^ Nice catch, I’ve seen that pic before and only noticed now there was a dual rack on the centre fuselage pylon.
Also note the random rocket launcher on the inner wing pylon where fuel tanks usually sit… so clearly they can at least carry something other than tanks.
http://forum.keypublishing.co.uk/showthread.php?p=1814789#post1814789
But does that mean the PLAAF’s J-10As didn’t want/need PGM/stand off capabilities on their own aircraft, if it’s only for export? ie; is the pic we saw showing a trial run rather than operational aircraft in PLAAF?
Like more stories of Chinese espionage attempts?
Yeah I believe that.
I think he meant that it’s more complicated than simply getting info to copy — it doesn’t really make sense seeing as they have HQ-9.
It said the espionage involved tech and maintenance documents — possibly to supplement insufficient russian cooperation on maitenance or what not, given previous chinese experience? Clearly china’s not trying to clone S-300 and the idea it’s for integrating with the rest of the system/maintaining existing batches is more logical.
I don’t see how S-400 is relevant here, though didn’t China partially fund that project or something?
Still waiting for JH-7 internal fuel figures, guys, hook a brother up.
And just ignore teh trolls.
Not sure we have solid figures like those in the public domain? :/
listen we know you want to compare JH-7 to aircraft of a different generation..but let us not fool ourselves, the JH-7 is the same generation as the Jaguar, Mitsubishi F-1, Mirage F.1. It just came later because China was behind technologically, but now as you can see that while they may not be at the same level as the US, especially engines, that with the J-20, they reached parity with Russians.. at least in the fixed wing combat aircraft area.
Oh I think it’d be one generation after the likes of jaguar surely. Let’s not heighten this discussion on the respective country’s aerospace industries… We’ve all seen how bad that turns put
@JSR jh7 can carry up to four stand off weapons on four pylons, leaving two spare on each wing for sraam or other munitions, centerline for fuel tank and a dedicated space or a targeting pod… There is surely some substance in that..
You seem to have big issues with the claim about th PGM number dropped at that blue sword exercise — it was only a rumour, you could always ask for clarification if you have issues with it. Rather that than comparing SMT with jh7 rofl..
I more or less equated the JH-7A to the A-6.
Supersonic vs subsonic?
What happened to the colour of nozzles ?
Cloud cover.
Please don’t kill me, but from this angle it really looks like the offspring of mig1.44 and berkut. 🙂
*runs away*

Lol we should be able to call t 50 a flanker raptor love child then :p
It is true that a circular shape is a good reflector… if it is made reflective. I rather think they leave the sphere transparent (i.e. without the reflective gold layer or so), and goes for RAM treatment on the stuff inside instead. The glass sphere is an important part of the lens system, isn’t it? Then it can’t be faceted if they want to keep the optical properties
F-35’s EOTS, the superhornet proposal’s IRST and sniper pod are all faceted too.
No one is going to accept this BS logic that WS-10 production cannot be increased as hardly 10 J-11 fighters are added a year. China high end industrial sector is in decay. It cannot complete anything on time. Look at ARJ-21 and compare it with SuperJet.
Everything new coming out from Russia is way better. I am still waiting for TVC equiped fighter from China .
I’m not very familiar with the PLAAFs orbat updates but I’m pretty sure somewhere around a regiment (28) of WS-10 equipped J-11Bs are entering service per year, since 2009, 2011. (?)
I think the chinese high end sector is only starting… you can’t really decay before you reach a peak.
Not sure how a comparison ARJ21 and superjet would be useful either.
Sure, but what have Russian Car industry to do with Aviation prospect?
Russia should do what they do best.
Pls do not derail the thread.
The state of the chinese industry in relation to its aviation industry is perfectly relevant to the PLAAF. Manufacturing, sub contractors, RD, money to invest and buy.
Replying to madrat’s comment about the chinese ability or inability to make ~100 high end engines per year, the strength of the overall chinese industry/economy and its overall trajectory will of course influence how long “quite some time” turns out to be.
How many WS-10s is shenyang liming producing a year anyway?
It seems every year the Russian fanboys have fewer and fewer things to gloat about.
Let them have their moment with their current engine manufacturing edge boasts, they have precious little else to be pleased about.
If anything, China should be amused that it’s advancement is getting the Russians so worked up. You don’t see them feeling this insecure around the Indians do you? :rolleyes:
C’mon plawolf, let’s not further this useless contest.
Dude, pls produce a reliable source to prove that Russian Aviation Industry is worse of than Chineese Aviation Industry.
Overall industrial base and their respective trajectories, not exactly aviation industry alone :/
Problem now with WS-10 seems to be they can’t make enough of them.
even if we dont know the length of j10b, which we kinda do, we should know the lengths of either: j7e, jf17 or the pl8 under the j10b’s wing or pl5e under the jf17’s wing. Using pl8, j20 is between 20,38 and 20,04 meters long, depending on whether we use 2,95 or 3 meters for pl8. using pl5e’s dimensions we get 20,27 meters for j20.
That sounds about right.
We can keep splitting hairs and bargaining over centimetres all day, but the key point is that the tail fin trailing edges on the J-20 protude *significantly* less beyond the nozzles than the tail sting on the Flanker or the tail planes on the Raptor. The fact of the matter is, based on the J-7 (IMHO the most accurate reference, given the uncertainty surrounding the JF-17 and the extensive modifications on the J-10B compared to the -A) our best guess for the J-20’s length is 20.9m.
I do not understand, there was confusion over values for J-7s length as well, shouldn’t that invalidate it as much as j-10b and jf-17?
Besides a few pages back pinko gave a good estimate of j-20s length from a picture of j-10a (both aircraft taxiing at the same positioning) and I gave myown estimate with a picture of j-20 and it’s tug, knowing the tug’s length from the manufacturers website (link now broken) — both measurements gave ~20.5 m, closer to the 20m mark.
Some people round these parts HAVE linked the two, however.
I dunno about here, but most other forums realized it was a cover about six months ago…
You were kinda preaching to the choir.
“whereas the J-20 does not have anything extending much beyond the nozzles.”
Look again. The canted tail stabilizers extend out about a metre or more from the nozzles which itself extend out partly from the main body (unlike the F-22). Don’t forget also that the overall shape of the F-22 and T-50 are relatively wider than the J-20.
A meter? I don’t think so, more likehalf a meter, 75 cm would be closer.