GiantPanda
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what is the third variant? you keep making up some none existance versions of yours,
J-15 is a continous project, they have j-15s for catapult test, aesa test, new weapons system test and others tests and all require changes from small to big```where is the interim version? let me put this way, even batch 0 and batch 1 are not exactlly the same within their body```so is batch 1 the interim version of your category??
let me put this way, there is more difference between J-11B to J-15 (the current one in service) than Su-33 to J-15. again a CATOBAR capable J-15 is more than just to put an enhanced landing gear, and everyone knows the obvious reason, fundamental structure design is required in order to be tossed it of from carrier, landing gear is just one of them, so thats why I keep saying it was design since day one, as apart from the landing gear, the most important one, the structure was ready!`````all I am saying is to Sinosoldier's weird theory of 'third version', 'overlap' and 'interim' version``
to your question of 'explain why You deem these structural changes NOT important enough to warrant a new designation ' let me explain it with the example of J-11D, most people would believe that J-11D is just like putting an AESA on J-11B, no its not. it involes major changes of structure design, and SAC having a big problem of it (one of the main reasons to buy Su-35, this is other story, I want to leave it like this)```in this field (PLAAF, dont want to drag others into it, as I am not familar with their system) if when major structural changes are needed, then they will have a proper ‘立项’ and will give them an official designation like ABCD etc```in our circle we dont even call J-10B, they are all J-10C, but for the public consumption so here we go A/B/C. For J-15 apart from the landing gear, there is no major changes of its inner structure, therefore``````
弹射的计划不是在飞鲨服役之后才有的,飞鲨在原型设计上就已经考虑到位了,不只是一个起落架的问题,内部的结构早就做好准备了,没有像很多人说得那样内部要很大的改造才可以(的确飞鲨的内部和筷子还有很大差别的,因为都是为了在航母上用,不管是弹射的还是滑跃的)。现在服役的飞鲨其实稍加改动(说的通俗点讲,就换个起落架)就可以弹射了。那帮家伙早就弄过了·····就讲到这吧
There has been discussion over this. CATOBAR and STOBAR aircraft in a lot of ways are diametrically opposite. STOBAR needs a high TWR to launch itself off a ski-jump. You need to reduce weight as much as possible while maintaining frame integrity for arrested recovery.
CATOBAR aircraft have less stringent requirement for weight since the catapult provides the required trust during takeoff but there is penalty and that penalty is added weight needed on on the front of the airframe to strengthened it.
If you are designing aircraft for STOBAR carriers you would not penalize it needlessly with catapult necessitated elements. Especially since STOBAR capability is new to PLAN. You would want as light a design as possible.
Type 001A is a STOBAR carrier so this launch system will be with PLAN for many years. The Navy would not leave a less than optimal design for STOBAR carriers just to get a head start on the CATOBAR design.
I am sure the designers of the J-15 had CATOBAR in their plans all along -- China had studied and test CATOBAR first with Hermes and then had maintenance crews working with Brazil on the Foch/Sao Paulo.
But their plan is with different variants that are optimized for either launch methods. Not one plane planned for CATOBAR that would carry needless weight for catapult launching and forcing it to fly off a STOBAR carrier.