India already has second generation scb , and there is article on net that HAL use blisk and 3D printing for their htfe . So a engine of 55/90 kn was already possible with out France help . If you mastered second generation scb , future generation is less difficult to master as main tech of casting remain more or less same , except change in composition of alloy . What is lacking is degining of low pressure stage for maximum utilisation of tet of high pressure stage with needing modern tech such as wide cord blade , computer assisted degine of blade , better blisk , better tensile strength disc of lighter weight . Also with increase of tet subsonic profile of low pressure stage will change to trans sonic profile with increase of pressure ratio . So Kaveri have to redegine in each and every expect , both in high as well as low pressure stage . I think base line Kaveri snecma will be 65/95 kn with third generation scb , thermobaric coating , better all fan blisk , etc etc with a scope of tweaking to 75/110 kn with better metallurgy . What way Kaveri snecma is executing I thing specks should already will be fixed , and engine should be going on ground testing . If all things go in right direction 2018 will be mile stone when engine goes to flying test bed .