Propulsion and Power System Selection: Feb 25-28

With the baseline airframe architecture defined, engineering efforts shifted toward propulsion and electrical system configuration.

Key considerations included:

• motor efficiency within the target thrust envelope

• compatibility with a 6S power system

• component reliability and availability within domestic supply chains

Following evaluation of several propulsion options, the development team selected a 2806.5-class motor paired with a 6S battery configuration for the initial demonstrator aircraft.

This propulsion architecture provides sufficient thrust margin while maintaining manageable system weight and electrical complexity.