Development of UAV aerostructures for civil application

Definition of innovative methods for the development, testing, validation, and certification of unmanned aircraft structures (UAV), which would allow creating a clear vector in creating value for the market, of products and technologies developed by the national industry, for the aeronautical industry.

It was possible to obtain a physical and operational prototype of an autonomous UAV with a 7.5 m wingspan, a range of 16h, a maximum take-off weight of 250 kg, and a maximum load of 70 kg.

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