Architecture Evaluation: Feb 21-24

Following program initiation, Chenault Aerospace evaluated several candidate airframe architectures suitable for the demonstrator platform.

Configuration studies focused on:

• compact multirotor geometries

• propulsion efficiency for short-duration tactical missions

• modular avionics stack integration

• structural durability and maintainability

The evaluation resulted in selection of a 10-inch class multirotor architecture as the baseline configuration for the demonstrator aircraft. This configuration provides a balance between payload capability, maneuverability, and component availability while remaining compatible with low-cost propulsion systems.