As the rocket goes transonic and potentially supersonic, we may experience shockwave and high dynamic pressure effects that come with the supersonic regime. This task is to research the potential, if any, effects this may have on our sensors and systems. This may include, but not be limited to:
[ ] How the barometer is affected when entering and exiting local supersonic flow, and how a potential shockwave may disrupt its measurements
[ ] Does the MAX-M10S hit CoComs limits at these speeds?
As the rocket goes transonic and potentially supersonic, we may experience shockwave and high dynamic pressure effects that come with the supersonic regime. This task is to research the potential, if any, effects this may have on our sensors and systems. This may include, but not be limited to: