Uttam is overweight by 40kgs for the Mk1a tender, simple fact why it was not considered.
And where did you find in RFQ the required weight of MMR to be under 80Kgs?
Tejas is not a ship or submarine that carries ballast, every gram is accounted for especially when they want stronger engines.
See...............Till date, Tejas is carrying ballasts in different sections including the nose. In other words, the full potential of Tejas is still to be realised and there are enough margins in different sectors.
Actually you have a very good taste dealing with French which is why GoI wants more tie-ups. The bad taste has a Russian flavour.
Case in point is M-MRCA negotiations that died on the table after wasting 5 years. I will elaborate no further as I am not interested in derailing this thread.
Just want to add that our taste while purchasing through competitive bidding is very bitter in general. Eg. MRTT
It is being integrated on a testbed for Mk2.
Old news.
Uttam was originally intended for MK-2 before the proposal for MK-1A came forth. Since the arrival of project MK-1A much has changed.
Uttam for MK-2 was a safe bait given time margins which MK-2's timeline was providing. But when the requirement of an AESA in Mk-1 as MK-1A's MMR came into existence in 2015, the LRDE reportedly speed up the development of Uttam to see if it can match MK-1A's timeline. And today we know they are already integrating it on LSP-2, after extensively testing it on the ground(rooftop actually).
It is interesting to add that earlier EL-2052 was considered an obvious choice, even by HAL because of the restricted timeline. But now, we know, there is an open tender for supplying AESA for MK-1A, which will take its own sweet time to materialise. The time in which Uttam will undergo testing onboard Tejas LSP-2. And if it concludes its development before global tender materialises it will become logical choice.
Going by the history of purchases through competitive bidding I have little doubt as which will eventually win the race.
It still needs better engines for IOC as it is 40kg overweight.
Present day AESAs are scalable and so is Uttam.
Anyone who has seen the PPP video from Aero India 17 cannot miss the fact that final weight of Uttam will depend on the size of its antenna and an appropriate cooling system which in turn will depend on intended power output. Something which will be specified by HAL on recommendations of IAF.