This is a bit off topic, but back in my engineering days one of the issues we had to deal with was stress on satellite structures due to acoustic energy during launch. When I first became aware of this, it surprised me how much energy from the sound waves was input to the structures. At the time there was no really good way (at least not that I was are of) to predict the response of the structure.
>>>The rationale for acoustic noise testing is straightforward, as acoustic energy is the primary source of vibration input to a space launch vehicle. . . . Acoustic energy is transmitted to the mission payload in two ways. First, fluctuating pressures within the payload fairing impinge directly on exposed spacecraft surfaces, inducing vibration in high gain antennae, solar panels and other components having a large ratio of area-to-mass. Secondarily, the fluctuating external pressure field causes an oscillatory response of the rocket structure, which is ultimately transmitted through the spacecraft attachment ring in the form of random vibration. . . . At the integrated spacecraft level, then, acoustic noise is a primary source of vibration excitation.<<<
The sound can be incredibly loud, and I doubt anyone will be generating 200+ decibels in a home audio system.
>>>Nasa's measurements at the time [of the Saturn V launches] captured the launch noise at 204 decibels.
The massive thrust needed to launch a rocket into space creates a lot of noise. With the launch of SpaceX's enormous Starship rocket, how loud did it get?
www.bbc.com