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Ninda ji did what a politician of Atal Bihari era use to do in his/her speeches,he probably forgot that the stage where he was making a speech was not a political one...

The dry variant is a separate version of kaveri (for the UCAV)...

As far as i know,their engine is not matured and has relatively less breakdown time conpared to 3rd gen western engine(Ex-GE404),short life span and inadequate thrust at variable altitude. The best example of their failure is the proposed Chinese engine for jf17 bl3 which was shot down by...

Not correct Su30 can achieve a greater AoA due to thrust vector than the mentioned only in certain flight regime, Rafale has 30 degree AoA, tejas trainer achieved 24 degree AoA not the single engine fighter aircraft. Higher AoA is required for higher ITR for tejas.

Not exactly, STR is still the sorrow of the project, also AoA has only been expanded to 23 degrees against 28 degrees.

Tejas is made to run on kaveri, and absence of kaveri as already stained the performance which resulted into unaccomplishment of ASQR requirements of 1998 .

Wrong, planes are designed around engines, that's why "identical" proven engine is used for testing and new engines with identical figures like air mass flow are used to replace in the production variant.

HAIL GTRE. Sent from my Aqua Ace II using Tapatalk

Someone who has little to do with offset clause and understands little what the offsets are really are can be a bit ignorant to ignore a business which is made. Sent from my Aqua Ace II using Tapatalk

Great you know more than the developers and their research papers, probably they should ask you whether to keep these words "Variable cycle engine" with Kaveri on their official website. Sent from my Aqua Ace II using Tapatalk

No one can help your BS who doesn't even know what offset clause are, French aren't fixing the problem, that's a joint work in which the money will be poured by the French for offsets that means Indians have to transfer some technology or manufacture something for French to balance the offsets...

Anyone has a little bit knowledge of gas turbine, is not replace a core of 90kN thrust engine with 75, it's not possible, the later core is much smaller in size. Flat rate is quite old yet a revolutionary concept which hardly any engines have in the current world scenario, apart from GE engines...

It would be interesting to know if any of Chinese engines are flat rated variable cycle engines rather some normal Russia engine architecture with terrible thrust to weight. Sent from my Aqua Ace II using Tapatalk

We never told the public that engine for 5th gen fighter is almost ready but engine for 4th gen fighter if getting ready. See the diff. Sent from my Aqua Ace II using Tapatalk

So that's the reason why Chinese engines are joke with terrible thrust to weight for a modern engine. Sent from my Aqua Ace II using Tapatalk

Problem is GEF404 and AL31FP, both have thrust to weight 7.8:1 by calculation, the 100kN Kaveri will weigh around 1280kgees, it won't be an improvement, and IAF will simply dumb the plan of integrating it on LCA. Sent from my Aqua Ace II using Tapatalk

Since the plan for KAVERI JET ENGINE is to bring down the weight bw 970-1150kgees and increase thrust equivalent to GEF414 , and if it adds thrust of 100kN, the thrust to weight ratio will be around 9:1 THEN IT will be same like F414 and EU200 and better than M88. But if the Trishul trident's...

We can get results equivalents to EJ200 if use 3rd gen SCB in flat rate thrust, while can match GEF414INS6 in total thrust, GEF414INS6 has thrust to weight 9:1 so if Kaveri makes equivalent to that we can do that with 3rd gen SCB . Sent from my Aqua Ace II using Tapatalk

Well for achieving Thrust to weight approx 9, or even matching the Snecma M88's 8.75:1, it's required that much heat in the hot section. GEF414 proposed EPE has thrust to weight of about 11:1, matching the 5th gen PW f135. 100kN Kaveri with 90kN flat rate limit the requirement is 1847C(2120K)as...

Kaveri needs 1800C in hot section for 100kN thrust. Sent from my Aqua Ace II using Tapatalk