Mirage 2000H, MiG-29UPG, Jaguar DARIN III - Medium Multirole Aircraft of IAF

@Ashwin

Don't know the veracity of this tweet but apart from what @_Anonymous_ & @marich01 just posted above, this could be the reason for higher cost of the latest 240 AL-31FPs over previous engine(s):



FADEC😍
FADEC upgrades have been available for a long time. The Rosoboronexport brochure specifically mentions it. If this is the reason for the high cost, then the Russians are milking us maximum. This is a very minimal change for an reliable but low TTSL engine. We could have switched to AL-41F-1S with the MLU.


As usual, the journalist is wrong to equate engine order and Su-30 MLU. Its been in making for a long time. It was forecasted during the 2000s that around 950 engines would be needed in batches because of the short engine life.
 
The guarantee of flying hours in modern aviation is based on engineering. The insurance is provided on the same. And lives of pilots depends on the same.

If our experience was substantial, we would have created an indigenous Mig-21.

We have the good experience of Mig 21 and hence we choose to go for Tejas MK1 instead of copying Mig 21.
 
Jaguar Frames have a good amount of life left. We should make Afterburner HTFE with 27.5/45 class engine. HTFE designers say that 10% upward dry thrust is possible. we can add afterburner to it. We can take help of Russia in worst case scenario. If we are able to do that ion next 4 to 5 years, we can keep Jaguar operational for one more decade. The teething problem with Jaguar is its under power engine and too costly replacement. We need to work on same and keep it operational till 2040 to enable us to have a room for arrival of our modern fighters which are under development.
 
We have the good experience of Mig 21 and hence we choose to go for Tejas MK1 instead of copying Mig 21.

Our experience counts as nada, none, zero because what I am saying is that

1. Mig-21, 23, 27 & 29 have not been actually designed / engineered to be used as long as we have used them or intend to use them.

2. The OEM (Mig/UAC) will sign any paper saying that it can fly more in exchange for payments and royalties. Their corrupt practices have been seen in Algeria and Egypt. And the epic failure of Mig-35 program is the proof of that incompetence on there side.

3. Finally I would repeat again, the proof is that Russia/Soviet Union itself never used these aircrafts for these long and they were professional services. No less than ours.
 
Jaguar Frames have a good amount of life left. We should make Afterburner HTFE with 27.5/45 class engine. HTFE designers say that 10% upward dry thrust is possible. we can add afterburner to it. We can take help of Russia in worst case scenario. If we are able to do that ion next 4 to 5 years, we can keep Jaguar operational for one more decade. The teething problem with Jaguar is its under power engine and too costly replacement. We need to work on same and keep it operational till 2040 to enable us to have a room for arrival of our modern fighters which are under development.

There is no active large scale push for HTFE. If GOI actually gives substantial resources and funding, it will still take HAL atleast 5 years to get the engine ready. Then it will take another 2-3 years to test and integrate the engine on Jaguars.

This step would have made sense even as late as pre pandemic. But not now.

The most sensible thing to do is to wind down Jaguar operations as soon as possible. It's already 40 years now.
 
Heck PAF is retiring F7PGs after 25 years.

No BVR, flying coffin. Too expensive to MLU without primary user.
Regular PR talk. I don't know how 54% is an improvement. Earlier HAL used to quote 80%.

54% by cost, 80% by components. But that's licensed version, not desi.

How can there be a testbed specific for AL-31? GTRE is building a testbed for engines for upto 130kn engines. No relation to that program with Russia engine. Can it be used to improve AL-31? Why not.




HAL's project.
 
There is no active large scale push for HTFE. If GOI actually gives substantial resources and funding, it will still take HAL atleast 5 years to get the engine ready. Then it will take another 2-3 years to test and integrate the engine on Jaguars.

This step would have made sense even as late as pre pandemic. But not now.

The most sensible thing to do is to wind down Jaguar operations as soon as possible. It's already 40 years now.

HTFE is a civilian engine, it's not designed to handle fighter-level performance. A militarized version will be developed later on. Jaguar has 15 more years to go. The IAF has decided to dump the DARIN IIs though.
 
@Ashwin

Don't know the veracity of this tweet but apart from what @_Anonymous_ & @marich01 just posted above, this could be the reason for higher cost of the latest 240 AL-31FPs over previous engine(s):



FADEC😍
If I'm not mistaken HAL aims to generate 132 KN wet thrust by re engineering components of the AL-31FP much like how the Russians did enhancing the TTSL of those TFs to 6000 hrs up from the present 2000 hrs.

How are they going to manage it along with the certification process while mfg 250 odd TFs in 8 yrs , I don't know .

In any case , the present lot of the AL-31FP mfg at Koraput generate ~ 132 KN up from the ~ 124 KN it was originally designed for purely due to efforts of DRDO & HAL. Or so reports I've read claim. Hence the test bed .
 
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Desi AL-31's TTSL has not been determined yet. 117S TTSL is 4000 hours.

The IAF seems to have junked the 117S proposal; too expensive, lack of infrastructure, no executive control over the engine, very long learning curve and no patience to create a whole new line when focus is on next gen technologies, like LCA Mk2, MRFA and AMCA. Did I mention expensive? It's either the regular AL-31FP somewhat modernised with Russian assistance or the desi version.

Tech transfer is at the same level. The F414 has better production tools, tech and roadmap. If desi AL-31FP is chosen, then both engines will be at the same level in 10-15 years; ie, 100% control over the production. While we are making 87% of the AL-31FP, the F414 will initially come at 80% (minimum per contract) using 100% ToT for the production process, but with a roadmap to 100% using Indian tech.

Both engines becoming desi eventually is the main goal.

AMCA's engine will give us true next gen know-how and know-why.
 
AL-31FP currently produces 122.6 kN, developed by Saturn. The 132 kN version is made by Salyut for the Su-34, along with a 134 kN version for the J-10B/C and 142 kN version for early J-20s. People tend to confuse Saturn's and Salyut's engines.

So at this time there is no 132 kN version from Saturn available in India, at best something experimental being offered for modernization of existing engines. The desi AL-31FP will generate that much power, considered to be enough for MLU.

Russia plans to standardize the 117S on Su-30SM2, Su-35S and Su-34M. 117 meant for Phase 1 Su-57 is a different engine. We are not participating in either program.

Sukhoi and HAL could have different plans if the Su-30SM2 is going to be exported in order to circumvent CAATSA. Then Russia could produce most of the jet and engine and assemble in India for a "Made in India" sticker. Then MRO is where HAL will make their money. Perhaps an Indian + multi-national avionics suite as well.

PS: The Su-30MKI is not underpowered.
 
If I'm not mistaken HAL aims to generate 132 KN wet thrust by re engineering components of the AL-31FP much like how the Russians did enhancing the TTSL of those TFs to 6000 hrs up from the present 2000 hrs.

How are they going to manage it along with the certification process while mfg 250 odd TFs in 8 yrs , I don't know .

In any case , the present lot of the AL-31FP mfg at Koraput generate ~ 132 KN up from the ~ 124 KN it was originally designed for purely due to efforts of DRDO & HAL. Or so reports I've read claim. Hence the test bed .
Turbofans generate most thrust through their inlet fans/turbines rather than their combustion by bypassing air above the combustion chamber. With better metallurgy(thanks to Kaveri program), we've gained plenty of experience in designing inlet fans. So if MIDHANI/HAL can design a better inlet fan that can sustain higher presurre/temperature than for an engine like AL-31FP that has 112kg/s air flow, achieving 132KN or even higher(140+KN) is no big deal.

If the above happens then we need to thank our Tejas and Kaveri program. The importance of both can't ever be overestimated. Thanks to Swargiya Narsimha Rao and Atal Bihari Vajpayee for that.
 
Turbofans generate most thrust through their inlet fans/turbines rather than their combustion by bypassing air above the combustion chamber. With better metallurgy(thanks to Kaveri program), we've gained plenty of experience in designing inlet fans. So if MIDHANI/HAL can design a better inlet fan that can sustain higher presurre/temperature than for an engine like AL-31FP that has 112kg/s air flow, achieving 132KN or even higher(140+KN) is no big deal.

If the above happens then we need to thank our Tejas and Kaveri program. The importance of both can't ever be overestimated. Thanks to Swargiya Narsimha Rao and Atal Bihari Vajpayee for that.

Sometimes it's worth going thru old posts to see if anything of value is present which can aid our discussions today. This is what I located from 5 yrs ago.

Back then @Gautam was a newbie in this forum , though technically sound courtesy his background at BRF I guess . Since then he's done his MTech in metallurgy. Time for him to weigh in , I think.

Post in thread 'GTRE Kaveri Engine' GTRE Kaveri Engine

Post in thread 'GTRE Kaveri Engine' GTRE Kaveri Engine

Post in thread 'GTRE Kaveri Engine' GTRE Kaveri Engine
 
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The main issue limiting the upgrade of the MKI's engine is the end user. The IAF doesn't want to make too many changes citing the old adage, don't fix what ain't broke. When the MKI was first introduced it faced a lot of engine issues that took years to resolve, primarily because we were the only user. We faced the same issue with the auto-ejection of the seat during maintenance. Sukhoi refused to believe it was their problem until Russian maintenance personnel started getting launched into the air. Hence the need for fully qualified aircraft by the primary user when it comes to imports like MRFA.

And considering the state of our current inventory, the IAF doesn't want to risk the MKI with upgrades that can put the aircraft's future at risk via expensive committments like the 117S, although it's a significantly much safer option today compared to the AL-31FP back in the 2000s.

All of this means the IAF doesn't care much about any core upgrades with the exception of compensating for any potential weight increase during MLU, where a supposedly 5 or 10 kN upgrade per engine could suffice, that's 127 to 132 kN. They very much prefer leaving things the way they are while committing to any non-core upgrades like boosting the electrical output by 30% or so. Even then, any weight increase can be avoided or mitigated with lighter new gen avionics and composites.

The primary goal of the MKI MLU is next gen avionics, not flight performance, which is already superlative compare to all other adversary jets, never mind the fact that drones will take over from manned jets within the same period as the MKI MLU anyway. So the IAF's not gonna care much unless the core upgrade is cheap and risk-free.

Also, HAL sucks. The IAF doesn't trust them to deliver high quality stuff on their own. It's the same reason why LUH is stuck, it's worse than what it's been designed to replace in terms of maintenance, and not just by a few times, which by itself is saying a lot. Both IAF and IA prefer the Lama derivatives to it. Hence, don't fix what ain't broke.
 
Back then @Gautam was a newbie in this forum , though technically sound courtesy his background at BRF I guess.
I was never a member of BRF. Was a visitor for a long-time though.
Since then he's done his MTech in metallurgy.
Material Science not metallurgy. I specialized in ceramics.
Turbofans generate most thrust through their inlet fans/turbines rather than their combustion by bypassing air above the combustion chamber.
Correct. But this effect is more pronounced in high bypass turbofans.
With better metallurgy(thanks to Kaveri program), we've gained plenty of experience in designing inlet fans. So if MIDHANI/HAL can design a better inlet fan that can sustain higher presurre/temperature than for an engine like AL-31FP that has 112kg/s air flow, achieving 132KN or even higher(140+KN) is no big deal.
You cannot improve the performance of a turbofan by simply upgrading the cold section of the engine. Things are connected. Let's say you were to increase the compression ratio of an engine beyond the specified surge margin while keeping the same hot section, this is the chain of effects that would follow:

Higher compression ratio > highly compressed & heated air entering the combustion chamber > significantly higher temperature at the turbine entry > service life of turbine blades & flame tube starts to degrade > Engine's mean time between overhaul reduces > Engine's total service life reduces

Thus, an upgrade at the cold section of the engine needs to be backed up by an upgrade at the hot section of the engine.
The main issue limiting the upgrade of the MKI's engine is the end user. The IAF doesn't want to make too many changes citing the old adage, don't fix what ain't broke.
Correct. Say if we were to change the compressor of the engine. The new compressor has to be made compatible with the core first. That is challenging enough.

Next, since the new engine will have different surge margins & stall properties, pilots have to re-learn flying the Su-30MKI. That is just too much money to spend behind an old aircraft.
All of this means the IAF doesn't care much about any core upgrades with the exception of compensating for any potential weight increase during MLU, where a supposedly 5 or 10 kN upgrade per engine could suffice, that's 127 to 132 kN.
I think this is a reasonable expectation, assuming IAF funds this.

Sometime ago GTRE had built a low-pressure turbine fan with 100 kg/sec flow rate with a compressor pressure ratio of 5:1.
1725799145026.png

The fan had an inlet tip diameter of 820mm which is slightly smaller than the tip diameter of Al-31FP. If this fan is scaled up for use on the AL-31, that would improve the engine's performance. The pressure ratio is the same as that of AL-31's low pressure compressor. But the GTRE fan has 3 stages, while the AL-31's fan has 4 stages. This should bring in some weight reduction. Also, since we are only replacing the low-pressure compressor the engine performance shouldn't change too much.

DMRL has been experimenting with Al-31's nozzle & turbine blades for quite some time now. Infact, 5-6 years ago DMRL had produced & tested DMS4 alloy single crystal blades for Al-31:
1725800049684.png

1725799877432.png

Combine these blades with YSZ-LZ thermal barrier coating you have TET capability of 1740+ K. This around the same TET that the 117S engine has.

This is doable is a fairly reasonable amount of time. Most of these aren't upcoming tech, these have been produced in limited numbers & tested already. Only question is if IAF is willing to invest.
 
I was never a member of BRF. Was a visitor for a long-time though.

Material Science not metallurgy. I specialized in ceramics.

Correct. But this effect is more pronounced in high bypass turbofans.

You cannot improve the performance of a turbofan by simply upgrading the cold section of the engine. Things are connected. Let's say you were to increase the compression ratio of an engine beyond the specified surge margin while keeping the same hot section, this is the chain of effects that would follow:

Higher compression ratio > highly compressed & heated air entering the combustion chamber > significantly higher temperature at the turbine entry > service life of turbine blades & flame tube starts to degrade > Engine's mean time between overhaul reduces > Engine's total service life reduces

Thus, an upgrade at the cold section of the engine needs to be backed up by an upgrade at the hot section of the engine.

Correct. Say if we were to change the compressor of the engine. The new compressor has to be made compatible with the core first. That is challenging enough.

Next, since the new engine will have different surge margins & stall properties, pilots have to re-learn flying the Su-30MKI. That is just too much money to spend behind an old aircraft.

I think this is a reasonable expectation, assuming IAF funds this.

Sometime ago GTRE had built a low-pressure turbine fan with 100 kg/sec flow rate with a compressor pressure ratio of 5:1.
View attachment 36135
The fan had an inlet tip diameter of 820mm which is slightly smaller than the tip diameter of Al-31FP. If this fan is scaled up for use on the AL-31, that would improve the engine's performance. The pressure ratio is the same as that of AL-31's low pressure compressor. But the GTRE fan has 3 stages, while the AL-31's fan has 4 stages. This should bring in some weight reduction. Also, since we are only replacing the low-pressure compressor the engine performance shouldn't change too much.

DMRL has been experimenting with Al-31's nozzle & turbine blades for quite some time now. Infact, 5-6 years ago DMRL had produced & tested DMS4 alloy single crystal blades for Al-31:
View attachment 36137
View attachment 36136
Combine these blades with YSZ-LZ thermal barrier coating you have TET capability of 1740+ K. This around the same TET that the 117S engine has.

This is doable is a fairly reasonable amount of time. Most of these aren't upcoming tech, these have been produced in limited numbers & tested already. Only question is if IAF is willing to invest.
Our plan is to enhance the service life and TBO of AL-31FP(along with thrust & electrical power), so maybe upgrade of hot section could be done along with upgrading the inlet fans. But of course, at the moment everything is pure speculation and more details will come out in due time, I guess.
 
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AL-31FP currently produces 122.6 kN, developed by Saturn. The 132 kN version is made by Salyut for the Su-34, along with a 134 kN version for the J-10B/C and 142 kN version for early J-20s. People tend to confuse Saturn's and Salyut's engines.

So at this time there is no 132 kN version from Saturn available in India, at best something experimental being offered for modernization of existing engines. The desi AL-31FP will generate that much power, considered to be enough for MLU.

Russia plans to standardize the 117S on Su-30SM2, Su-35S and Su-34M. 117 meant for Phase 1 Su-57 is a different engine. We are not participating in either program.

Sukhoi and HAL could have different plans if the Su-30SM2 is going to be exported in order to circumvent CAATSA. Then Russia could produce most of the jet and engine and assemble in India for a "Made in India" sticker. Then MRO is where HAL will make their money. Perhaps an Indian + multi-national avionics suite as well.

PS: The Su-30MKI is not underpowered.
1/ The engines are called AL (Архип Михайлович Люлька) because they ALL start from a common base and design office (Lyulka). The Salyut/Saturn distinction is irrelevant as they both work within the ODK holding company.

2/ The Su-27's AL-31F will give rise to the AL-31FP, which is distinguished by the presence of vectored thrust nozzles: the power between the two models is identical... while the Su-34 is equipped with the AL-31F (Izd.99V) identical to that of the Su-27. As a result, the three engines develop the same thrust: 75.2 kN dry and 122.6 kN in PC mode. The difference lies in the presence or absence of vectored thrust (AL-31FP: with / AL-31F: without). The ‘132 kN on the Su-34’ story is the result of an (old AND unrealized) project to re-equip the Su-34 with the AL-31FM-1.

=> What's more, the Russians are transparent: Rosoboronexport even indicates on its website which engines power which aircraft.

3/ The J-10B is equipped (at least initially) with an AL-31FN, the main modification of which is that the reduction gearbox is located in a lower position (unlike the ‘Russian’ variants). This would make the aircraft slightly more powerful, although this has never been officially confirmed. There have been ‘discussions’ about AL-31FN ‘series 2’ and ‘series 3’, but to be honest it smacks more of Sino-Russian forum jibber-jabber than factual information. The J-20? No idea.

4/ The AL-41F1S (Izd.117S) is designed above all for the Su-35S. It is above all an in-depth work on the AL-31F with a new hot section in the engine. It develops 86.3 kN of dry thrust (compared with 75.2 kN on the AL-31F/-FP), 137.3 kN of PC thrust (compared with 122.6 kN on the AL-31F/-FP) and 142.2 kN of emergency thrust. Eventually, the Russians plan to standardise the Su-30SMs brought up to the Su-30SM2 standard with the Su-35S's Izd.117S, but the Su-34 should in theory switch to a dedicated variant of the AL-51F-1 (Izd.30), i.e. the second-stage (and therefore definitive) engine for the Su-57. It should be noted that the ‘definitive’ version of the Su-30SM2 with new engines is still awaited...

5/ The Su-57 in its current state has AL-41F1 (Izd.117) engines, the main difference between which and the Su-35S lies in the latter's control mode (integrated or not into the flight control system). Eventually, the Su-57M (unofficial designation) will be fitted with the AL-51F-1 (Izd.30).

In short, didn't you get anything? No problem!

Let me summarise.

Su-27/Su-34: AL-31F.
Su-30SM: AL-31FP.
Su-30SM2: AL-41F1S.
Su-35S: AL-41F1S.
Su-34M: variant AL-51F-1 (+/- long term).
Su-57: AL-41F1.
Su-57M: AL-51F-1.

In short, it starts with ‘AL’, it has a ‘1’ and an ‘F’ in the designation, but basically, it has nothing to do with anything.

As far as India is concerned, apart from a rehash of the AL-31FM-1 project (which is unlikely, and what's the point, given that it was never completed), I can't see what the Russians are going to come up with: either it'll be an AL-41F1S, but that will require a lot of work because the points at which the engines are attached to the airframe differ between the Su-30MKI (which gave rise to the Su-30SM/-SM2) and the Su-35S, or it'll be an AL-31FP on steroids but without any major changes.
 
Only question is if IAF is willing to invest.

That's actually a much bigger question. A simple engine modernization is still expensive, but changing the entire engine to something like the 117S is worth an LCH contract, not counting the engine cost to generate capabilities the IAF thinks is not worthwhile. But what makes it worse is HAL's greed. That could result in Russia withdrawing certification, which would be a serious death blow to the IAF's overall capabilities. They basically don't want to be taken for a ride by HAL.

What is problem(s) with LUH?

LUH is a light helicopter, but has the maintenance requirements of a medium helicopter like the Dhruv or Mi-17. It requires about 10-15 times more inspections than the Lama series.
 
1/ The engines are called AL (Архип Михайлович Люлька) because they ALL start from a common base and design office (Lyulka). The Salyut/Saturn distinction is irrelevant as they both work within the ODK holding company.

2/ The Su-27's AL-31F will give rise to the AL-31FP, which is distinguished by the presence of vectored thrust nozzles: the power between the two models is identical... while the Su-34 is equipped with the AL-31F (Izd.99V) identical to that of the Su-27. As a result, the three engines develop the same thrust: 75.2 kN dry and 122.6 kN in PC mode. The difference lies in the presence or absence of vectored thrust (AL-31FP: with / AL-31F: without). The ‘132 kN on the Su-34’ story is the result of an (old AND unrealized) project to re-equip the Su-34 with the AL-31FM-1.

=> What's more, the Russians are transparent: Rosoboronexport even indicates on its website which engines power which aircraft.

3/ The J-10B is equipped (at least initially) with an AL-31FN, the main modification of which is that the reduction gearbox is located in a lower position (unlike the ‘Russian’ variants). This would make the aircraft slightly more powerful, although this has never been officially confirmed. There have been ‘discussions’ about AL-31FN ‘series 2’ and ‘series 3’, but to be honest it smacks more of Sino-Russian forum jibber-jabber than factual information. The J-20? No idea.

4/ The AL-41F1S (Izd.117S) is designed above all for the Su-35S. It is above all an in-depth work on the AL-31F with a new hot section in the engine. It develops 86.3 kN of dry thrust (compared with 75.2 kN on the AL-31F/-FP), 137.3 kN of PC thrust (compared with 122.6 kN on the AL-31F/-FP) and 142.2 kN of emergency thrust. Eventually, the Russians plan to standardise the Su-30SMs brought up to the Su-30SM2 standard with the Su-35S's Izd.117S, but the Su-34 should in theory switch to a dedicated variant of the AL-51F-1 (Izd.30), i.e. the second-stage (and therefore definitive) engine for the Su-57. It should be noted that the ‘definitive’ version of the Su-30SM2 with new engines is still awaited...

5/ The Su-57 in its current state has AL-41F1 (Izd.117) engines, the main difference between which and the Su-35S lies in the latter's control mode (integrated or not into the flight control system). Eventually, the Su-57M (unofficial designation) will be fitted with the AL-51F-1 (Izd.30).

In short, didn't you get anything? No problem!

Let me summarise.

Su-27/Su-34: AL-31F.
Su-30SM: AL-31FP.
Su-30SM2: AL-41F1S.
Su-35S: AL-41F1S.
Su-34M: variant AL-51F-1 (+/- long term).
Su-57: AL-41F1.
Su-57M: AL-51F-1.

In short, it starts with ‘AL’, it has a ‘1’ and an ‘F’ in the designation, but basically, it has nothing to do with anything.

As far as India is concerned, apart from a rehash of the AL-31FM-1 project (which is unlikely, and what's the point, given that it was never completed), I can't see what the Russians are going to come up with: either it'll be an AL-41F1S, but that will require a lot of work because the points at which the engines are attached to the airframe differ between the Su-30MKI (which gave rise to the Su-30SM/-SM2) and the Su-35S, or it'll be an AL-31FP on steroids but without any major changes.

Sorry to say but most of this is wrong. Lulkya is Saturn, NPO Saturn is a merger of Lulkya-Saturn and Rybinsk Motors. Now it's called UEC NPO Saturn or just UEC Saturn. It's only a designer, not a producer.

Salyut is a producer, but also designs stuff on their own.

For example, ADA designed LCA, similar to how Saturn designed AL-31F. And Salyut and UMPO are the producers. While UMPO produces engines designed by today's UEC Saturn, Salyut went a step further and have also made their own modernizations. So Salyut's similar to HAL, in terms of how ADA developed LCA Mk1, but HAL went a step further with Mk1A on their own.

Similarly Sukhoi designs jets, but the producers are Irkut, NAPO and KnAAPO. Irkut produces Su-27UB, Su-30K, Su-30MKI, MKA, MKM, SM and SM2 while KnAAPO produces Su-27, Su-30M/M2/MKK/MK2, Su-35S and Su-57. Su-34 is produced by NAPO. So there are three of these Flanker derivative manufacturers, which explains their high rate of production. At more or less 1 regiment each, they have production capacity for 60-75 jets, which they are expanding to 100 per year. I guess it's 'cause they added the Su-57 line as well.

India works with Saturn+UMPO/Irkut while the Chinese work with Salyut/KnAAPO.

So AL-31F has two branches. One directly by Saturn with AL-31F, FP, AL-41F1 and AL-41F1S whereas Salyut designed the AL-31FM and AL-31FN families.

While the FN is used by J-10, the FM series was developed for Su-34, S-27M and Su-30M2 for the Russian air force. AL-31FM1 has a slightly increased inlet diameter of 924mm vs AL-31F's baseline 905mm, it increased thrust to 132 kN. They used a new core similar to the AL-31FP's generation which increased TTSL to 2000 hours. Then an AL-31FM2 was made for the J-20. Prototypes and early LRIP models used it. Its thrust was increased to 142 kN and TTSL was 3000 hours.

FM3 was special. It went through a long development process as Saturn's AL-41F1 did, with new cold and hot parts. It was designed to generate a thrust of 147 kN and competed with AL-41F1 for Su-57 and lost.

Salyut's derivatives are a cause of friction with Saturn who have accused Salyut of IPR theft. When it comes to India, we will obviously not use Salyut's tech designed for the FM family. Saturn's pushing for AL-41F1S for the IAF's MKI MLU, but it's obvious they will have a simpler modernization for the AL-31FP instead.

Similarly, Irkut and KnAAPO competed for the IAF MKI contract too. While Sukhoi and Irkut modernized the Su-30M with Su-37 tech, KnAAPO took their older Su-30MKK and modernised it to the same standards as MKI on their own, with pretty much the same avionics, like the Bars radar. It was called Su-35UB. After the IAF failed to show interest, they offered it to the Chinese when they were whining about J-11A being inadequate, who rejected it citing the use of experimental tech, but had different plans via J-11B.

While I never brought it up before, I'm sure internal rivalries between Irkut and KnAAPO played a significant part in scuttling IAF's FGFA, 'cause HAL had to partner with KnAAPO this time, using MKI production tech supplied by Irkut while Irkut was pressuring HAL to keep the MKI production going. And now, Irkut seems to be keen on using HAL to circumvent CAATSA for Su-30SM/SM2 while eventually placing themselves as the future partner for any new Su-57 program with the IAF. So if the IAF buys 40-60 jets, they can then circumvent CAATSA for the Su-57 as well.

When you look deeper, there's a lot of dirt under their aerospace industry. UAC and UEC were created to end such ridiculous rivalries so things are a lot cleaner now. Irkut is now called Yakovlev as of last year and has their own design bureau similar to Sukhoi. So now that there's Yakovlev and Sukhoi, Mikoyan is being subsumed into Sukhoi.