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I curious what happens when you open the missile bay doors positioned right before the inlet at Mach 3. How does that affect the airflow at those high speeds.


Also, to prevent hot gas injection, the missile release mechanism would have to be similar to F-22, with the missile separating from the aircraft before igniting its engines. And all that at twice the cruising speeds of F-22 and 30 years prior to it. WOW!

I just see some big technical difficulties there.


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