The noise floor that propulsion engineering cannot reach.
Small fixed-wing UAVs operating in low-speed, low Reynolds number flight regimes remain acoustically detectable despite significant advances in propulsion noise reduction. Quieter motors and optimised propellers have progressively reduced tonal noise — but they cannot eliminate the residual broadband turbulent noise generated by the wing itself.
This wing-generated noise is the irreducible acoustic floor. It is the unsolved layer. And it limits operational effectiveness across three high-value mission contexts: covert military ISR where acoustic detection by adversaries is a critical and combat-proven threat; urban airspace operations where community noise is a regulatory and public health barrier; and ecologically sensitive environments where platform noise disrupts the subject being monitored.
"No existing solution addresses this at the wing level. The industry has been looking at the propeller. The problem is in the wing."