Nope... Su-33 & J-15 have
far too low T/W ratio for takeoff length to make much difference. I have extensively looked into it, but not a single exception I've found.
You can tell yourself whatever helps you cope
but you cannot provide a single photographic evidence of such "taking off with full load from the long position".
I looked for information,
The take-off trajectory of a ski jump has an "up-throwing section". When the aircraft leaves the ship, there is an upward velocity component. At this time, the aircraft's lift is not enough to offset the acceleration of gravity, so the aircraft's ascent speed gradually becomes zero and gradually changes. Is negative.
But before falling back to deck height, there is at least 4 seconds of extra space time. With the maximum afterburner, it is enough to accelerate to the normal take-off speed, so the aircraft can fly.
Obviously, the stronger the acceleration capability of the aircraft (the greater the T/W), the safer the skid-jump takeoff, because the greater the speed off the ship, the more speed vectors will be thrown up, and the more time left for the same time. The greater the acceleration within
In general, when the wind speed on the deck is 25 knots, the su33 can take off at two shorter take-off points at 28.2t, which means that at this time, the su33 can obtain the same take-off weight at the short take-off point at the long take-off point. weight
When the deck wind speed is 0, su33 can take off at 27.0t at two short take-off points,
The normal take-off weight of the su33 is 26.6 tons. It is not full of fuel or full of bombs. Its combat radius is about 700 kilometers. It can take off normally at a short take-off point with zero wind speed.
su33 can take off at 32.8t at the long take-off point with 0 wind speed on the deck