Nice one! It says from 110m primary position with 25 knot headwind MTOW is 32 tons and 0 wind its 28 tons
However the secondary 195m position is not compete, what is the MTOW with head wind of 25 knots and what is MTOW in no wind from this longer position? I reckon they could do 32 tons from this position without head wind and maybe more if there is head wind, but what is the maximum take off weight for J-15?
Well it claims it can do the Su-33s MTOW of 32 tons at the 195 position without headwind, so if they had headwind, they can't do anything more than MTOW, that is to say, the structure of the aircraft won't support anything heavier. (It's called "maximum" takeoff weight for a reason )
Btw 9 ton internal fuel load doesn't seem right
I think the Su-27SK has an internal fuel load of 9.5 tons. Having looked at some forums with Russian aviation followers, they say Su-33 has a slightly larger wing fuel tank. Of course, the wing is also designed with a folding mechanism, reducing fuel volume. Add the two together, and you get a final internal fuel load of about 9 tons.
Remember, the flanker is a massive aircraft.