The Chinese authorities and CCTV are very OPSEC savvy, so it's blatant that SAC/AVIC, PLAAF/PLANAF, and/or another state organ is intentionally publicizing the manufacturing capacity SAC has built up for the J-35/A.
Question is: what for?
Some people — inevitably and mostly Westerners and Indians — will scream "Chinese psyop" in response to the quoted footage to frame the PLA as a "paper tiger" desperate to exaggerate its capabilities. Savvier bigots of that variety might add that such a "psyop" would be intended to deceive DoD planners so they'll misprioritize programs intended to counter emergent Chinese capabilities.
However, let's think about this critically for a second . . . If there are people on this board who can do a good job estimating J-20 production rates, there are going to be plenty of professional analysts at NASIC and elsewhere with access to classified reporting on JWICS capable of competently assessing J-35 production capacity with or without watching CCTV.
The intended audience of such CCTV "leaks" is not a state actor. They wouldn't need it.
A more plausible scenario is that SAC/AVIC is publicizing the massive manufacturing capacity it has achieved for spitting out J-35/A fighters because it's good for business () and good for the careers of those leading these efforts. It's no secret that under General Secretary Xi.
The PLA might not have objected to such transparency as a certain degree of disclosure would've been inevitable given the export oriented nature of the J-35/FC-31 program since its inception.
With that said, we'll see more J-35/A "leaks," especially if an export customer — blessed by Allah with hydrocarbons — has already made a deposit for deliveries. That'll be an achievement that SAC/AVIC, especially their senior leadership, will want to milk publicly if permitted to do so.
View attachment 155895
Found it, but for obvious reasons, I won't disclose the specific coordinates (should be easy tho).
This is purely for estimating the factory's size: 290m × 750m = 217,500 m². It's a big one indeed.
Notably, this is just one facility within the complex. The rendering (bottom right) suggests at least three additional adjacent factory structures.
Is there a clear image comparison between the horizontal stabiliser types? The "hinge" Vs "pivot" types, as I recall seeing in text?
There is nothing wrong with "psyops", i.e.:Question is: what for?
Pivot stabs (see F-22 as another example) on the J-35A:
View attachment 155910
Hinge stabs (see F-35 as another example) on the J-35A:
View attachment 155911
View attachment 155913
The tail sting is part of the fuselage, when horizontal stablizer is turned, the sting stays straight.
FC-31 2.0 with pivot
View attachment 155917
J-35A with pivot
View attachment 155916
J-35A with hinge type.
View attachment 155914
The horizontal stablizer is one piece in the yellow outline. The red outlined part is the hinge. There is no sting.
First prototype 31001 with hinge. When horizontal stablizer is turned, there is no sting.
View attachment 155915
The size of the composite material processing center is humongous. That is 2.7B RMB investment for 136k m2 area.Rick noted that we've never seen similar footage for the J-20. A key difference here is that the J-35 is intended for export, and this will naturally result in different publicity.
More
![]()
I made a post about the difference, probably in this thread some weeks ago. The pivot type is better in performance up to mach 1 and then better again somewhere in higher mach number. Hinge typle is better in transonic and just above mach 1. So pivot type is better overall by a good margin particularly in low speed. One quoted advantage of hinge type is its smaller size and lower demand of force needed. But by the look of J-35 and pivot type J-35A, it is not much bigger than hinge type, so hinge's advantage seems not worth for its performance. It's never about cost.Thank you both for the explanations and images, they were exactly what I was looking for.
Is there a known/speculated functional difference between the two types? I can see that pivot-type is called "fancy" and I believe hinge-type was said to be cheaper?
I understand the J-35 and J-35A prototypes suggested they would finalise with different types, but now apparently they have both settled on the hinge-type (to increase parts commonality)?
Rick noted that we've never seen similar footage for the J-20. A key difference here is that the J-35 is intended for export, and this will naturally result in different publicity.
The size of the composite material processing center is humongous. That is 2.7B RMB investment for 136k m2 area.
Titanium alloy and processing center is also a 1.5B RMB investment, altough of just 31k m2 area.
Both entered production in 2024 or scheduled to have one so.
There is nothing wrong with "psyops", i.e.:
1, there is national goal of world class military, and it's outright reporting to the population. Unlike western type democracies, ironically, there's a concept of accountability.
2, there is a certain important foreign country, which doesn't even spot anything wrong when it speaks about peace through strength, etc.
Projecting strength is important, unless you really want to use it.
Because the West keeps China's COMAC from entering their market to compete by not certifying the plane.To be frank China is still behind the West in aerospace because of the civilian sector which massively lags behind.