5 foot UAV (2025-26):
(expected ~20 lbs payload capacity) (current design)
After working on RC planes and other unmanned projects in middle school, I became frustrated by how little space and flexibility there was for meaningful systems integration in most commercial UAS platforms. I began designing this project as a modular heavy lift UAV focused specifically on payload integration, onboard compute testing, and rapid hardware iteration, while still keeping the platform cost efficient.
The airframe includes two 50×50 mm mounting hardpoints (which also support 30×30 mm and 20×20 mm patterns) and four 1×1 inch side mounts to accommodate a wide range of payloads and sensing equipment. Internally, I included three power rails: 22.2V for propulsion, 12V for onboard compute (Jetson), VTX, and higher draw sensors, and 5V for most logic and low power sensing systems (there is also isolated 3v3 for GPIO).