We brag about the high use of composites in LCA, which suppose to be light weight, but somehow our fighter ended up with similar empty weight as comparable light weight fighters, that were build with standard materials.
Drag issues were created by design flaws, which had to be corrected later too.
This then lead to the fact, that the initial conclusion to have an engine with around 80kN was not enough to meet the goals for speed, turn rates or G-limits.
So were the goals the problem, or the issues in the development?
It's always easy to blame IAF, but that doesn't help our defence industrial development, if we always look for excuses to shift the accountability from our scientists, who messed things up. And it's not like LCA was the only project that saw similar overweight, drag or size problems!
LCH, IJT, Saras suffered weight and drag issues, even Arjuns size and weight are the main problems.
We can only improve, if we admit to our mistakes and learn from them.
Making performance concessions all the time and leave the forces with less capable material to defend the country, is not a solution.
Another twisted attempt at misinformation.
But key point here is
tejas has 20 percent larger wing area
&
Higher internal fuel capacity
than gripenC.
Tejas which uses highest composite content, still weighs marginally less than GripenC.
So composites is definitely one of the key ingredient in getting tejas upto this level.
Gripen STR & ITR are given for atmospheric conditions as per International standards,
Where temp , humidity are all far lower than indian conditions ,
at which tejas STR, ITR figures are given.
Surely no typhoon , Gripen, rafale can repeat those Brochure spec STRs, ITRs, Gs, AOA s at indian high temp, high humidity conditions.
So larger , light weight, composite wings of tejas is of big help in giving it agility.
Ask gripen C to take off with the same loads & at same runway length as tejas mk1 does in Leh & you will see the difference.
TABULATE THE THE
WING LOADINGS OF FIGHTERS FROM
MIG 21 era
To
F22 & PAKFA era
know why fighter designers are increasing wing loading, & designing larger wing area fighters.
So a higher composite content has given tejas
a larger wing ,
Higher radome dia,(more nose cone volume)
&
Higher fuel capacity, (more fuselage volume)
then ,"comparable light fighters", like gripenC.
Completing this low wing loading , compound delta wing , the RSS fly by wire makes tejas as contemporary as any other fighter.
CEMILAC report mentions drag only in ,"transtion to supersonic flight regime at sea level , which prevented tejas from achieving supersonic speeds at sea level".
But this too is remedied & now tejas is supersonic at all altitudes.
Tejas has the same top speed as that of su 30 mki in sea level.
Does any one call su 30 mki draggy design????
LOL.
That too because of poorer fitness ratio due to far bigger radome dia(teja has a bigger radome dua than rafale).
So there is a reason for this poorer fitness ratio, it is aimed at getting a far bigger radar, making tejas a potent BVR fighter with a deadly combo of high tracking range & low RCS.
As far as STR, ITR, AOA is concerned, they are all done at far lower speeds than trans sonic & supersonic speeds,
So no drag penalties there.