GTRE GTX 35VS Kaveri

I'll tell the you problem with your thought process & approach . This bit of news you're posting about the Kaveri achieving ~ 1400°C is unverified for the GTRE given severe limitations of testing & calibration facilities will not be able to verify these parameters for a substantial amount of time if they go in for a change of blades / blisks.

What this means is they've conducted preliminary bench tests for limited periods of time . It was the same with the Kaveri engine ~ 2010 where bench tests were fine , also HAT tests but the moment this TF was mated onto the FTB & tested , it developed the now legendary screech , flutter & other issues with the AFB (?) .

It's only once they get it tested on an FTB they'd know where exactly they stand . For that , the previous experience is something which will have more than necessary bearing on their decision making process. What if this model also develops similar or related issues ? That'd mean they return to the drawing board & start reworking the design .

The last time it took them a good 8-10 years plus SAFRAN consultancy before they overcame these issues. And time is a luxury they cannot afford especially since the project has already dragged on for ~ 4 decades now for little fault of theirs .

Hence discretion is the better part of valour. They went in with tried tested & proven solutions of lesser calibre instead of experimenting & here we are .

Agreed to most part. I searched alot but didn't find anything significant to say dms4 is proven tested certified but rather found other thing thing abt it which I have already shared on this threads that's all is there in public.

the sameer kamat chief of drdo provided this data dms4 i suppose they have performed limited testing given what infra they. But still impressive then.

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This one is from dmrl folks themselves.
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DMS4 is in same league as 3rd gen CMSX10, Rene N6, and TMS75. DMS4 offers 1140°C TET compared to 1104°C of Rene N6 (f414), 1135°C of CMSX10, 1110°C of TMS 75 and 1150°C of TMS 196.
This raw number i.e without TBCs & intricate coolings channels.
Dms4 is in same league if we had to go by the papers published by dmrl folks papers. Also they have patented it.

Whatever they made public in those parameter i suppose dms4 is quite advance 3rd gen alloy.
And this was developed in 2013.
I have heard it was produced in existing facilities of hal koraput and with existing YSZ coating.
But I didn't find anything in that regards either.
Just that one SS on claiming to outperformed sukhois engine turbine blade and vanes. Which I had shared already. Nothing available in public wheather those dmrl made al31 blades & veins were tested it al31 (inflight as well) Or not.

So yeah here we're without much available we can just speculate.
Anyways expect good progress as this dms4 were developed in 2013 since then alot of iterative progress would have had happened.

And for jv I think posts sum up why
Why drdo desires jv i have no idea most likely mistrust of the policy makers in them. Lack of confidence of babus in drdo. few years back they were facing issues with small nirbhay cruise missile engine.
Unfortunately , at the moment it seems like that . Moreover with the kind of perverse no risk strategy pursued by the MoD babooos , any slight setback in the program were it to be run indigenously will immediately see a cessation of funds .

Hence the thinking within the DRDO establishment must be - why risk it ? Go in for a JV , run the program in parallel with the meagre funds at their disposal & get all those tech which DRDO is unable to realise due to a paucity of funds thru the JV.

This thinking is also the result of what I've pointed out in a post on the Economy sub forum wherein a majority of these babooos are of a non technical background.
 
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GTRE folks are on record stating it takes 3 years for a single design iteration as they have to wait for slot to test on Russia Test beds, which can only be applied for after the Engine has passed all ground level tests.

If a FTB were to be available within India, the same design iteration can be completed in about a year
 
GTRE folks are on record stating it takes 3 years for a single design iteration as they have to wait for slot to test on Russia Test beds, which can only be applied for after the Engine has passed all ground level tests.

If a FTB were to be available within India, the same design iteration can be completed in about a year
Aree sar sab bahane hai. Govt kehte hai GTRE kuch nahin karte, GTRE kehte hai govt kuch nahin karte , bus loopp main din nikalte chale jayenge
 
Gov se puccho ab tak Kitna funding and test facilities gtre ko mili hai.
Gtre doesn't have a fault in this case at all
who ever be at fault, but atlast our armed forces facing a problem.

Does ever any general dare to ask govt why they not giving facilities to GTRE.
 

Good summation of recent events concerning the Kaveri TF / KED .
 

Good summation of recent events concerning the Kaveri TF / KED .
Without FTB and HATF , these all shall reduce to academic exercise.
 

View: https://youtu.be/AvpaxTVVQW4?si=NHMnnweiQptlzEI1

Looks like we may get our JV partner for the 120 KN TF for AMCA Mk-2 in the next 2 months as per this video quoting Dr Samir Kamat.

Jv is just jumla french or British won't give us engine tech even for insane amount of money TOT is just jumla for babus
we should hire scientist and western expert from RR , GE or saffran their employees might be willing to share full tech and help us work through it for right prize
If china is hiring western operator to train thier sf and nato pilots for training of thier airforce who can say Western scientist are not working on chinease jet engine project or thier aviation industries or thier military industrial complex
 
Sv kamat also said AMCA mk2 will enter production in 2035.
Reiterating the fact that there given timeline is just to avoid any future backlash incase if AMCA project gets delayed.
That could very well be a misunderstanding too. Mk-1a is due to take to the skies by 2029 . Unlike LCA Mk-2 , this program WILL definitely take 5 years for FOC certification which takes us to 2034.

Add a year or 2 for LSP & another 2-3 years for mass production which in any case will be between 40-80 nos ( as of now we're projected to get 40 nos AMCA Mk-1 ) but I'm of the view the nos could go up.

In any case there's no way the AMCA Mk-2 will begin air trials before the Mk-1 has been certified or is on the verge of certification. Then there's the 120 KN TF which needs to be realised.

If the Mk-2 actually begins its air trials with the F-414 instead of the 120 KN TF it is supposed to get , it simply would mean we'd be duplicating efforts which in turn pushes back the FOC further.

So , if everything goes right we can expect the AMCA Mk-1 to receive FOC by 2034-35 & go in for production within a year or two from the date of the FOC & as far as the Mk-2 is concerned hopefully the 120 KN TF materialises by 2035 & the FOC of the Mk-2 happens by 2040 following which it goes in for production by 2042.
 

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