I remember P&W said their XA101 can only fit inside F-35A but will have issue with F-35C that will need some development work and impossible to fit in F-35BDon’t forget the P&W XA101, which has also demonstrated the AETP performance goals.So basically F-135EEP give 10% improvement in range and thrust and 50% improvement in cooling
XA100 AETP gives 20% improvement in thrust, 30% improvement in range and 100% improvement in cooling.
Though to be fair, if they don't choose the XA100 then it likely stall the tech just like what happen to scramjet tech
But if the F-35 picks the XA101, doesn’t that also cause the same industrial base issue as retaining the F135 in EEP form?
By contrast, GE said their XA100 can easily fit in F-35A and F-35C with no structural redesign of either aircraft is required, they also study the option to adapt it on F-35B
https://aviationweek.com/shownews/farnborough-airshow/ge-studies-xa100-adaptive-engine-option-f-35b