I have a question.
I noticed that TAI lists the Hürjet's payload at 2,721 kg. However, KAI says that it's T-50 (which uses the same engine as the Hürjet) has a payload of 3,740 kg.
Is the difference in payload due to different design decisions? For example, did KAI focus on reinforcing parts of the airframe (e.g., wings) to enable the greater payload? Or is TAI planning to develop a more fighter-like variant of the Hürjet that would have heavier payload? I know TAI is positioning the Hürjet as a 'light attack aircraft,' but is it in the context of the current variant?
@Cabatli_53 @Nilgiri @Nutuk