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Dissertation
Analysis of hybrid electric propulsion for a microlight aircraft prototype
Authors: --- --- ---
Year: 2024 Publisher: Liège Université de Liège (ULiège)

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Abstract

This project aims to test the combination of existing equipment to obtain efficient hybrid-electric propulsion for a microlight aircraft which feats the ULM description and has a MTOW of 530 kg. Some of the additional objectives would be to dimension a battery, get data for the possible emissions of the system, study efficiencies of various components and an estimation of the costs.

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