Review and investigate current State-of-the-Art (SoA) technologies.
Sizing, layout and performance of the components.
Identification of scientific and technical challenges of the proposed concepts.

Coupling of individual components after a technology and opportunity down-selection procedure.

Integration of powertrain components in the airframe and optimization of the proposed architectures.

The target is to minimize the environmental impact of the system and reduce overall operating costs and include a Life Cycle Analysis of the down-selected architectures.

Pave the ground for future exploitation of the proposed design and target for an iron bird or flight demonstrator. Communicate benefits of the proposed design and disseminate project results.