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I answered you why F 110 with higher thrust can not used in AMCA/MWF and GE 414 EPE or Proposed new Kaveri (Or whatever name it may have) shall be used in AMCA and How it will enhance the Performance of the Duo. Provide the Referance of 3X life.

When we planned to used proposed new engine, defense experts said that it will reach the top speed of 2600 KMPH i.e 2.15 mach revised from 1.8 mach with GE 414. Now extending same logic, MWF may also have significantly higher performance with proposed new engine. More importantly, higher dry...

Do you know that we have chosen GE 414 for AMCA and we have a plan to use Proposed 75 KN dry /125 KN after burner in AMCA 2? That engine will make AMCA fastest 5th generation plane. Now look at the Dimension of Both the engines. General Electric F110 Wikipedia https://en.wikipedia.org › wiki...

Borrow, but or steal. We need a good engine at any cost. A 75 Kn Dry and /125 KN + afterburner is the need of hour. If we are able to make this engine and put into MWF or AMCA, the platforms' capabilities will enhanced significantly. MWF can substitute MKIs in many roles. It will be a far...

To fir Aap Ke munh mai ghee Shakkar.

Baba kalyani had said that India can make its own engine witching next 7 years if we focus properly in different technologies. We have not been able to finalize a Joint venture nor we are focusing on developing our own technology. How can we make our engine realized? I remember that Antony said...

Yes, this is a land where rishis got enlightenment from almighty which spread across in different form. We have the science to make engine god who can tell us how to make engine like Ramanujan's godess used to tell her about maths formulae.

GE 414 EPE with significantly more power has same dimensions as GE414 IN 6. It has 1% better fuel efficiency. If power comes by improving design and metallurgy, it is possible to omprove power and fuel efficiency together.

125 KN does mot matter much because it is the highest thrust with Afterburner. 75 kn dry thrust is very impressive and can significantly improve MTOW if airframe so provide.

Thumb rule is MTOW=Dry thrustX0.25 in Tons. Tejas has 54 kn Dry thrust engine. 54X0.25=13.5 Which is MTOW of Tejas Mk1. However, Modern fighters due to its superior design exceeds Dry ThrustX0.30 MTOW. Example is MWF. 58/17.5>3. This ratio is too high for MWF which some times forces me to...

There is a news that a JV dith safran is getting finalized for 75 kn/125 kn engine for AMCA. I am highly impressed with dry znd Afterburner thrust. If we will put this in Tejas Mk2, It will become super Tejas. Now, we should make fifth generation Tejas with TVC kaveri. This 75 kn/125 kn matches...

No infact Russia is willing to share many Technologies but India is not interested. Russia is poor in electronics and jet engine Technologies. They don't produce the best stuff. This is the reason why India is more and more enclining towards west and US.

I think it is not a big Challenge 2 develop the the material of cold areas I.e. areas prior to combustion chamber. However, it is very difficult to to make the material of hot areas where the temperature goes above 1600 degree centigrade. Here the main challenges are making of those parts...

We are making more and more building blocks of Kaveri engine ready by developing new technologies used in aero engines. New crystal blades, thermal coating, new fan design, new burner design etc. are becoming ready. we should keep developing it by investing more money and manpower. Evenif we...

Everybody will rush to help us when we are about to make it. Nobody except Russia will help till we are about to realize this Technologies. US offered us patriot when we were Successful in making AAD and PAD. They offered us javelin when we succeeded in Nag etc. If US offer us engine...

Excellent. I never knew that engineering college of my city does such a nice work. I knew that it is a good college but this is very special.

No idea but these Odisha building blocks for making bhai trust engines. The limitations we faced in making kaveri operational can be e overcome with these technologies which includes lower weight, higher trust , sustainable performance, vibrations under control, no deformation of blades...

Annular combustor and new fan designed which is capable of giving compression ratio of 5+ and air velocity above 1556 m per second and temperature above 450* Kelvin. Now many buildings blocks of jet engine are ready. Once the reliable coating material is developed, we will be able to achieve...

New fan and combustion chamber design work is about to finish. This will help in making kaveri a high thrust engine.

only because US will not transfer the technology untill we are very close to achieve that. There are numerous examples of that. Even they blackmailed us for Jaguar engine by quoting exorbitant price. When we successfully developed Nag, they came up with the offer of Javlin. When we tested AAD...