span is 7.843 m and the backward support span is 5.968m. The total surface area of the vehicle is 63.42 m^2. The design was made in such a way that the propeller sucked the air layer on the upper and lower surface of the vehicle so that it will provide damping for any vortices with its function of propulsion. No material was applied to the vehicle but it’s easy to apply the required material from the Solidworks options according to your requirement. The missile was designed with a converging-diverging nozzle and sharp cone for adopting the supersonic flow properties. Note that for manufacturing, the aerodynamicists need to calculate the required load according to the material's density and the weight of the motors to get the location of the center of gravity and compare it with the aerodynamic loads- forces and moments- for gaining stability and smooth operation for the desired conditions like the required height and speed. That design represents a primary idea for innovation and combining sustainability with military aircraft for long-duration operations. I also provided a small forward canard to adjust the pressure distribution with the center of gravity for control and stability. The vehicle was designed as only one part( There is no assembled parts). and it is presented in solidworks file SDTL. and STL file