Well, it should be convenient because that is what the soviets designed it for (lol)
I've already reposted supporting material for this over and over again, it has become a bit of a chore.
But I've got a few extras to add now I suppose.
First is this famous series of charts from a chinese military magazine. The context and the magazine has never been made fully clear, but the sheer detail to which they list the various take off, range and headwind profiles makes me think it is not some numbers that have been just made up
http://www.sinodefenceforum.com/nav...-programme-news-views-44-6479.html#post247737
Second, is the book,
Gordon, Yefim (2001). Flankers, The New Generation. Midland Publishing. p. 91. ISBN 1 85780 121 0.
In it, the author supposedly states "Even using the station which afforded shortest take-off run of only 105m, Su-33 can take off easily with full fuel and weapons load."
I don't have the book, but the fellow is a fairly well respected Russian military aviation watcher, and his statement corresponds with positions held by other Russian watchers.
Third, is a book specifically about the Su-33 buy Andrei Fomin, and a relevant section is translated below:
""Su-27K with incomplete filling of fuel tanks, depending on the amount of suspended missiles " air" , ranged from 25 to 28 tons while he was starting thrust 0.9-1.0 and could take off from the 1st or 2nd starting position on the deck of the ship ( the takeoff distance of 105 m ) . With full fuel tanks and maximum ammunition missiles " air" take-off weight increased to 32 tons, and thrust was reduced to 0.8. In this case vzleet aircraft had to be made with the third starting position ( takeoff distance of 195 m ) . Hence , the aircraft could start and the maximum load it with bombs and rockets .
Despite a significant increase in landing weight , compared with the Su -27 , the introduction of a new wing mechanization and canards possible to reduce the approach speed shipborne fighter up to 240 km / h (Su- 27, usually landing with a speed of 270 km / h and only it absorbs the leveling process to 225-240 km / h , depending on the weight of the seat ) . In this case the mean free path of the Su- 27K on the deck when braking its arresting gear was to be only 90 m""
These stats correspond with the take off performance of Su-33 taking off from a carrier at zero headwind in the magazine scans I posted
Fourth, if anyone bothers goes around to a Russian military aviation forum of their choice and ask this question, you will get a host of the same answers that the Su-33 can (and even did) take off from ski jumps with full loads.
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And in your calculation, things like aerodynamics and also the all important headwind must be taken into account as well.