| Hybrid-Electric Aircraft (HEA) Performance through Multidisciplinary Design Optimization (MDO) |
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Development of an automated optimization tool for the design and exploration of hybrid-electric aircraft (HEA), integrating sizing, mission analysis, and auxiliary systems. The project identifies the economic feasibility of HEA and the most suitable mission types for their operation, as well as the benefits of combining More Electric Aircraft (MEA) technologies with Hybrid-Electric Propulsion Systems (HEPS). |
