*New J-10 Thread*

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crobato

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Officially, we should stop calling the two seater J-10B, but J-10S. The "S" could be the Chinese word for twin seater. Two seater J-11B might be caleld J-11BS.
 

tphuang

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Like I said before, J-10s were tracked towards Matsu trying to get ROC SAM radars to light up. These happened days before the formal announcement.

Whether or not they're photographed by US or Taiwan aircraft is probably irrelevant, especially with the tons of internet photos, news articles, declared engine purchases, satellite photos, and even model kits being sold of the thing.

At least 100 aircraft is consistent to at least 3 confirmed regiments, plus one possible and two in the process of conversion.

to Simonov, J-10 payload is 7t. At least that is what the articles are saying. 4.5t is the internal fuel load, which is quite a lot for a single engined fighter. That means plenty of endurance to keep up a fight and use its afterburners often. Remember there are planes out there on paper, has a high TWR but achieves that with a low internal fuel weight, making this paper advantage a bit moot since you can't use the ABs that often.

Now reviewing again the pic of the older FTTC J-10s up there, looks like they got the white uplink on the back of the canopy now fitted. Looks like a field upgrade.
They were talking about the empty weight of J-10 online. One of the guys who apparently has access to confidential info said that the weight is closer to 7.5 tonnes than 8. Anyhow, I don't think we've seen the end of this. I think Aviation weekly is pretty close, but still a little off.
 

crobato

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We will wait for more info. The data is from AFM, not AW. Looks like major mags will have J-10s featured for this and the next month.

The weight issue for me is an Internet invention to further seperate the J-10 from a Lavi root (Lavi empty weight is 7000kg) to something closer to the Typhoon (original prototype 9750kg). I think that was suspicious and so off the scale.

From what I know is that the J-10 has TWR parity on combat weight, though its hard to say if its 12,500kg (AL-31FN) or 13,200kg (WS-10A). The chart given showed that parity on the 13,200kg level.

And if what you're saying is true, then no surprise, 12,500kg - 4900kg (fuel and AAMs/ammo/pilot) is 7600kg. I use 4900 because 13,200-8300kg and apparently that figure is used in the calculation.

The 13,200kg combat weight is probably on the high end of it. If I were only putting 3300kg like an F-16, the combat weight is like 12,000kg and thats higher than unity even with an AL-31FN.

To Mehdi,

Yes, -BS has its own funny meaning too. But I guess the two seater J-11 may just end up being called J-11S.

Certainly the B on J-11B and J-10B has very different meanings, and we know the J-11B tag is official, and J-10B therefore shouldn't be.
 

Gollevainen

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that is with the nose probe, based on Deino's sizing. Without the nose probe, its closer to 15.5.

not just Deino's calculations, many others have done it as well...And in fact as soon as I've around my own comp. I will try it myself...
 

crobato

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But which ones have a reliable basis? Other than Deino's, I have not seen anything that you can base with an absolute standard.
 

Gollevainen

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I ment that others have done the same type of calculations before and the results have been somewhat similar. The proplem is that you need to have a picture taken straight from the side so that the plane is in 90 degree agle compared to the camera, then the optical error is minimal

so just give me a pic and I'm on to it:p ;)
 

crobato

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With a reliable standard to compare, I have my doubts on these calculations. The only ones with some merit would be to take the PL-8's length into account, or less reliably the nozzle. The PL-8's length is already documented at 3m based on the Python 3 it was copied from. I remember doing the same on prototype 1006 when an early picture came out years ago.
 
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