FIELD: aviation.
SUBSTANCE: invention relates to aviation technology, mainly to unmanned aerial vehicles (UAVs). The proposed UAV comprises a streamlined body, an air intake connected by an air duct with a chamber for mixing and burning hydrogen with air oxygen. The chamber ends with a nozzle with a central body. The onboard hydrogen generator comprises a closed container with plates of activated aluminium (1/2 volume) and a reaction solution (RS). The hydrogen generator is connected with a container of an RS receiver equipped with a pump for supplying the RS to the generator. The receiver is equipped at the output with a pipeline for supplying hydrogen to the distribution chamber and therefrom through the nozzle unit into the chamber for mixing and burning hydrogen with air oxygen. The mixture produced in the chamber is compressed in the area of the critical section of the nozzle with a central body.
EFFECT: increased design excellence and reliability of the UAV.
1 cl, 4 dwg, 1 tbl
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