Story
The Y1101 was developed entirely in SolidWorks, focusing on structural integrity and aerodynamic resistance management. The airframe employs a compact, low-drag geometry with balanced mass distribution to maintain dynamic stability during rapid maneuvering.
The NACA-M18 airfoil propeller design was selected for its high lift-to-drag ratio and stall resistance, making it ideal for aggressive pitch and forward-thrust conditions. Each propeller and frame segment is optimized for 3D printing, enabling rapid iteration, low-cost testing, and modular upgrades.