The interval from 10% maximum initial pressure (or thrust) to web burnout, with web burnout usually taken as the aft tangent-bisector point on the pressure–time trace is called as
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Web burnout marks the end of useful combustion, and burning time is vital for performance prediction.
Burning time refers to the duration during which the propellant grain is actively combusting, measured typically from the point of significant thrust onset (around 10% pressure) to web burnout.