I believe that the original topic about HAL Tejas's Cost Vs Performance thing is more or less finished.
Now this thread, if it proceeds, is going to talk about unrelated issues (and off course, I have no issues with that).
Actually, J-10 data needs revision:
As per wikipedia (which many people here don't trust) ... still:
Loaded Weight = 18,500 kg
Empty Weight = 8,850 kg (average of the range given on wikipedia).
As a formula I have used, Useful Weight = Loaded Weight - Empty Weight
(for all aircraft)
However, for J-10, another figure called "Useful weight" is quoted in wikipedia as 6000 kg.
So, possibly useful weight of J-10 is not 9650 kg, but 6000 kg, and it will then lie between Eurofighter and Sukhoi30MKI.
18.5 tons is quite a heavy aircraft to run on a single engine even though the engine used - AL31FN is quite a large engine (much larger than eurofighter's engines).
The empty weight of J-10 (= 8850 kg) is quite comparable to other single engined aircraft (One less engine does save weight !). But to carry a loaded weight of 18.5 tons, I think J-10 was better designed as a twin-engined aircraft.
I am beginning to suspect that J-10 could be underpowered with it's single engine.
(And this is a great statement to invite flaming and lead to closure of this thread).
Try to remain calm .... HAL Tejas can be BS on lot many features, too.
So, can be US / Russian or European fighters (You may have heard about Gripen's crashes, Sukhoi30MKI crashes). No aircraft if perfect on everything.
I am really keen to know the maximum AoA of J-10 (from a reliable source). Have not been able to find.
I'll write what I know:
HAL Tejas = 28 degrees (tested upto 24 degrees, as of now).
Sukhoi 30MKI = 50 degrees
F-18 Super Hornet = 58 degrees
Can anyone compile AoA of all the aircraft ?