If that's the case, how does the F-22's engine handle the high pressure in the intake when flying at supersonic speed, since a Fixed intake will not be able to control the inlet air-flow - something which the variable intake or the DSI intake would be able to handle? Furthermore, I tend to think that the F-35 is meant to be marketed among member countries, whereas the U.S. seem to keep the more capable F-22 just for themselves.


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