18 research outputs found
Mossbauer-spectroscopy Studies of the Preparation Steps of Unsupported Fe and Femo-sulfide Hydrotreating Catalysts
Mossbauer Emission-spectroscopy of An Unsupported Cobalt-molybdenum Hydrodesulfurization Catalyst
Characterization of Unsupported Como Sulfide Catalysts and Their Precursors By Temperature-programmed Reactions
Temperature-programmed Reaction and Desorption Studies of Unsupported Mos2-based Hydrotreating Catalysts
Temperature-programmed Reaction and Desorption Studies of Unsupported Mos2-based Hydrotreating Catalysts
Due to the advantages of electric motors and electric batteries, the electric propulsion systems are widely used in UAVs [1,2]. The UAV’s performance and endurance, the payload capacity and the flight time of the vehicle are affected highly by the structure and design of the electric propulsion system. In this paper, a new systematic design methodology for electric propulsion system (propeller, electric motor and battery pack) is proposed based on the design specifications given in terms of the required thrust, permissible propulsion system’s weight and required flight time