ADA Tejas Mark-II/Medium Weight Fighter

No that's redesign of the same airframe. It's more complicated, like how our Sainik sir wanted the pylons shifted on MWF. Not possible for to structural strength reasons.

However designing a derivative based on a larger fighter is possible, like La'vi. Actually one exists for the very Rafale you cited as example.
It's the Novi Avion of Yugoslavia created by Dassault consultancy.

View: https://m.youtube.com/watch?v=kKabJF3uFecView attachment 20733


My concept ALCA was on similar lines as the Novi Avion only.

You may not convert a legacy Tejas LCA to stealth, but you can convert a stealthy AMCA to a single engine light fighter based off it. as our Sainik sir opined HAL/ADA should have done much before. I'd even come up with isometric views from al 3 sides.
editamca1-copy-2_1_orig.webp
55.webpamca-aero-india-2013_1_orig.webp
 
Very 😆 a complete redesign from scratch... you can't just draw lines & expect it to work!

They tried to alter the Rafale & call it TEDBF & now everyday it looks more like Rafale


ADA/ADE intentionally benchmarked TEDBF against Rafale. So it is pretty much Indian version of Rafale with slight difference.
 
My concept ALCA was on similar lines as the Novi Avion only.

You may not convert a legacy Tejas LCA to stealth, but you can convert a stealthy AMCA to a single engine light fighter based off it. as our Sainik sir opined HAL/ADA should have done much before. I'd even come up with isometric views from al 3 sides.
View attachment 20765
View attachment 20767View attachment 20768

I'm avoiding DSI due to more stealth hence the only other option is of F-22.
- 1 engine of F414 class or AL-31/41/F-100/110 class initially. If USA gives just the F135 engine then nice :ROFLMAO: But still F-35 TWR is not like F-22.
- 2 side intakes to make some IWB & SWB.
- IWB can carry 4 BVR-AAMs or 2 AGMs. Each SWB can carry 1, may be 2 CCMs, depends on size.
- half length all-moving rudder which can be researched into tail-less or rotating rudder-stab.
- Wing shape & size not determined yet.
- Some people might want canards for Naval model.
The 1st/top one's fuselage outline looks like cousin of Su-75 (F-22 inlet cut half width-wise)
The middle one like child of Su-57 + F-22 :facepalm2::facepalm4: (F-22 inlet cut half height-wise)
The below one like younger sibling of F-35 (F-22 inlet reduced to 1/4th quadrant)
NOTE: These are notional & not to scale.

1736087411932.webp
 
I'm avoiding DSI due to more stealth hence the only other option is of F-22.
- 1 engine of F414 class or AL-31/41/F-100/110 class initially. If USA gives just the F135 engine then nice :ROFLMAO: But still F-35 TWR is not like F-22.
- 2 side intakes to make some IWB & SWB.
- IWB can carry 4 BVR-AAMs or 2 AGMs. Each SWB can carry 1, may be 2 CCMs, depends on size.
- half length all-moving rudder which can be researched into tail-less or rotating rudder-stab.
- Wing shape & size not determined yet.
- Some people might want canards for Naval model.
The 1st/top one's fuselage outline looks like cousin of Su-75 (F-22 inlet cut half width-wise)
The middle one like child of Su-57 + F-22 :facepalm2::facepalm4: (F-22 inlet cut half height-wise)
The below one like younger sibling of F-35 (F-22 inlet reduced to 1/4th quadrant)
NOTE: These are notional & not to scale.

View attachment 20777
You can look at Mitsubishi X-2 shinshin for inspiration. Although it got 2 engines they are of half the thrust of F-414 class with 25kN dry and 50kN wet. It also got some 13-Ton MTOW which can be increased i think.
 
You can look at Mitsubishi X-2 shinshin for inspiration. Although it got 2 engines they are of half the thrust of F-414 class with 25kN dry and 50kN wet. It also got some 13-Ton MTOW which can be increased i think.
Personally i'm twin engine jet minded. Redundancy is good thing & if 1 engine fails then other engine should be sufficient to make the jet RTB (return To Base) safely.
But some people also prefer 1 engine jet in medium weight category due to less maintenance cost & time. So i'm putting up these. Otherwise these same frontal notions can be assumed for twin engines also.
 

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