During the execution of the research project, the following scientific and technical tasks will be accomplished:
- substantiated the flight profile, payload mass, and aerodynamic characteristics of a low-altitude UAV with a supersonic flight segment;
- substantiated promising powerplant (PP) configurations for use in a UAV with a supersonic flight segment, which will be further considered in the comprehensive optimization of the PP scheme and parameters according to the selected criteria;
- developed mathematical models of turbomachinery that account for the specific features of the powerplant for the UAV.