The idea of thrust augmentation, if that is what we are now talking about, is very different from gas dynamic stabilization. Separately, the augmentation of jetex motors and our current solid rockets motors is also very different. The thrust augmentation of jetex motors was documented in the jetex literature and would have some meaning for such low thrust, long-burning motors. Our solid rockets motors burn very short and the time for heating incoming air is short, too. Many or all of the jetex motors consisted of a pin-hole nozzle exit, which also acted as the throat, meaning that the motors were highly under-expanded. This could mean that there was a lot of external aft-end surface area on the jetex motor for incoming air to mix, be heated, and exert a positive forward thrust. These conditions are not as abundant in our solid rocket motors.