This work should be understood as the challenge of integrating different technologies that have a strong boom in the aeronautics field. The aim is to perform a micro air vehicle, where the entire structure consists of a single wing built by inflatable structure. This prototype will be an unmanned vehicle capable of vertical takeoff and landing as if it were a helicopter. We must solve various technological problems arising from constructing and manipulating inflatable structures within the micro air vehicle category and keep it running efficiently as helicopter and flying wing according to a list of limitations agreed with the customer. The weight that is able to support in every phase of flight will be a significant aspect to optimize. This challenge will be faced by studying the technologies available to meet every need, we will establish a requirements and consider various implementation solutions backed into simulations and experimental assays to become compliant as many requirements as possible. In case of non-meet any of them, solutions and future work to be done will be indicated.