Deadline: 2025-12-31 Status: Future Opening
Description
Design, development, manufacturing and ground test demonstration of an Ultra HighBypass Ratio (UHBR) ducted geared turbofan engine, including advanced core engineand combustion technologies, advanced thermodynamic (variable) cycle; andhybridisation technologies targeting ultra-efficient propulsion systems for SMRaircraft, with a fuel burn reduction of minimum 20% at aircraft level compared to2020 state-of-the-art. TRL 5 at ducted geared engine architecture system level fromground test demonstration at project completion
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