I honestly thought NG would win it, due to their performance on the B-21, but I guess that didn't really count for much.
As did I.
Now after Boeing has won we can go to the important part. Will the use the McDonnell Douglas name for this fighter, i sure hope so.
Wraith/Phantom/Demon etc?
What the Navy needs and what the Navy wants are two different things. To their credit in more recent years that gap has closed significantly. Right now what they want and how to get there quickly is a problem.
Finally NAVAIR has internalized how stealth worked. And/or had their heads removed from their ass, whichever.
@quellish's point about the logistics chain is certainly valid but I think that could be alleviated by having a "high-low" mix of carriers with F/A-XX and F-35C respectively so that the carriers only need to be resupplied with
F-110 and F-414 OR F-135 and F-414, instead of all 3 together.
You've got that backwards, boss.
F110 (FAXX) and F135 (F-35C) or F414 (Super Bug) and F135 (F-35C).
None of the Lockheed ATF proposals looked like those renderings. None had a canard for example. Those renderings fed into the expectations of the time. The perception it would be a canard-equipped, twin-tail, TVC aircraft was almost universal.
Agreed, the shock that they'd figured out how to stealth a supersonic fighter was pretty palpabable.
You can get one for the low-low price of $499.
So, not that different from current specialty law books then.
But definitely no longer something that the interested layman would be buying.
I had ruled out a single F-135 as an option, but maybe if you were not too concerned with acceleration and time to altitude, F-135 would be enough? For a strike platform, it would not necessarily be that underpowered, and there would be huge cost and logistical advantages.
A single F135 would give the notional fighter a takeoff TWR of about 0.5, and a combat (50% fuel) TWR of about 0.75. Which is about what the F-4 had in 1965.
I realize multiple people who are better informed are saying F110 (presumably two). Even if that is the case, just curious what other engine installations would be practical.
Twin F135s would make sense for something in the J36/F-111 weight class. 105,000lbs+ MTOW, and something around 90,000lbs at 50% fuel.
Twin F414s are a little wimpy
for something with a 66,000lb MTOW, nevermind something with an ~80,000lb MTOW. Even the F414 EPEs that made 26,500lbs thrust. (USN decided they'd rather take the higher-temp-tolerant EPE turbines and install them in the standard F414 to make the Enhanced Durability Engines, instead of keeping the short time between overhauls but make more power.) Twin M88s or EJ2x0s have the same wimpy problem as F414s.
Twin late F110s (or F119s) would be about right for something in the ~80-90klb MTOW range, which is about the maximum size you can operate off a carrier.
F100s are a little weaker than F110s but are better than F414s.
The question then becomes why is it advantageous to Boeing to apply that technology in their supply chain, but not on their own shop floor?
Because it would involve (expensive) highly-trained machinists setting up the parts in fixtures to drill some holes using a stupid-expensive CNC machine that Boeing would have to buy.
While Boeing's suppliers already have said machines and machinists
and are doing the parts setups anyway for the rest of the machining of those parts.