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  5. Definition of requirement specifications engine for light unmanned aerial vehicles

Definition of requirement specifications engine for light unmanned aerial vehicles

U.M. Osipov, S.V. Orlov
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The paper presents an assessment of the expected mass-dimensional characteristics of light drones method of determining the required thrust and fuel consumption of the engine depending on the weight of the unmanned aerial vehicle , a predetermined height and speed cruise flight. The obtained results allow to pre-set design parameters for the development of the jet engine or choose one of the engines created for the planned UAV.
Keywords: mean unmanned aerial vehicle , needs engine performance , sustainer engine thrust