Please, stop posting such half baked posts. You have no idea what you are posting. Please lurk around a bit more before you start posting, it is painfully obvious that you are in no position to answer even the basic queries related to the program.
You too have no proof either for or against the statement ,"tejas has lower RCS and better radar than grippen ". So what is the fuss?
What is the radome dia of grippen,rafael ,typhoon,and tejas?
What is the average RCS(as measured by russians, not frontal clean config RCS) of rafale, typhoon,grippen and tejas?
If it is so, then why did the MMRCA contenders insisted on their performance specs not to be revealed in public and wanted the IAF to hand them over to each in sealed envelopes?
All their peak performance advertised by these 5 MMRCA contenders are in their own mostly cold climatic conditions.
And other than the f-16 and f-18 all the other contenders had fielded incomplete products or prototypes in case of SAAB.
Has grippen Ng achieved FOC?
If we add the clean take off weight with full fuel and add it to the max advertised external weapon load , the sum sometimes exceed their max take off weight!!!!
You probably know which fighter I was mentioning in the above sentence.
With such jugglery of figures no one knows whether they achieved their peak advertised specs for ITRs , STRs, sea level and high altitude topspeeds in indian conditions.
Till today not a single MMRCA contender has revealed what is the peak performance specs their fighters achieved in indian hot and humid conditions,
it is common knowledge that in indian hot and humid climate conditions ,in which tejas is being tested saps quite a bit of engine thrust for any jet engine,
So it will be interesting to know what the MMRCA contenders achieved in top speeds, STRs and ITRs in hot and humid indian conditions.
If you have any specs achieved by all the five contenders in MMRCA competition please post the link, before asking other guys to learn a bit more.
And all along you and many posters here kept on saying that tejas can not achieve its top sea level speed due to the 3.7 dBSM drag resulting from sudden increase in cross section according to CEMILAC report dating 2009.
But during flutter tests(
in a power less dive from 4 kms , not powered) in very hot engine thrust saping sea level summer trials in Goa tejas crossed the maximum speed achieved by Mig-29 and Su-30 MKI in
Indian skies.
this is not my statement , but IAf