Preliminary Aircraft Design for Hybrid Electric Propulsion Architectures: A Focus on Critical Loss of Thrust

Hybrid electric propulsion architectures offer a promising solution for reducing fuel consumption and emissions in aviation. However, the introduction of dual-energy carriers adds complexity to preliminary aircraft design, particularly in terms of power distribution, failure analysis, and compliance...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Jonas Mangold, Andreas Strohmayer
Format:	Article
Language:	English
Published:	MDPI AG 2025-03-01
Subjects:	preliminary aircraft design failure critical loss of thrust one-engine- inoperative redundancy hybrid electric
Online Access:	https://www.mdpi.com/2226-4310/12/4/275