Good, but we need this engine to start flying/testing by 2030 - is that possible? Then we need it mass produced by 2035 for AMCA Mk-2, and TEDBF...
Question - assuming we develop this 130KN, mass produced by 2035, what will it take for us then to develop variable cycle engines say in the 200+KN, thrust range (this is what is likely to power NGADs, which are already being tested now and will be deployed before 2030)...
Just asking as it is important to know where does cutting edge stands and how far back we are, and whether we ever plan to not only catch up but move ahead - of course this is a long term game, and we need to play it.