Hindustan Fighter
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currently how many mig 21's are with IAF ?
250 at least not sure about the exact figure
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currently how many mig 21's are with IAF ?
With slightly more than 1 billion for the engine to move from 7.5 to 9 pounds of thrust, at the request of Abu Dhabi.
But Gogbot some of the compoents in Euro and Typhoon is also US made and we always have the risk of facing Seaking type of debacle..
Yes Mirage was the original choice, but MoD seems to want more, also we asked Quatar for their M2ks before, but they wanted a way to high price for them, so why should this be different now?
Personally, I thought to buy the UAE M2k-9, instead the upgrade of our M2ks would be a good idea. Half of them are pretty new and it is known that these are upgraded with techs and weapons that not even the M2Ks of French forces had.
I see some interesting equation here.
1. For all we know that French are helping us to improve the Kaveri Engine, which will come to same thurst.
2. Will Rafale actually with UAE invest another 1 billion to make another type of engine. They can use Kaveri if its proved to be succesful. What could be the best choice at this time that India-UAE-France investing on something like Kaveri to make it F4 engine!!!!....
3. If this can somehow get to drawing board then rafale will have an even get into a partnership, Now you share the profit incurred by the engines developed.? Possible??...
4. This will lead Rafale to make an even stronger pitch. Earlier we were seeing it as a bilateral partnership, it can be trilateral and also it will have monetary benifts.
5. I mean french already said they can fit Kaveri to Rafale so fit it to UAE Rafales will not be a problem....
Prateek/Sancho/Gogbot...any comments???
Below is latest update on Gripen NG
They have increased combat load to 7200 Kg
Both fighters would offer a cost-effective high/low combination for any export country, with high commonality and a win-win solution for France and India!
We could be the perfect partner for exports with a high number of Rafales on order too, but it seems we miss this big chance, because everything takes way too long.
Yes I agree...
Good that we went for the tender process. It has great advantages to arrive at what IAF is looking for. Like Prateek said attack capability and Life cycle cost.
But my question why there is another M88 engine developement with UAE when you already have partenered with India to make an engine which can go to LCA. You are actually not diversifyingthe funds but spending unwisely. We should pitch in here btn UAE and France to convince them to invest on Kaveri engine..and use the same engine in F4 Rafale!!!....
The above picture you gave on Rafale and LCA is really a promising one.
Even if you use Elta Radar in LCA or our home grown RADAR with Israel/France who ever will still be a punch.
That's why I said, imo we are missing a big chance here, not only because of Kaveri engine and LCA, but also to be an equal partner of the Rafale.
No, just in the early testing stage, they didn't even fixed how it should look like (swashplate, or fixed AESA), given the good performance of the normal Captor and the good diameter of the EF nose (it is speculated with 1400 T/R modules), we can expect much.is the eurofighter s's captor aesa ready ??
what are its specs ??
Snecma
First test flight of Rafale fighter powered by upgraded M88-4E engine
Courcouronnes, May 4, 2010.
The first test flight of a Rafale fighter powered by the Snecma (Safran group) M88-4E engine (formerly designated the TCO Pack, for total cost of ownership) took place on March 22 at the Istres air base in southern France. Lasting 1 hour and 30 minutes, the flight was a total success, and was used to expand the flight envelope. The complete test campaign for the M88-4E engine comprises some 70 flights in 2010, with different engine configurations. Ten test flights have been carried out to date...
PS: Does anybody have any information about this engine,like thrust,dimensions,etc..
M88 Developements for Domestic and Export markets:
First the main developement was destined to the domestic market (MN/AdA) with the steps taken by SNECMA from M88-2E1 to M88-2E4.
FROM Standard M88-2 to M88-2E4 developed from <> 1995.
New:
----Three-dimensional high-pressure (HP) compressor.
----Turbine blades.
----Blisks (one-piece blades and discs).
----Improved thermal coatings on the HP turbine.
----Advanced cooling channels for the combustion chamber.
Noticeable technological progresses:
TURBINE BLADE LIFE AUGMENTED BY A FACTOR OF THREE.
BLISKS.
TOLERANCE TO HIGHER TEMPERATURES.
SFC LOWERED BY UP TO 4% COMPARED TO M88-2-Evolution1.
---->
FROM Standard M88-2E4 to M88-3.
New:
----LP compressor.
----Variable stator vane stage.
---->
FROM M88-3 to M88 ECO.
----HP corps.
----Combustion chamber.
---->
M88-3 VS M88 ECO.
Diameter:--------- 790mm 31.1-in VS 700mm 27.56-in.
Length:----------- 3.6 m 12-ft VS 3.5 m 12-ft.
Weight:----------- 985 kg 2,172-lb VS 897 kg 1,978-lb.
Thrust:----------- 89.9 kN 20,250-lb VS 75.5 kN 17,000-lb.
According to these figures:
M88-3 diameter is <> 90mm superior, it is 100mm longer and 88 Kg heavier than M88-2; this would add 176 Kg to Rafale away from CG.