Yes only in my dreams or by the fact that IAFs rejected the Kaveri / Snecma engine in the first place, in fact IAF had doubts if the joint engine will reach 90kN at all and if there actually was a joint development, or simply a replacement of Indian parts with French once. You could also add the fact that ADA itself required up to 95kN for MK2 and let's not forget that this requirement was made nearly a decade ago! In the mean time, LCA got heavier and heavier and the MK2 initially was not planned in the medium class either. So if they Base it now on the weight and performance of the Mirage, 90kN obviously can't be enough for MK2.
Air marshal Mateshwaran, who headed the, "rejection" committee, once opined
Why only 6 stages on kaveri,,,,,
increase it, to 10 or 12, it doesn't matter, all we need is more thrust.
He is oblivious to even the simple fact, that modern jet engines derive higher thrust,
by increasing thermodynamic efficiency, through higher TET,
& operating pressure,
there by reducing stages & engine weight,,
Because what matters I not just absolute thrust, but engine thrust to Weight ratio.
Kaveri is shorter than GE 404,
Such genius being given appointed to head the committee, to evaluate, snecma GTRE jv
has made IAF & GOI a laughing stock around the tech world,,,
Because Pratt & Whitney guys who hv experience In variable cycle engines inspected kaveri & said it is a world class engine,
even the French don't hv kaveri's variable cycle jet engine technology, the same tech which powers F22
That says a lot about the, "technical capabilities" of IAF review committee headed by Air marshal, "Matheswaran".
Goto Bharathrakshak kaveri engine thread & read a few of, Maitya's post about what design changes will unleash the full potential of kaveri, before placing expert here.
Just because your old favorite forums went belly up, don't litter DFI with falsehoods.