I know it's fantasy at this point but how would swapping the F101s out for F135s change that?
Alright
@sferrin, while the fact sheet lists the max gross as 477,000 lbs. the heaviest we launched them at DY was 450-460,000 lbs., which was with max internal fuel, 205,000 lbs., 16-24 GBU-31's and/or a forward bay tank at 20,000 lbs. We may have launched one with two forward bay tanks and 8 GBU-31's. The takeoff roll took most of the runway and the climb angle was quite shallow, shallow enough for us to wonder if they'd clear the mesa ridges in Buffalo Gap since they took off to the south. It's also worth mentioning that once the fuel load gets above 180,000 lbs. CoG becomes a concern, so something needs to be in the forward bomb bays.
Anyhow, the fantasy presupposes that the airframe could handle 40,000+ lbs. of thrust without several thousand pounds of structural reinforcement, otherwise they are flat rated engines that only improve performance for higher density altitudes, but I digress... Assuming they could handle the thrust and that the gross weight stays the same, the empty weight would still be more than the listed 192,000 lbs., worst case scenario let's say 200,000 lbs. Full internal fuel would give a useful load of 72,000 lbs., after 24 GBU-31's that leaves maybe 18-20,000 lbs. for the external pylons and weapons, AGM-158's weigh a lot more than GBU-31's so any way you cut it 14 external AGM-158's will trade significant internal fuel, that doesn't even consider CoG.
All of that to say, even with 30-40% more thrust, assuming it's even available, all of that extra drag would make for a long takeoff roll, slow climb and low cruise altitude. Range would suffer pretty bad as well since the 135's have a far lower BPR and would burn a lot more gas.
That's my gut feel without digging out the performance annex and backing out any aero coefficients to come up with some rough numbers. Can't even remember if the -1-1 has tables for externals.