Chinese Radar Developments - KLJ series and others

Blitzo

Lieutenant General
Staff member
Super Moderator
Registered Member
It's not "decently powered". It's a weak AESA. It may very well be weaker than all comparable AESA systems in other countries. There's plenty of evidence for that. It's also irrelevant for a multitude of factors which influence tactics and operations more than radar range.

For example Rafale will be able to generate more power because it has two engines meaning it can better manage power load to sustain high energy emissions. F-22 will be able to generate even more power.
  • J-10C / ~90kN engine / ~10t empty weight
  • F-16 / ~80kN / ~8,5t
  • Rafale / 2x ~50kN / ~10t
  • F-22 / 2x ~115kN / ~20t
  • F-35 / ~125kN / ~13t
This is very simplistic (mostly wrong) comparison because it doesn't account for energy threshold for generating lift but it gives some idea about how energy corresponds with radar power.

Aircraft with more power will have more powerful radars because it doesn't make sense to build an expensive and heavy (AESA arrays are heavy) radar for an aircraft that won't be able to use it properly. And let's not forget that any VLO aircraft can cut temporarily on energy use for EW while non VLO aircraft can't. And that's beside the issue of cooling, or peak power or many other factors that affect the minute details of every radar's performance.

I would say that if J-10C has AESA that is slightly weaker than F-16s SABR it's still good enough and PL-15 has plenty of viability despite lack of radar range.

Engine thrust can be a proxy for estimating the electrical power of the aircraft, but it also depends on the generator the aircraft has as the engine itself doesn't directly provide that power.
Advances in the onboard generator between variants can be made while retaining the same engine between those variants, in theory.


In any case, I agree that the J-10 family's power generation has a ceiling on it placed by its engine thrust (as all aircraft do), and that its power generation available to it is likely similar to other aircraft in its weight and configuration class (namely the F-16 family).

Though there are certainly other aircraft with lower engine thrust, lighter MTOW and smaller radomes than J-10/F-16 which would naturally have less powerful AESAs as well (JF-17 B3, LCA 1A, Gripen E etc), so I'm not sure why they aren't included in the comparison when they're arguably far more relevant to something like J-10C than F-22 or F-35 are.
 

Jason_

Junior Member
Registered Member
Extreme ranges are not that useful. They're disclosed (with all the usual limitations) because they give a general idea of the energy of a missile without revealing how much energy it actually has.

The actual engagements occur at much closer ranges but they still have insufficient probability of kill, so that threshold is being slowly moved back and forth - by extending effective ranges and by lowering Pk via EW or VLO. The "angry red circles" of military wonks and talking heads are a convenient illusion for getting grants and repeating talking points.
Scoring a kill at very long ranges is very plausible. RWR does not give range information so the target would not know it is in range or being fired upon.

Even if the target maneuvers and avoids the shot, the missile still provides value because it forces the target away from the high altitude high speed position when defending, meaning that its missile are now lower energy.
It's not "decently powered". It's a weak AESA. It may very well be weaker than all comparable AESA systems in other countries. There's plenty of evidence for that. It's also irrelevant for a multitude of factors which influence tactics and operations more than radar range.

For example Rafale will be able to generate more power because it has two engines meaning it can better manage power load to sustain high energy emissions. F-22 will be able to generate even more power.
  • J-10C / ~90kN engine / ~10t empty weight
  • F-16 / ~80kN / ~8,5t
  • Rafale / 2x ~50kN / ~10t
  • F-22 / 2x ~115kN / ~20t
  • F-35 / ~125kN / ~13t
This is very simplistic (mostly wrong) comparison because it doesn't account for energy threshold for generating lift but it gives some idea about how energy corresponds with radar power.

Aircraft with more power will have more powerful radars because it doesn't make sense to build an expensive and heavy (AESA arrays are heavy) radar for an aircraft that won't be able to use it properly. And let's not forget that any VLO aircraft can cut temporarily on energy use for EW while non VLO aircraft can't. And that's beside the issue of cooling, or peak power or many other factors that affect the minute details of every radar's performance.
The idea that fighter jet engines are too weak to power fire control radars is a complete myth. Remember that similar (non afterburning) engines power ten thousand ton warships with much bigger radars. Much more powerful SAM radars are powered by diesel generators. The limiting factor has never been engine thrust but the portion of engine power devoted to electricity generation, which is a factor in engine design independent of engine thrust.

In most cases, the ability to sustain high power radar operation is limited by cooling not power generation. The fact that the J-10C radar is liquid cooled and housed in a redesigned forward fuselage implies that it should compare very favorably to the retrofitted AESAs on the Rafale or the F-16.
 

MarKoz81

Junior Member
Registered Member
Exceed the 10k limit. Edit post to fit in. Be forced to write another 10k post to explain things you deleted. Genius.

Regardless of other parts of the post(which I generally support), this statement appears to be conflicting with visible realities.
It's not "decently powered". It's a weak AESA

It's a weak AESA as opposed to strong AESA in the same way that AN/APG-67 is a weak slotted array as opposed to AN/APG-63 which is a strong slotted array.

My point was to address an incorrect perception of AESA which is informed by American design choices which don't correspond to how either China would design its radars currently, or how US designed its radars in the past. American AESA is largely uniform as consequence of procurement of aircraft types.

AESA radars are not made equal because "AESA" is like "pulse-doppler". It's like a jet compared to a turboprop. It shifts the overall performance of radars compared to older technology but it still retains the same spectrum of performance within its own category. So it's like arguing that somehow AN/APG-67 is just as good as AN/APG-73 or AN/APG-63.

It isn't and it isn't supposed to be.

The argument of "my AESA is better than your AESA" is as pointless as it is misinformed because AESA takes the usual problem of radar and multiplies it by whatever amount of transcievers there are in the array. Processing is much bigger part of radar than ordinary people imagine. And then you have to put it in proper context of information acquisition which is EW and environment. That's another factor. Radar is a complex problem in the most literal sense of the term "complex". It's never one factor.

To answer your points:

(1)J-10c has enoughpower generation to fully utilize a standard antenna array of its size [...]

Also, from that we know, the amount of other power-hungry consumers onboard is significantly less than on the Rafale. Main array can have a significant priority.

"Enough" power is relative because AESA works differently from a slotted array. It's difficult to tell what is "enough" power without going very deep into the details which makes your entire point meaningless. We can only agree that it has enough power per PLAAF requirements which might as well be J-10A performance with some margins plus new technology. I don't know what it was. Do you?

As for comparisons - power can be intelligently managed and Rafale has two engines. For power generation two is always better than one but not economical. Rafale is intentionally expensive because it's a strategic program. J-10C is intentionally cheap.

The argument of having more electronic equipment is misleading because part of that equipment is an EW system that makes enemy radar less effective. Radar is a tool for writing on EM spectrum. It is effective in context. This is why technological progress made slotted arrays obsolete - they are less effective in context of modern EW, AESA and VLO regardless of their nominal output power. The same applies to AESA.

If your radar has more power but the enemy can negate it with EW while your EW can't negate enemy radar as efficiently then the effectiveness of enemy radar is better despite lower power. Remember that EW and passive detection work over distance of r=1 & r^2=1 while radar and active detection work over distance of r=2 & r^2=4. Balanced approach is better.

(2)The array - as far as we guess - is really well-sized medium fighter installation of its generation: around Eurofighter/Superbug. [...] area of the array(antenna) and nosecone is the basic stupid metric here - and the most obvious design optimization from the outside. J-10 is in the same area with significantly larger airframes - that counts for something.

Size of array is calculated in two ways:
  • absolute aperture size - physical dimensions
  • relative aperture size - number of transcievers
Both matter but the latter is more important for performance. Better technology allows to pack more transcievers into the array which can physically reduce the aperture size but increase it in relative terms.

This is Uttam.Arguably the worlds most advanced AESA radar. Needs only 30 rows of T/R.
640px-AAAU_of_DRDO_Uttam_AESA_radar.jpg

This is AN/APG-81. Arguably a useless piece of junk. Needs 52 rows of T/R and still sucks.
640px-AN-APG-81.jpg

Both have their R&D and production cost margins. J-10C has an array somewhere in the middle, but in all likelihood closer to Uttam than to AN/APG-81. If anything the cost margins on J-10C would made it so.

Similarly comparing refits of F-15/16/18 radars is an error. Those radars weren't intended to be refit. F-15s weren't supposed to fly that long because the planned number of F-22s was 750. F-16s are getting SABR as means of continuing sales and sustainment of product and USAF F-16s are upgraded only because F-35 is a procurement disaster. SuperHornet is a child of procurement review in early 90s that cut B-2, cancelled A-12 etc. All these aircraft got AESA back-fitted to existing radar architecture, often with incremental changes and insufficient funding. AN/APG-77 and the resulting AN/APG-81 is the "proper" AESA as far as USAF is concerned and navy was told to be happy with what they got.

Eurofighter has a mechanically scanned antenna which is also AESA so it's hard to tell how large it is because it must be able to move, losing some transcievers. CAPTOR-E is also somewhat of a mess as a system, typical for European procurement - badly funded, badly managed good technology. I wouldn't use EF as an example of anything. Rafale is more underfunded but it's more coherently developed and an overall better system at least IMO but it's a system. France accepts shortcomings to gain autonomy first and desired synergistic effect second. In a way it's closer to J-10C but it's Frances main fighter, while China has J-20 and J-16 so it can afford to cut cost and rationalise with J-10. France's system is Rafale and baguettes. China's system is all the fighters combined and possibly some dumplings.

(3)J-10 - and we more or less can see it - was specifically optimized for BVR radar performance (intercept-type mission), through the whole airframe (a bit more, and it would start smelling like a 1960s design). Direct radar performance is a part of this mission. Rafale, on the other hand, as a design outright discriminated against its radar installation.

What? This is not even wrong. This is utter nonsense. All of it.

10k limit. Moving on:

While true for realities of a2a combat - this isn't how the combat is planned.
There, units(fighters)/missiles are judged precisely through their approximated 'ranges'(several). [...]

This is close to how land mission is planned not an aerial one. Effective missile range is just one of the factors. Another is the ability to evade enemy missile from the target, as well as other planes or SAMs. Sometimes you have to get closer despite having range advantage because all the other factors negate it in combat conditions.

And then you have an entire manual on energy and flight parameters that constrains what you can and can't do with your aircraft while it's in the air.

Mission planning in aerial warfare is a complex problem because you can never just say "we'll sit here until they move". You first fight against gravity. Then you fight against the enemy. Enemy kills sometimes. Gravity kills always.

At least, it was until very recently(as late as late 2000s/early 2010s stupid fixed circles were it, as far as i know).

The fixed circles were never "it". It's a deliberately dishonest PR/marketing strategy. It works because it includes kickbacks for everyone who could challenge the narrative but didn't.

Advances in the onboard generator between variants can be made while retaining the same engine between those variants, in theory.

Upgrading generators as well as electrical system is easier than upgrading engines but it can't help much if there's already a performance limit set by the engine/airframe. And we're really speculating here because this is a question for proper data-based analysis that costs a lot of money.

Though there are certainly other aircraft with lower engine thrust, lighter MTOW and smaller radomes than J-10/F-16 which would naturally have less powerful AESAs as well (JF-17 B3, LCA 1A, Gripen E etc), so I'm not sure why they aren't included in the comparison when they're arguably far more relevant to something like J-10C than F-22 or F-35 are.

I don't know JF-17 and LCA well enough to say anything useful and I try my best not to mislead.

I know Gripen but it's a very special case involving special operations and tactics as well as Eireye AEW as part of the system. Gripen works for Sweden because of the system. This is why it failed as an export product. Not really applicable.

And to close off I'll restate my point: J-10 is not F-35 but an F-16. It's part of a system. We should measure its performance as such. War is not a beauty contest. It's a contest of practical adaptation and perseverance.

OK, that's enough. Take care everyone.
 

Blitzo

Lieutenant General
Staff member
Super Moderator
Registered Member
Upgrading generators as well as electrical system is easier than upgrading engines but it can't help much if there's already a performance limit set by the engine/airframe. And we're really speculating here because this is a question for proper data-based analysis that costs a lot of money.

I don't think we are in disagreement here.


I don't know JF-17 and LCA well enough to say anything useful and I try my best not to mislead.

I know Gripen but it's a very special case involving special operations and tactics as well as Eireye AEW as part of the system. Gripen works for Sweden because of the system. This is why it failed as an export product. Not really applicable.

And to close off I'll restate my point: J-10 is not F-35 but an F-16. It's part of a system. We should measure its performance as such. War is not a beauty contest. It's a contest of practical adaptation and perseverance.

I'm not sure if this is intended to be a straw man or if you've legitimately misinterpreted what someone else wrote, but I can't see anyone in the last few replies suggesting that J-10 is in the same category as F-35.
And in my last reply I directly said that J-10 family is in the same category as F-16 family.


As for Gripen, LCA and JF-17, my point for raising them is to illustrate that there are single engine 4.5th gen lightweight fighters with AESAs that are much more valid comparisons to the J-10 and F-16 category of aircraft than aircraft like F-22 and F-35.
 

Michaelsinodef

Senior Member
Registered Member
Size of array is calculated in two ways:
  • absolute aperture size - physical dimensions
  • relative aperture size - number of transcievers
Both matter but the latter is more important for performance. Better technology allows to pack more transcievers into the array which can physically reduce the aperture size but increase it in relative terms.
I suppose the following 2 lines is sarcastic? Or did you switch up a line?
This is Uttam. Arguably the worlds most advanced AESA radar. Needs only 30 rows of T/R.

This is AN/APG-81. Arguably a useless piece of junk. Needs 52 rows of T/R and still sucks.

Both have their R&D and production cost margins. J-10C has an array somewhere in the middle, but in all likelihood closer to Uttam than to AN/APG-81. If anything the cost margins on J-10C would made it so.
As for the J-10C radar, well we really can't say much about it apart from maybe it's 'general/overall' size and the fact it should draw/use less power compared to bigger radars in say the J-20 or J-16.
And to close off I'll restate my point: J-10 is not F-35 but an F-16. It's part of a system. We should measure its performance as such. War is not a beauty contest. It's a contest of practical adaptation and perseverance.

OK, that's enough. Take care everyone.
I don't think there were many people thinking the J-10 is a F-35 or comparing it to the F-35, not to mention just due to size and it being single engine, it kinda is a given that it's radar is smaller and therefore at the very least, should have less range compared to the radar in say J-20.
 

Flanker enjoyer

New Member
Registered Member
Exceed the 10k limit. Edit post to fit in. Be forced to write another 10k post to explain things you deleted. Genius.



It's a weak AESA as opposed to strong AESA in the same way that AN/APG-67 is a weak slotted array as opposed to AN/APG-63 which is a strong slotted array.

My point was to address an incorrect perception of AESA which is informed by American design choices which don't correspond to how either China would design its radars currently, or how US designed its radars in the past. American AESA is largely uniform as consequence of procurement of aircraft types.

AESA radars are not made equal because "AESA" is like "pulse-doppler". It's like a jet compared to a turboprop. It shifts the overall performance of radars compared to older technology but it still retains the same spectrum of performance within its own category. So it's like arguing that somehow AN/APG-67 is just as good as AN/APG-73 or AN/APG-63.

It isn't and it isn't supposed to be.

The argument of "my AESA is better than your AESA" is as pointless as it is misinformed because AESA takes the usual problem of radar and multiplies it by whatever amount of transcievers there are in the array. Processing is much bigger part of radar than ordinary people imagine. And then you have to put it in proper context of information acquisition which is EW and environment. That's another factor. Radar is a complex problem in the most literal sense of the term "complex". It's never one factor.

To answer your points:



"Enough" power is relative because AESA works differently from a slotted array. It's difficult to tell what is "enough" power without going very deep into the details which makes your entire point meaningless. We can only agree that it has enough power per PLAAF requirements which might as well be J-10A performance with some margins plus new technology. I don't know what it was. Do you?

As for comparisons - power can be intelligently managed and Rafale has two engines. For power generation two is always better than one but not economical. Rafale is intentionally expensive because it's a strategic program. J-10C is intentionally cheap.

The argument of having more electronic equipment is misleading because part of that equipment is an EW system that makes enemy radar less effective. Radar is a tool for writing on EM spectrum. It is effective in context. This is why technological progress made slotted arrays obsolete - they are less effective in context of modern EW, AESA and VLO regardless of their nominal output power. The same applies to AESA.

If your radar has more power but the enemy can negate it with EW while your EW can't negate enemy radar as efficiently then the effectiveness of enemy radar is better despite lower power. Remember that EW and passive detection work over distance of r=1 & r^2=1 while radar and active detection work over distance of r=2 & r^2=4. Balanced approach is better.



Size of array is calculated in two ways:
  • absolute aperture size - physical dimensions
  • relative aperture size - number of transcievers
Both matter but the latter is more important for performance. Better technology allows to pack more transcievers into the array which can physically reduce the aperture size but increase it in relative terms.

This is Uttam.Arguably the worlds most advanced AESA radar. Needs only 30 rows of T/R.
View attachment 111840

This is AN/APG-81. Arguably a useless piece of junk. Needs 52 rows of T/R and still sucks.
View attachment 111841

Both have their R&D and production cost margins. J-10C has an array somewhere in the middle, but in all likelihood closer to Uttam than to AN/APG-81. If anything the cost margins on J-10C would made it so.

Similarly comparing refits of F-15/16/18 radars is an error. Those radars weren't intended to be refit. F-15s weren't supposed to fly that long because the planned number of F-22s was 750. F-16s are getting SABR as means of continuing sales and sustainment of product and USAF F-16s are upgraded only because F-35 is a procurement disaster. SuperHornet is a child of procurement review in early 90s that cut B-2, cancelled A-12 etc. All these aircraft got AESA back-fitted to existing radar architecture, often with incremental changes and insufficient funding. AN/APG-77 and the resulting AN/APG-81 is the "proper" AESA as far as USAF is concerned and navy was told to be happy with what they got.

Eurofighter has a mechanically scanned antenna which is also AESA so it's hard to tell how large it is because it must be able to move, losing some transcievers. CAPTOR-E is also somewhat of a mess as a system, typical for European procurement - badly funded, badly managed good technology. I wouldn't use EF as an example of anything. Rafale is more underfunded but it's more coherently developed and an overall better system at least IMO but it's a system. France accepts shortcomings to gain autonomy first and desired synergistic effect second. In a way it's closer to J-10C but it's Frances main fighter, while China has J-20 and J-16 so it can afford to cut cost and rationalise with J-10. France's system is Rafale and baguettes. China's system is all the fighters combined and possibly some dumplings.



What? This is not even wrong. This is utter nonsense. All of it.

10k limit. Moving on:



This is close to how land mission is planned not an aerial one. Effective missile range is just one of the factors. Another is the ability to evade enemy missile from the target, as well as other planes or SAMs. Sometimes you have to get closer despite having range advantage because all the other factors negate it in combat conditions.

And then you have an entire manual on energy and flight parameters that constrains what you can and can't do with your aircraft while it's in the air.

Mission planning in aerial warfare is a complex problem because you can never just say "we'll sit here until they move". You first fight against gravity. Then you fight against the enemy. Enemy kills sometimes. Gravity kills always.



The fixed circles were never "it". It's a deliberately dishonest PR/marketing strategy. It works because it includes kickbacks for everyone who could challenge the narrative but didn't.



Upgrading generators as well as electrical system is easier than upgrading engines but it can't help much if there's already a performance limit set by the engine/airframe. And we're really speculating here because this is a question for proper data-based analysis that costs a lot of money.



I don't know JF-17 and LCA well enough to say anything useful and I try my best not to mislead.

I know Gripen but it's a very special case involving special operations and tactics as well as Eireye AEW as part of the system. Gripen works for Sweden because of the system. This is why it failed as an export product. Not really applicable.

And to close off I'll restate my point: J-10 is not F-35 but an F-16. It's part of a system. We should measure its performance as such. War is not a beauty contest. It's a contest of practical adaptation and perseverance.

OK, that's enough. Take care everyone.
Uttam> apg-81? You’re joking right? Uttam isn’t even in the same league as apg-81
 

99PLAAFBalloons

New Member
Registered Member
Uttam> apg-81? You’re joking right? Uttam isn’t even in the same league as apg-81
Sarcasm isn't always obvious on the internet (which is saddening as a Brit) but in this case it's fairly clear that he's joking, especially with the context of the rest of his post. Not even the most fanatical cases of Jai Hind believe the Uttam is comparable with the APG-81
 

Gloire_bb

Captain
Registered Member
It's a weak AESA as opposed to strong AESA in the same way that AN/APG-67 is a weak slotted array as opposed to AN/APG-63 which is a strong slotted array.
It is strong AESA within its class - stronger than average.
Classification of "proper" and improper" AESAs, which leaves ~70% of the modern air superiority fleet off the board doesn't work - even regardless of its merits.
In some parallel universe with 750 F-22s - maybe.
As for comparisons - power can be intelligently managed and Rafale has two engines. For power generation two is always better than one but not economical. Rafale is intentionally expensive because it's a strategic program. J-10C is intentionally cheap.
That's a peculiar(biased, mildly speaking) way of putting things.
Rafale is expensive because it's a low series, completely national program, which barely crossed 200 airframes. It is indeed quite a packed, "omnirole" airframe - but that isn't what we're talking about; doing so is just leading the conversation astray.
The argument of having more electronic equipment is misleading because part of that equipment is an EW system that makes enemy radar less effective. Radar is a tool for writing on EM spectrum. It is effective in context. This is why technological progress made slotted arrays obsolete - they are less effective in context of modern EW, AESA and VLO regardless of their nominal output power. The same applies to AESA.
Let's not move the argument elsewhere.
In this particular conversation, no one bothers whether "EW system makes what". We aren't talking about it. We're talking about specific radar performance. Dumb intercept profile - take off, climb, detect&classify the target, engage.
No spectrum warfare/ buzz words leading the conversation elsewhere. Radar performance.

Non-ESA arrays became obsolete because mechanical scan is tactically worse than an electronic one to the point of unfairness. Nothing more, nothing less - no spectrum warfare(even if that will later become one is a huge part of it). But there was no such term in the early 1980s, when ESAs were making first inroads onto fighters.

J-10C has an array somewhere in the middle, but in all likelihood closer to Uttam than to AN/APG-81. If anything the cost margins on J-10C would made it so.
That's a novel estimation of mid-late 2010s Chinese ESAs (and related industries, which are notorious for rather desperate US attempts to suppress them). I, however, wonder if it's a mainstream opinion.

We have no reasons to believe that J-10c radar came from a different generation of radars compared to J-20.
Similarly comparing refits of F-15/16/18 radars is an error. Those radars weren't intended to be refit.
Those radars, together with J-10 and flanker arrays, represent the absolute majority of the modern fighter fleet. So if anything - the opposite is true - until the F-35(which still isn't exactly the most numerous fighter in the world), it's the -79 which didn't really matter.
Also - no, Raytheon & Chinese institutes don't make their front ends shitty just to keep NG happy. Architecturally they're behind (because of their fighters), but arrays themselves are built on more or less similar - and often newer - underlying technology and solutions.
Also, J-10c radar isn't a refit. It came with a new, fully redesigned front section of the fighter. J-10A, as far as we know, get a completely different set.
Eurofighter has a mechanically scanned antenna which is also AESA
That's an interesting interpretation of Vixen/Captor arrays. No, they're still PD radars, just with a better directional diagram.
While Eurofighter can to a degree compensate it by using pirate - it is beyond our radar topic...
The fixed circles were never "it". It's a deliberately dishonest PR/marketing strategy. It works because it includes kickbacks for everyone who could challenge the narrative but didn't.
There is more than enough imagery of how it looked like - some decently fresh, and from all sides.
Yes, it may be weird and so on - but that's just how it was(was?). Yes, fixed circles.
What? This is not even wrong. This is utter nonsense. All of it.
Ft_uF1JaAAArFjk
I wonder why radar is so much smaller than the average fuselage cross-section. Can't help but connect it with worlds' richest IRST/EOTS fit (2 dedicated optical windows with a huge block underneath - right where normal people place radar back end).
article_64063e24c6f890_35438455.jpeg

Just to compare with the J-10C.
 
Last edited:
Top