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It seems weird that the supercruise performance figures of the P&W powered aircraft would be the same.  Also if the figure was indeed mach 2 for the PAV-2/YF-120 combo, then I would officially be astonished beyond a reasonable doubt.  It's times like these where I wonder if the F-119 will be compatible with an ADVENT style third flowpath/extra duct for a possible future upgrade?  It might be a bit overly complex but still, one can dream. :)


Also Sundog, don't you mean the YF-23/GE combo?  It is already understood that both P&W powered aircraft achieved mach 1.43.


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