Validating ozone generation at -60°C and FL400 altitudes.
Role: CTO & Lead Engineer
Tools: Arduino, SolidWorks Flow Simulation, Ozone Sensors
Developing an ozone restoration payload for aircraft required the system to operate at 10–13 km altitude (Crusing Altitude), where temperatures drop to -60°C and air density is minimal.
Fig 1. CFD Aerodynamic Analysis
Fig 2. Mechanical System Layout
Fig 3. Manufactured Prototype
Validated the aerodynamic design and sensor fusion logic. Established the baseline architecture for the "In-Flight Ozone Restoration" concept (Provisional Patent work).