J-15 carrier fighter thread

Axyan

Just Hatched
Registered Member
Hello everyone,

I'd like to discuss an issue regarding the J-15. The J-15 has a major flaw: its 3x2 pylons, including the wingtip ones, are located on the outer, folding section of the wings. This means the J-15 cannot be armed with weapons unless its wings are unfolded, which severely impacts deck operational efficiency. In contrast, aircraft like the F/A-18 series and the F-35C have most of their hardpoints on the non-folding section. This results in the J-15 having only 6 "quick-load" hardpoints available in its folded state: the 2 under-intake pylons, 2 wing-root pylons, and 2 centerline fuselage pylons, in addition to the 6 non-quick-load pylons on the folding wing sections.

Furthermore, there's another issue: the non-folding wing-root pylons can interfere with the main landing gear, imposing restrictions on the shape of the munitions.

However, I recently saw a diagram showing that the J-15T (the catapult-capable variant) has further reduced the width of its folded airframe from 7.4m (on the Su-33/J-15) to 7.1m. Doesn't this exacerbate the problem? Is this diagram authentic? What could be the reason for such a modification?
 

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by78

General
Just a cool image, nothing more.

54626458694_1266037a63_o.jpg
 

4Tran

Junior Member
Registered Member
Hello everyone,

I'd like to discuss an issue regarding the J-15. The J-15 has a major flaw: its 3x2 pylons, including the wingtip ones, are located on the outer, folding section of the wings. This means the J-15 cannot be armed with weapons unless its wings are unfolded, which severely impacts deck operational efficiency. In contrast, aircraft like the F/A-18 series and the F-35C have most of their hardpoints on the non-folding section. This results in the J-15 having only 6 "quick-load" hardpoints available in its folded state: the 2 under-intake pylons, 2 wing-root pylons, and 2 centerline fuselage pylons, in addition to the 6 non-quick-load pylons on the folding wing sections.

Furthermore, there's another issue: the non-folding wing-root pylons can interfere with the main landing gear, imposing restrictions on the shape of the munitions.

However, I recently saw a diagram showing that the J-15T (the catapult-capable variant) has further reduced the width of its folded airframe from 7.4m (on the Su-33/J-15) to 7.1m. Doesn't this exacerbate the problem? Is this diagram authentic? What could be the reason for such a modification?
I don't think that the PLAN thonks this is much of a problem. It might hurt sortie rates a bit but the sortie rates on Liaoning and Shandong are already pretty decent. In any case I'd much rather get inro a fight with J-15Ts rather than Super Hornets.
 

ACuriousPLAFan

Brigadier
Registered Member
I know the Chinese saying, just cautious of that off-chance of it being the nails of the coffin.

Uh no?

To be specific, the idiom 板上钉钉 means something has already been decided or fixed upon, which is always used as positive or neutral terms. It's not the same as the phrase "nail in the coffin", which means something is doomed/certain to fail or end in bad ways.

In fact, in the Chinese-speaking realm, I have never seen anyone using the 板上钉钉 in negative ways. If anything, the English correspondence to 板上钉钉 would be "set in stone" or "the die is cast", whereas the Chinese correspondence to "nail in the coffin" would be 致命打击 or 催命符.
 
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sunnymaxi

Major
Registered Member
Uh no?

To be specific, the idiom 板上钉钉 means something has already been decided or fixed upon, which is always used as positive or neutral terms. It's not the same as the phrase "nail in the coffin", which means something is doomed/certain to fail or end in bad ways.

In fact, in the Chinese-speaking realm, I have never seen anyone using the 板上钉钉 in negative ways. If anything, the English correspondence to 板上钉钉 would be "set in stone" or "the die is cast", whereas the Chinese correspondence to "nail in the coffin" would be 致命打击 or 催命符.
so it means WS-10 with J-15T has finalized ?? right.
 
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