In Apollo Mission Rules and Saturn V Flight Manuals, I have seen the following abort rules:
I understand what most of this means -- if the launch vehicle begins turning at more than 4 degrees per second, abort is indicated, and so on.
However, in the Max Q region (50 seconds to 2 minutes after launch, so really the "high Q" region), an angle of attack of "100%" is grounds for abort. I'm used to angle of attack meaning the angle between the vehicle's long axis and the airstream, and given in degrees, not in percentage.
How should I interpret "Angle of Attack (Q α) = 100%" in this document?