Feasibility of a helium closed-cycle gas turbine for UAV propulsion
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DOI: 10.3390/app11010028
Abstract: When selecting a design for an unmanned aerial vehicle, the choice of the propulsion system is vital in terms of mission requirements, sustainability, usability, noise, controllability, reliability and technology readiness level (TRL). This study analyses… read more here.
Keywords: cycle gas; propulsion; closed cycle; cycle ... See more keywords