ADA Tejas (LCA) News and Discussions

Which role suits LCA 'Tejas' more than others from following options?

  • Interceptor-Defend Skies from Intruders.

    Votes: 342 51.3%
  • Airsuperiority-Complete control of the skies.

    Votes: 17 2.5%
  • Strike-Attack deep into enemy zone.

    Votes: 24 3.6%
  • Multirole-Perform multiple roles.

    Votes: 284 42.6%

  • Total voters
    667
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Pulkit

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The budget is dependent on requirement and is not absolute.
Current allocations does not support your statement IAF, IA and Navy all said they needed more funds and the budget was insufficient.
If there is a requirement, there will be higher budget. Why assume that budget is made arbitrarily without keeping needs in mind?
Not assuming just check the last 10 years budget allocation any deal which goes into billions is troubled. Remember Rafale original deal People were concerned how were they gonna pay for it....
Yes, Kaveri is capable of being used. Though I am not sure if it will be for Tejas MK1 or Mk2.
My guess would be Tejas Mk1
I don't think a new engine is being developed for Tejas MK2 but instead the Kaveri itself will be made into 100kN engine by modifications.
French have said it cannot go beyond 90KN
Also, making an engine for just 120 planes appears to be meaningless. Tejas Mk1 will be discontinued and replaced by Tejas Mk2 as soon as possible. MK1A is just an attemt to develop the subsystems and technology which can be used in Mk2
agreed....
 

Pulkit

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Even if it clears all tests, Kaveri is still not suitable for Mk1/Mk1A because the current thrust of Kaveri is lower than F404!
F404 was to fill the gap and was more than what the IAF originally wanted for Mk1. As they say currently Kaveri is at 80 KN will it still not be sufficient given F404 is 85KN
Also, mating Tejas & Kaveri (even if lower thrust is acceptable) will push the schedule by 4-5 years!!!!
4-5 years is doubt though yes it will take some time but remember the original design was for Kaveri only later modified for F404.

this is just a hypothetical scenario.
 

Kshithij

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Current allocations does not support your statement IAF, IA and Navy all said they needed more funds and the budget was insufficient.
No one says that funds are enough no matter what. India is planning long term, not short and hence the idea is to develop technology and make strategic purchases that provides technology which will be used to make indigenous items in the future. So, the intention is not to buy items to improve short term strength but to buy items with ToT and reverse engineering ability to get technology. India has Su30 manufacturing wnd can make its own planes when needed.

F404 was to fill the gap and was more than what the IAF originally wanted for Mk1. As they say currently Kaveri is at 80 KN will it still not be sufficient given F404 is 85KN
Kaveri is 81-84kN with flat rating and variable cycle. Flat rating means that the thrust is deliberately reduced to maintain a flat peak thrust across altitude and variable cycle means that te bypass is changeable. So, 81-84kN would mean 100kN in normal terms. Why are you ignoring flat rating and variable cycle? WHat kind of engine ever uses bypass ratio of just 0.16? 03-05 is the standard bypass and 0.16 is only the least bypass value.

French have said it cannot go beyond 90KN
When did France tell this? Also, do you think India will not look at the design of F414 and the cooling vanes and other items used to optimise Indian design?
 

Pulkit

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No one says that funds are enough no matter what. India is planning long term, not short and hence the idea is to develop technology and make strategic purchases that provides technology which will be used to make indigenous items in the future.
But you need to pay the bills. Imagine your expenses are more than your salary how will you plan to save for a house or car? when you cannot even pay installments. you wont... and same is the case with our forces when they dot have enough why will they put money in tech development.
So, the intention is not to buy items to improve short term strength but to buy items with ToT and reverse engineering ability to get technology.
Reverse engineering is not the field where we excel and to maintain superiority on the ground we need to buy.
India has Su30 manufacturing wnd can make its own planes when needed.
Assembling is not manufacturing.
Kaveri is 81-84kN with flat rating and variable cycle. Flat rating means that the thrust is deliberately reduced to maintain a flat peak thrust across altitude and variable cycle means that te bypass is changeable. So, 81-84kN would mean 100kN in normal terms. Why are you ignoring flat rating and variable cycle? WHat kind of engine ever uses bypass ratio of just 0.16? 03-05 is the standard bypass and 0.16 is only the least bypass value.
Its not perfect like Tejas like you said... perfect match
When did France tell this? Also, do you think India will not look at the design of F414 and the cooling vanes and other items used to optimise Indian design?
Its been quoted multiple times. Read between the lines in the article...
http://idrw.org/how-90kn-kaveri-and-125kn-kaveri-engine-projects-will-be-game-changer-for-india/
 

ersakthivel

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No one says that funds are enough no matter what. India is planning long term, not short and hence the idea is to develop technology and make strategic purchases that provides technology which will be used to make indigenous items in the future. So, the intention is not to buy items to improve short term strength but to buy items with ToT and reverse engineering ability to get technology. India has Su30 manufacturing wnd can make its own planes when needed.


Kaveri is 81-84kN with flat rating and variable cycle. Flat rating means that the thrust is deliberately reduced to maintain a flat peak thrust across altitude and variable cycle means that te bypass is changeable. So, 81-84kN would mean 100kN in normal terms. Why are you ignoring flat rating and variable cycle? WHat kind of engine ever uses bypass ratio of just 0.16? 03-05 is the standard bypass and 0.16 is only the least bypass value.



When did France tell this? Also, do you think India will not look at the design of F414 and the cooling vanes and other items used to optimise Indian design?
To achieve 100 KN, & to increase bypass ratio to 3&4, we need far higher Turbine Entry Temperature (TET).

Because mass flow increases with higher bypass ratio, we need to withstand different OPR Operating Pressure Ratio as well.

Do we hv the Tech to design SCB to withstand higher TET,,,,


And finish the trial & certification in time for mk2,,,

I don't think so & neither it is going to be an easy & quick process.

If French help us, the process may even be within our grasp.

But do French hv the tech I hand,,,,

Will they give TOT or just supply us the finished core, ,,

No nation transfers its strategic cutting edge know how for any price.

Who wants to handhold a competitor in business ,,,

But will it arrive in time for mk2,,,,,
 

Kshithij

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Reverse engineering is not the field where we excel and to maintain superiority on the ground we need to buy
How did you conclude this? Reverse engineering is much easier than developing one's own items. Revserse engineering does not mean exact replica but just getting ideas and understanding concepts

But you need to pay the bills. Imagine your expenses are more than your salary how will you plan to save for a house or car? when you cannot even pay installments. you wont... and same is the case with our forces when they dot have enough why will they put money in tech development.
What bills one has to pay? Stop watching too many hollywood movies speaking of USA lifestyle.

Assembling is not manufacturing
Su30 is manufactured and assembled in India. do you have problems in english?

Its been quoted multiple times. Read between the lines in the article...
http://idrw.org/how-90kn-kaveri-and-125kn-kaveri-engine-projects-will-be-game-changer-for-india/
By unreliable source which has been disproven. Read the article you have and read the statement of french president. French president has denied any Kaveri engine development with M88 core as given in the article. So, the article is fake news.

To achieve 100 KN, & to increase bypass ratio to 3&4, we need far higher Turbine Entry Temperature (TET).

Because mass flow increases with higher bypass ratio, we need to withstand different OPR Operating Pressure Ratio as well.

Do we hv the Tech to design SCB to withstand higher TET,,,,


And finish the trial & certification in time for mk2,,,

I don't think so & neither it is going to be an easy & quick process.

If French help us, the process may even be within our grasp.

But do French hv the tech I hand,,,,

Will they give TOT or just supply us the finished core, ,,

No nation transfers its strategic cutting edge know how for any price.

Who wants to handhold a competitor in business ,,,

But will it arrive in time for mk2,,,,,
India makes Al31F engine fully 100% from raw material stage. This is similar to F404 and M53 engine of Mirage2000 in technology levels and is one level below F414. So, India is not starting from scratch but ahs good enough expertise in making engines already. Prior to this, India made R25B engine for MiG21 in India.

India has the technology of SCB but will use 2nd generation DS as rhenium is difficult to obtain during wars and if engines are made from SCB, then during wars, India will not be able to procure engines in mass scale due to lack of rhenium.

The most important aspect of TET is from thermobaric coating and design of cooling vanes in blades. Coating gives an advantage of 300kelvin TET while cooling vanes can improve that by 100Kelvin. So, total of 400 kelvin is increased because of coating and cooling. SCB offers advantage of 40Kelvin per generation and hence total of 80 Kelvin for 3rd generation over 1st generation SCB. The 2nd generation DS on the other hand, has 10-15Kelvin better temperature handling than 1st generation SCB while the maximum difference is 70Kelvin less than 3rd generation SCB. Comparing engines like EJ200 which has TET of 1800-1850 Kelvin, Kaveri of 100kN thrust needs a TET of 1730K which is easily obtained without any SCB and weight of 1200kg (EJ200 weighs 1000kg for 90kN and is more efficient than Kaveri).

The TWR of Kaveri will be lower than that of EJ200 or M88 but will be higher to F404 and there will be lower lifespan for Kaveri but it will be still be good enough.

I have already answered you question a few days back. Here is the post:
https://defenceforumindia.com/forum...-news-and-discussions.1/page-842#post-1442358
 

Pulkit

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How did you conclude this? Reverse engineering is much easier than developing one's own items. Revserse engineering does not mean exact replica but just getting ideas and understanding concepts
Firstly its unethical to do that but keeping that aside I m not expert but even a expert will tell you that reverse engineering it not easy had it been everyone would have made everything. Leave everything aside you said we have been building engines for long then why are we not able to build a stable core for Kaveri. We can reverse engineer anytime right???
What bills one has to pay? Stop watching too many hollywood movies speaking of USA lifestyle.
Bills: Salaries/Fuel/Rationing/ammunition/Installments those come under category of bills.
I wont stop watching any less Hollywood movies and will suggest you to avoid personal remarks.
Su30 is manufactured and assembled in India. do you have problems in english?
You can believe what ever you wanna believe. what % of Su is indigenous?
My problems with English is nothing of your concern. Again asking you not to make personal remarks.
By unreliable source which has been disproven. Read the article you have and read the statement of french president. French president has denied any Kaveri engine development with M88 core as given in the article. So, the article is fake news.
there would be many sources and you need not believe them and I am not here to convince you either.
 

Kshithij

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I m not expert but even a expert will tell you that reverse engineering it not easy had it been everyone would have made everything. Leave everything aside you said we have been building engines for long then why are we not able to build a stable core for Kaveri. We can reverse engineer anytime right???
Reverse engineering is not exact replica but understanding the ideas and concepts and thus reducing time for lengthy trial and error process. Also, India did not have access to high end engine technology, metallurgy to simply get things done quickly. Without infrastructure, it is not possible to reverse engineer. Also, Kaveri has been designed after understanding other engines and not imagined from scratch. But, due to UPA cutting funds, Kaveri could not even get a test bed and GTRE chief was saying in Aero-India 2009 that funds are being cut or delayed and test bed is not being approved. Kaveri will be built soon and in next year will see flight as this government has been supportive

Bills: Salaries/Fuel/Rationing/ammunition/Installments those come under category of bills.
Everyone knows this. Budget is allocated according to needs of fixed payment and additional capital for technology acquisitions.
You can believe what ever you wanna believe. what % of Su is indigenous?
Engine, airframe, avionics are fully indigenous. BARS radar is also indigenous but may not be fully indigenous. a few items like IRST, EW, ejection seat, minor parts like nuts and bolts and raw materials like titanium for airframe is imported. Except for IRST, India can make other parts but still import due to contractual obligations. Otherwise, Su30 can be made fully indigenously except for IRST
there would be many sources and you need not believe them and I am not here to convince you either.
Fake news must not be considered as sources. There is no news about Kaveri being developed with M88 core from either India or France but simply a fake news by detractors who don't want India to have indigenous engines and instead want to exert pressure on India to import foreign core
 

Sancho

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In your dream 90kn will not be enough for tejas
Yes only in my dreams or by the fact that IAFs rejected the Kaveri / Snecma engine in the first place, in fact IAF had doubts if the joint engine will reach 90kN at all and if there actually was a joint development, or simply a replacement of Indian parts with French once. You could also add the fact that ADA itself required up to 95kN for MK2 and let's not forget that this requirement was made nearly a decade ago! In the mean time, LCA got heavier and heavier and the MK2 initially was not planned in the medium class either. So if they Base it now on the weight and performance of the Mirage, 90kN obviously can't be enough for MK2.
 

abingdonboy

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So MMRCA 2.0 is a just smoke screen in disguise to order more Rafales later.
Smokescreen makes it sound like there is something nefarious about the intentions.

Instead it is a simple procedural affair that bean counters insist upon and politicians are happy to oblige to cover their a$$es.

You cannot buy 100+ fighter jets with localised production, ToT, after sales support etc etc that could cost upwards of $15bn through a govt-govt deal, at least not in the Indian set up. This would be a guaranteed red flag for CAG. You need to go through a price discovery process, you need to have competitive bidding, you need to reasses the competition. Remember MMRCA 2.0 kicked off about a decade ago now, none of the original bids are relevant anymore from an economical and technological perspective. The Rafale the IAF has ordered is VERY different to the Rafale offered under the original competition. But the terms the GOI got for the G2G deal we’re not conducive for a much larger order.

As the PM himself said, those 36 were for the immediate needs of the IAF. others will follow.


Sancho’s analysis is off, the govt has done far from “anything but to order the rafale”. Sorry pal, but this is laughable, €7.8bn tells a different story. You don’t shell out that kind of taxpayer money
 

Sancho

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It’s based on requirements, there is more TOT going to Europe rather then other way around.
Any tech development is based on requirements, but the US prefered to develop just a longer range AIM 120, while Europe understood that speed not range is the key and developed Meteor.
Same goes for WVR missiles, where Europe started developments of HOBS missiles as a reaction to R73 and because AIM 9 was inferior and when you see how many customers prefer European missiles over AIM 9X, you will understand where the know how is.
 

Sancho

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I know it's french plane, I'm talking about design
Other than the delta wings, they don't share anything design wise. High wing on LCA vs low wing on the mirage, air intake positions, different twin seat design, weapon station layout similar to Jags...
 

Enquirer

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Trishul dude is suggesting that Tejas Mk1A will have Levcons! According to him the flight of Naval version was to complete the Levcon test, so it could be incorporated into Mk1A.

While I have always argued that Levcons should be part of Mk1A, I am not so sure if Levcons could be incorporated into Mk1A in the timeframe (that's left). Trishul guy is known to blow a lot of hot air!.
Levcons will lead to significant changes in the FCS - which was not anticipated in Mk1A!
(unless HAL/ADA have been working away at this for the last 2 years!)
 

ersakthivel

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Yes only in my dreams or by the fact that IAFs rejected the Kaveri / Snecma engine in the first place, in fact IAF had doubts if the joint engine will reach 90kN at all and if there actually was a joint development, or simply a replacement of Indian parts with French once. You could also add the fact that ADA itself required up to 95kN for MK2 and let's not forget that this requirement was made nearly a decade ago! In the mean time, LCA got heavier and heavier and the MK2 initially was not planned in the medium class either. So if they Base it now on the weight and performance of the Mirage, 90kN obviously can't be enough for MK2.
Air marshal Mateshwaran, who headed the, "rejection" committee, once opined

Why only 6 stages on kaveri,,,,,
increase it, to 10 or 12, it doesn't matter, all we need is more thrust.

He is oblivious to even the simple fact, that modern jet engines derive higher thrust,

by increasing thermodynamic efficiency, through higher TET,
& operating pressure,

there by reducing stages & engine weight,,

Because what matters I not just absolute thrust, but engine thrust to Weight ratio.

Kaveri is shorter than GE 404,


Such genius being given appointed to head the committee, to evaluate, snecma GTRE jv

has made IAF & GOI a laughing stock around the tech world,,,

Because Pratt & Whitney guys who hv experience In variable cycle engines inspected kaveri & said it is a world class engine,

even the French don't hv kaveri's variable cycle jet engine technology, the same tech which powers F22

That says a lot about the, "technical capabilities" of IAF review committee headed by Air marshal, "Matheswaran".

Goto Bharathrakshak kaveri engine thread & read a few of, Maitya's post about what design changes will unleash the full potential of kaveri, before placing expert here.

Just because your old favorite forums went belly up, don't litter DFI with falsehoods.
 
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Enquirer

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Because what matters I not just absolute thrust, but engine thrust to Weight ratio.
Not quite!
If a 20% (say) increase in thrust can be achieved with 20-30% increase in engine weight, then the engine thrust/weight ratio would remain same or get worse! But it's inconsequential!
Because the AIRCRAFT thrust/weight ratio would see a major boost (as engine is only a small part of the aircraft weight!)
As such, a ~300 kg increase in Kaveri weight might be totally acceptable if it came with a 20% boost in thrust!
 

ersakthivel

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Not quite!
If a 20% (say) increase in thrust can be achieved with 20-30% increase in engine weight, then the engine thrust/weight ratio would remain same or get worse! But it's inconsequential!
Because the AIRCRAFT thrust/weight ratio would see a major boost (as engine is only a small part of the aircraft weight!)
As such, a ~300 kg increase in Kaveri weight might be totally acceptable if it came with a 20% boost in thrust!
Modern jet engines get,

Higher thrust from better SCB blades,

withstanding higher tubine entry temperature,

leading to higher thermodynamic efficiency, due to higher energized mass flow,

Produce the same thrust for lesser fuel,

& these engines come smaller & lighter especially.

Heavier weight, lower thermal efficiency, bigger size, fuel guzzling engines,

Increase both the radar,heat signatures of the fighter,

Along with higher fuel needs, leading to spiraling weight gain of the fighter.

They r the past, not future

Certainly not the future of jet propulsion.
 

Kshithij

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Not quite!
If a 20% (say) increase in thrust can be achieved with 20-30% increase in engine weight, then the engine thrust/weight ratio would remain same or get worse! But it's inconsequential!
Because the AIRCRAFT thrust/weight ratio would see a major boost (as engine is only a small part of the aircraft weight!)
As such, a ~300 kg increase in Kaveri weight might be totally acceptable if it came with a 20% boost in thrust!
The TWR of engine is also about fuel consumption, optimal thrust for weight class of plane etc to optimise range. Bigger engine means smaller fuel tank in the plane, thus lower range. Bigger engine consumes more fuel for sustaining itself and hence more fuel wasted to sustain itself rather than propel the plane. The fuel conumption per unit thrust goes up even though TWR stays same as more fuel is needed to maintain engine due to overall increase in dimensions and moving parts
 

Sancho

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Just because your old favorite forums went belly up, don't litter DFI with falsehoods.
I would highly recommend to you to read more and inform yourself, no matter where and from whom, because you have a clear lack of knowledge and understanding for sure. I don't need to go to other forums, since my aim is always to seek and "share" credible infos wherever I am =>

The delinking though is not the end of the road for the Kaveri. A committee headed by Air Vice Marshal M. Matheswaran, has been asked by Air Headquarters to scrutinise an offer made by the French engine house Snecma to co-develop and co-produce an engine along with the GTRE.

Snecma will have to convince the committee that they can indeed co-develop with the GTRE, an engine with a thrust of around 95 kilo kN. Crucial aspects like the transfer of technology to GTRE, number of engines to be produced and costs involved will be studied by the committee.
https://defenceforumindia.com/forum/threads/kaveri-engine.5097/page-119#post-1382731
 
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