- To perform a concept study at aircraft level?
- To evaluate different design solutions given multiple multidisciplinary requirements?
- To determine the propulsion system requirements for an innovative aircraft, e.g. with hybrid electric propulsion?
- To calculate weight estimates for aircraft concepts?
- To estimate the performance of novel aircraft concepts, e.g. in terms of environmental impact?
- A long track record in aircraft multidisciplinary design and optimisation (MDO) including collaboration with international industrial and research partners
- Conceptual design and sizing methodologies for conventional and (hybrid-)electric propelled aircraft
- Corresponding efficient and integrated tooling: MUCH – MUltidisciplinary Conceptual design of Hybrid electric aircraft
- Aircraft propulsion and mission modelling capabilities
- Aircraft performance analysis
- Mission optimisation
- Multidisciplinary analysis
- System power requirements