If I remember correctly, Hürjet's latest updated length was 13.6m and the wing area was increased from 24m2 to 32-34m2 but what is the reason of 3 different aircrafts powered by the same engine and having similar wing areas (Gripen-E/F: 30m2, Tejas Mk1: 38m2) have such different payload values?
I'm guessing it could be a result of the number of hardpoints & how the wings are engineered?
Even though the plane with that engine is capable of higher payloads, it may not be able to carry more than a set amount at a particular point in the wing, limiting the overall capacity? The Tejas Mk1's hardpoint layout for example is far less efficient than the Gripen's (something HAL hopes to fix with Mk2), its likely Hurjet suffers from the same, to a more severe degree.
Just guessing though, I'm no aeronautical engineer.
Sounds great, the only concern is if it can take off from a shorter deck. TCG Anadolu is about 230 meters long.
Considerably shorter than the indian aircraft carrier.
I'm thinking not...but even if it could, the payload penalty would be too much.
Any other fighter is also likely to face the same problem but some improvement could be noticed if the weight of the aircraft itself were to be considerably lesser (like at least 3-4 tons lighter).