Another beauty idea, only someone did it in a model…
The Panavia Tornado with proper wings from a F/A-18.
An ugly hack of PAKFA with an F-14 set of wings and elevators.
And a cross between the Flanker and Tomcat approaching the first Chinese aircraft carrier.
I wish I had your photoshop skills. My goal is to graft the head of an Vought XF8U-3 Crusader III on to the body of an English Electric Lightning F.6 and add in the F-8E’s Y-racks with Sidewinders. Go with the overwing tanks. That would give it a front heavy load of 4 Sidewinders and 3 Sparrows/Skyflash missiles.
I have found this crazy XF8U incantation mixed with an F-4: 
In the context of F125 for a fighter, the 9K pounds of wet thrust may not be enough. However, if it fleshed out to 10-12K pounds of wet thrust it puts it right there.
We should be comparing to T-38, not F-5E. Don’t forget we’re talking existing F125, not the improved series. We aim for affordable and cheap for the trainer. If you want to expand the role to fighters then you hot rod from there.
If you are going to spring for a full afterburning F404 then you may as well opt for the non-afterburning F100 or F110 at the same price for better lifetime performance. I think the USAF is better served using an engine based on current product lines than to adopt a new engine it doesn’t use except in a few small niches.
I was hoping to combine the X-29 forward swept wing, long nosecone of the RF-5B, canard of either X-29 or X-31, the X-31 tailpipe and paddles, the F-5E QSB modified fuselage, twin tails of the Saegeh or F-CK-1, and maybe even steal something off a JF-17. It will be the F-5 frankenplane. Its difficult finding the planes at matching angles so I may freehand it later.
Okay, resorted to freehand.
I beg to differ on the F4x4 being the engine relative to the time period. One F125 can push 8-9K pounds of wet thrust. That is more than any other dedicated single engine trainer until the current generation. Most trainers topped out in the 5-6K pounds of thrust and solely had dry thrust. The JJ-9 is superior, but it isn’t really a dedicated trainer. An F125 would push a streamlined trainer similar to the T-38 across the same performance curve. Whether it can do it sufficient for the KPP is the issue. I do believe it would be lucky to do so, because the KPP threshold is ridiculously steep.
Someone did a solid nosecone EE Lightning.
I was hoping to combine the X-29 forward swept wing, long nosecone of the RF-5B, canard of either X-29 or X-31, the X-31 tailpipe and paddles, the F-5E QSB modified fuselage, twin tails of the Saegeh or F-CK-1, and maybe even steal something off a JF-17. It will be the F-5 frankenplane. Its difficult finding the planes at matching angles so I may freehand it later.
Its not a fat or slim question of choices, its about performance design. The strike fighter is going to look fat, the air superiority fighter is going to look thinner. The strike fighter has the gigantic internal bay to optimize flexibility in the load, whereas the air superiority fighter opts for more numerous and smaller internal bays.
Most of the surviving Su-24’s, Tornadoes, Lancers, Backfires, Blackjacks, and Floggers were from the 80’s and 90’s. Much newer than the F-111. It’s contemporaries, the F-14’s and MiG-23’s are mostly gone forever.
An F-5E replacement shouldn’t need more than an F125 engine. The F404 dramatically escalates the costs.
Searched out a forum for a lot of interesting photomashes:




Some better than others, but many more I did not post.
J-17.
DSI.
Nuff said.
We may as well lump F-20A, JAS39, F-15E, Rafale, Super Hornet, and Typhoon as they are LO designs
I hope they get more granular pictures.
More comparisons. May be off a few %; I didn’t get the rulers out.
9365 – WTF 😮 That… is actually slightly disconcerting.
6540 here. You get monitored much more. I am jealous!