Problem to be solved: to provide a sensor unit which can be reliably and continuously driven without depending on the battery and is easy to install and use.An acoustic drive sensor unit 100 for acquiring sensor data indicative of the flight characteristics of an aircraft includes a housing, a first portion 200A having a diaphragm 112, and a second portion 200B connected to the outside of the aircraft.Diaphragm 112 includes a voice Coyle actuator 114 that receives acoustic energy from an aircraft engine and receives kinetic energy by vibration of diaphragm 112 and generates a power signal.Further comprising one or more sensors 120 provided within the housing and powered by energy from the power signal.One or more sensors 120 are configured to acquire sensor data indicative of the flight characteristics of the aircraft.Fig.2a
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