And per article posted by Austin, the latest 2 prototypes received the radar from serial production workshops of Ryazan instead of NIIP’s experimental workshop. Looks standard enough for me.
Interview with Yevgeny Marchukov, general designer of the Lyulka Design Bureau on Product 30 Engine
Some interesting notes :
1.Development target of T/W of 10:1 has not change.
2.Internal Weapon Bay capacity of Su-57 is about 4200 Kg.
3.Still hasn’t give up on flat nozzle eh.
Oh my God. 3 pages and still stick on what happened in Kashmir.
Where is the Uttam ?
I would love to know more about “Super-Sukhoi” project and how it’s going.
Should India really master AESA radar production and have industrial support for Uttam. It would be a matter of scaling up the design for MKI’s aperture. The achievable power aperture would be quite high as Su-30MKI would offer roughly 22 kW/sqm of cooling capacity for the radar. The high end of the radar using GaN module of 21 Watt peak (The value which will match the cooling capacity) will put range performance considerably over Irbis-E.
My estimate on high end of the Super-30 Radar using GaN modules.
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Even module with half power can still bring about considerable performance
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This of course assumes that the radar will feature 2700 modules as the potential aperture may provide.
For the love of God now it’s Indian airforce thread along with cache of precious photo archives.
Wait, there is one though it’s bit blurry
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The NPK-SPP apparently responsible for the whole optronics for both Su-35 and MiG-35. The T-220 targeting pod spec is thre. tho it’s hard to make anything out of the poster.
Sadly the real technical coverage would be rare. instead i would expect to see more people downplaying or exaggerate whatever avionics piece released at MAKS.
The desire of having multiple sensors and one that can still offer some performance in bad weather are strong. Everyone wants a piece from “hiding beyond the horizon only to expose radar mast”.
The only odd member is the Ka-52, but then this is mostly a naval helicopter, it will lob anti ship missile and may need radar that perform accordingly, which atm cannot be mounted on mast.
You don’t need a targeting pod for dropping dumb bombs.
joking aside are there any particular information availabme on that T-220? Is it related to the 101KS-N or something entirely different?
Entirely different. as T-220 is made by NPK SPP while the 101KS series is made by UOMZ.
Unfortunately there is no real disclosure/brochure info yet, as far as i can see.
But the targeting pod,where is the targeting pod?
If its gonna get what Su-35 got, you can be sure T-220 will be among that
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Lets also say theoretically https://ieeexplore.ieee.org/document/6217012 I have this ultra high resolution to distinguish someone’s face from 400kms away. Does resolution effect the RCS of a target? For example I have a very high resolution SAR to see a 1m2 target from 400kms away on radar would ultra-high resolution give me the ability to see a smaller RCS target than this?
Resolution helps you identify the target by distinguishing various parts of it and allow you to build imagery out of it. and no it does not affect target RCS.
Target rcs from who?
From airplane which is jammed or Rcs from own airplane?
It’s clearly the target aircraft that do the jamming.
The equation for self protection jamming presented in the book assumes that the jammer can always be in the mainlobe of the victim radar e.g you’re being locked. With this the jammer will always have the advantage of injecting its techniques which will not be/seldom noise but RGPO etc.
Target RCS have little meaning for self protection as it will always be lower in terms of magnitude of power compared to what being emitted by the jammer.
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Future works for AESA radar calculator :
-more refined path propagation
-signal processor, time to introduce what is pulse doppler or MTI.
-Clutter (Sea, Land, Rain)
-Auto PRF select (user no longer have to specify PRF, the sheet will generate it instead based on target velocity or some general requirement like 95% visibility etc) It will instead prompt user to select “High, medium or low” PRF
Evaluation of clutter and signal processor is rather bit complex and specific as it may require user to actually specify some variables like target speed. The radar equation for those can also be no longer closed term, but rather have to be analyzed iteratively. It will be somewhat like this in appearance :
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This is a simplified model i use to estimate detect ability of target in sea clutter for an anti ship missile. The simplified equation is used and as seen the target is detectable in sea state 0-4 (i skipped sea state 1 as the base data i use for the clutter model is inaccurate) With doppler or MTI processing.
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Above is the example of rain clutter evaluation , as seen i need to specify detection range first.
The way of implementation i envisaged atm is to actually use the detection range from the calculation and later “evaluate” it using the user supplied “Processor improvement factor” to see if the radar can detect the target at specified range. If it cannot detect it then the sheet will look into similar signal strength to range table as i provided in the first image, then give range value where the signal strength exceeded the required threshold which in this sheet i would assume to be the same as one in thermal noise environment.
Russian is extending the SU-57 range considerably; https://www.youtube.com/watch?time_continue=172&v=ht-buGDmupg
Are you sure you’re linking correct video ?
So Russia is able to produce Irbis in reasonable numbers, but not the AESA.
The question i am making is related to backfitting Irbis to earlier sukhoi airframes. not whether the Russia can suddenly mass produce things or not.
Given that as we see, no Su-27SM3 nor Su-30SM use Irbis. i think it’s reasonable to assume that it’s not backward compatible hence might as well wait and use AESA instead.
What you didn’t IMHO consider is that installing an AESA radar in substitution of a mechanical steered one would change completely the plane balance itself (as they are extremely nose-heavy compared to them), at the same time it would mean to have a quite limited FoV. when russians absolutely prefer to not compromise such value.
So is PESA and with PESA like BARS you’re not only dealing with antenna weight (which also considerable BTW) you also deal with weight of the hydraulics too. Let’s give an example the N011M Bars. The antenna alone weighs 100 Kg compare it with 7.9 Kg conventional slotted planar array.
N001 Pero reflective array system is lighter but still a respectable 90 Kg.
a
What do you think would be the remaining useful life of those old Su-27?
1000? No problem at all. 1500? a little extra investment on maintenance. 3000? you take them aground a week, change the tubes and the antenna and you are ready to go again.
and with AESA. no need to worry about those tube changing + It can tolerate up to 10% module loss without worry. PESA if the tubes by any means damaged, your set is practically useless.
Well, aside from Su-27SK (J-11A) Most if not all exported Flankers like Su-30MKK,MK2,MK2V still have pretty long life and can see more upgrades to be useful.
Adapting the N036 would mean to spend years into developing it, as no studies have ever made to adapt it to a Flanker even the newer ones, while the work about installing a Pesa radar are already been made but in the end not implemented for Su-27-SM3 update.
Then what makes you think adapting 20 kW irbis would be any easier than having AESA ?
And we haven’t even talked about the economics of mass production which will help lowering cost even further for Russian AESA.