- Achieving energy self-sufficiency or at least extended flight time.
- Development of the airframe supporting structure with high tensile strength in order to achieve the appropriate functional parameters.
- Obtaining the appropriate load capacity while drastically minimizing the weight of the load-bearing structures.
- Development of functional UAV systems that allow maximum use of specific flight parameters, high altitude variability and low cruising speed.
- Development of various types of sensors enabling the measurement of atmospheric pollutants both during the day and at night.