Hi, I am part of a university project for launching a high altitude glider onboard a sounding rocket. We are considering using a pixhawk 2.1 cube as the flight computer but after a while of searching I am unable to find out if there are and G-limit constraints for the pixhawk and/or the onboard IMUs.
Specifically, the flight computer used would have to withstand 22Gs of acceleration when the payload is launched in the rocket. Can anyone give me an answer to my question? or suggest further steps I can take to find out whether or not we could use the pixhawk 2.1 cube in this application.