Kaveri Engine

Rajaraja Chola

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Trololo

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The countries of Europe (governments and citizens) are outraged that Russia has attacked a country on the edge of Europe. Why? For no better reason than that the despot running Russia wishes to conquer a democratic Ukraine and to absorb the country into a tyrranical Russian empire. India made itself conspicuous by declining to condemn this naked aggression at the UN. Of course, India is very dependent on Russia for weapons so it looks - at best - like India chose to stay in Russia's good books rather than to condemn the indefensible.

I do not think this bodes well for developing a 110kN engine in conjunction with a European partner. Neither UK nor France will be so keen on partnering with a Russian sycophant.

Unfortunate timing, isn't it, with US looking like it would waive CAATSA over S-400. If things develop the wrong way and India is viewed as a country so lacking in backbone that it will not display dissent to emperor Putin, whatever he does, what are the prospects of GE being allowed to offer 110kN engine co-development?

Time for India to start investing seriously in Kaveri?
We are perversely dependent on Russia for line items and strategic items. But the west also realises that we are a key player, in fact a heavyweight, when it comes to dealing with China. So I expect pragmatism from the west. They are no fools. And they also know that trying to coerce India will not have the outcomes they are looking for. India should use this opportunity of a financially weakened Russia to gobble up as much IP as it can from them. Upgrades of Russian equipment should be done in India using Indian tech as much as possible. And future Russian purchases should be reconsidered. The S400 should be the last major Russian import. XR-SAM should be the way forward. I do not think the 21 MiG 29s and 12 Su 30s are going to happen.
 

no smoking

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Should we see something in this year? 125KN engine for AMCA means, it's design might have to be modified a bit again
I am afraid it is the opposite. Originally, it requires 2 x 110kn to archive super-cruise for AMCA. Now suddenly, everyone starts talking about 125kn, it implies one possibility: Indian scientists realize that AMCA may be heavier than their initial calculation.
 

no smoking

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If we cant get to that tet, then why dont we develop variable cycle engine with 1900k blades.

by this method we can get somewhat closer to the next gen performance ??
Because variable cycle engine means you will need to change the engine's working model between turbojet and turbofan by changing internal physical structure when flying. It can be simplified as: you will need some material with super strength to build some small doors to move in the high speedy hot air flow. Meanwhile you need to keep the weight and cost in check.

These materials are much superior than those blade material technologies.
 

MonaLazy

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I am afraid it is the opposite. Originally, it requires 2 x 110kn to archive super-cruise for AMCA. Now suddenly, everyone starts talking about 125kn, it implies one possibility: Indian scientists realize that AMCA may be heavier than their initial calculation.
It could be that this future engine produces 110KN in Indian conditions, & 125KN in Western environment. Engine power drops in hotter climes by as much as 10% compared to cooler Europe, Russia & US where the air is denser at all altitudes, 125*.9 = 112.5. They must adopt the 125KN name for uniformity (for ease of benchmarking), clarity of purpose and also to capture the enormous leap it will be over anything within our grasp today. Said engine must generate 80-90/120-125KN in ~4m length.
 

Maveli

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Upgrades of Russian equipment should be done in India using Indian tech as much as possible. And future Russian purchases should be reconsidered. The S400 should be the last major Russian import.
Maybe we should ask to renegotiate prices for S-400 and Super Sukhoi and engine IP. Come up with some excuse about sanctions and dropping ruble values. Or whatever they came up with when they doubled the price of Vikramaditya.
 

Covfefe

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Maybe we should ask to renegotiate prices for S-400 and Super Sukhoi and engine IP. Come up with some excuse about sanctions and dropping ruble values. Or whatever they came up with when they doubled the price of Vikramaditya.
Better to go for Hypersonics. S400 is already contracted, Super Sukhoi isn't that big a challenge- govt can do it inhouse if it's willing to spend money. Hypersonics can be a real gamechanger and Ruskies have quite good development- something like Brahmos
 

Rajaraja Chola

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It could be that this future engine produces 110KN in Indian conditions, & 125KN in Western environment. Engine power drops in hotter climes by as much as 10% compared to cooler Europe, Russia & US where the air is denser at all altitudes, 125*.9 = 112.5. They must adopt the 125KN name for uniformity (for ease of benchmarking), clarity of purpose and also to capture the enormous leap it will be over anything within our grasp today. Said engine must generate 80-90/120-125KN in ~4m length.
I am afraid a engine is not designed around an aircraft with engine power drops in warmer climate assumption. The engine will be rated and tested at 125KN. And AMCA has to be designed for that range and power and not 110KN.

Even in India, we have cooler climates in North and North East. More power is required at higher altitudes (even if they are cooler) to take off.

And yes while for Mk1, it's fine, for MK2, AMCA has to undergo design mod, even a elongated fighter similar to Tejas Mk2. Let's see.
 

Rajaraja Chola

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I am afraid it is the opposite. Originally, it requires 2 x 110kn to archive super-cruise for AMCA. Now suddenly, everyone starts talking about 125kn, it implies one possibility: Indian scientists realize that AMCA may be heavier than their initial calculation.
Yes it will be. There is a reason why Koreans call their KFX 4.5th gen and not 5th gen cos it uses F414 engine with around 100KN. The turks are going with heavy engine from.the start with F16 engine rated at 130KN. I think many pointed out that 110KN engine won't be enough if AMCA want to achieve air superiority. ADA scientists have come to the same conclusion. 125KN is the right way to go about it. Better to be safe.than sorry.
 

SimplyIndian

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I am afraid it is the opposite. Originally, it requires 2 x 110kn to archive super-cruise for AMCA. Now suddenly, everyone starts talking about 125kn, it implies one possibility: Indian scientists realize that AMCA may be heavier than their initial calculation.
125kn will be 110kn in indian condition unless plan is to prepare 125kn indian condition engine ( which is 140 kn euro engine)
 

Lonewolf

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Yes it will be. There is a reason why Koreans call their KFX 4.5th gen and not 5th gen cos it uses F414 engine with around 100KN. The turks are going with heavy engine from.the start with F16 engine rated at 130KN. I think many pointed out that 110KN engine won't be enough if AMCA want to achieve air superiority. ADA scientists have come to the same conclusion. 125KN is the right way to go about it. Better to be safe.than sorry.
You know it because ? You read some op ed or you contacted scientists ??

Turks are designing tfx as a 21 meter long aircraft , not same for amca
 

Rajaraja Chola

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You know it because ? You read some op ed or you contacted scientists ??

Turks are designing tfx as a 21 meter long aircraft , not same for amca
Common sense? And this news article from The Hindu is saying a deal is expected in 2 months for AmCA deal? And Koreans calling their fighter 4.5th gen. They are refraining from calling it 5th gen.
Why so angry?

AmCA is designed as a air superiority fighter. If 125kn engine is better to achieve it with also significant load under it's belly then great. 110kn is not going to be enough.
 

Vamsi

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Common sense? And this news article from The Hindu is saying a deal is expected in 2 months for AmCA deal? And Koreans calling their fighter 4.5th gen. They are refraining from calling it 5th gen.
Why so angry?

AmCA is designed as a air superiority fighter. If 125kn engine is better to achieve it with also significant load under it's belly then great. 110kn is not going to be enough.
125KN will be an overkill for AMCA, at MTOW of 25T ,it will have T/W of exactly 1. Show me which fighter, be it a 4.5Gen or 5th Gen which had T/W= 1 at MTOW ?

Also I think 110KN will be baseline version, 125KN will be for possible future upgrades...
 

fire starter

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125KN will be an overkill for AMCA, at MTOW of 25T ,it will have T/W of exactly 1. Show me which fighter, be it a 4.5Gen or 5th Gen which had T/W= 1 at MTOW ?

Also I think 110KN will be baseline version, 125KN will be for possible future upgrades...
There was always scope for 15pc thrust increment.
 

Lonewolf

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Common sense? And this news article from The Hindu is saying a deal is expected in 2 months for AmCA deal? And Koreans calling their fighter 4.5th gen. They are refraining from calling it 5th gen.
Why so angry?

AmCA is designed as a air superiority fighter. If 125kn engine is better to achieve it with also significant load under it's belly then great. 110kn is not going to be enough.
Koreans are calling kfx as 4.5 gen because it lacks iwb , lot of antenna aren't conformal , irst in place of conformal DAS , no EOTS , plus engine .

Not just because of engine .

And you won't go mach 1.6 plus with use of external hardpoints in a dogfight , and in stealth mission , dry thrust matters more which if is near 73 kn then is good enough for it to supercruise at mach 1.5 plus in clean configuration .

So afterburner thrust is less important in stealth jets than dry thrust , if it increases the dimensions too much to increase afterburner thrust then Better settle for lower afterburner thrust initially
 

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Concard

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Because variable cycle engine means you will need to change the engine's working model between turbojet and turbofan by changing internal physical structure when flying. It can be simplified as: you will need some material with super strength to build some small doors to move in the high speedy hot air flow. Meanwhile you need to keep the weight and cost in check.

These materials are much superior than those blade material technologies.
If I am right variable cycle Engines are meant for 6th generation aircrafts. We don't even know what makes a 6th generation aircraft. The British who are working on it say they are employing Big data, Artificial Intelligence for their tempest project. But still nothing is clear as of yet. Yes the variable engine is one key difference which will distinguish 6th generation jets. And what else exactly? Americans have already learnt the hard way that 5th generation jets are expensive in terms of R & D and also to maintain and their flying cost per hour. That is why they are back to inducting more F-15's in their arsenal even though they are to receive more F-35's. Once USAF knew F-22 was eating into their budget they had to stop production of F-22's.

If 6th generation jets is all about only variable cycle engines and eliminating vertical stabilizers then we might as well stick to 5th generation jets for sometime and reduce their operating costs. The flying cost of F-35 per hour is $25,000 and that itself is expensive to USAF who have the highest budget in the world. One wonders what would be the cost of 6th generation jets.
 

ObiWanKenobi

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125KN will be an overkill for AMCA, at MTOW of 25T ,it will have T/W of exactly 1. Show me which fighter, be it a 4.5Gen or 5th Gen which had T/W= 1 at MTOW ?

Also I think 110KN will be baseline version, 125KN will be for possible future upgrades...
That MTOW will increase if you have more thrust. MTOW will shift closer to 30 ton mark if you put those engines and your T/W will remain at 0.8 or so
 

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