FuturePAF
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A higher thrust will open doors to improvements like CFTs
With current engine or even rd93ma that wouldnt be a feasible option
Dry thrust is around 57about 15% higher then baseline model
While wet is around 94
More important is increase fuel effiency and life
Considering the outreach by the Russians, we should be trying to get ToT for the RD-93MA to build it under license. It will create a baseline engine capability, so that we are able to always field fighters. Even if, eventually, we pick the WS-19 (probably by 2030 at the earliest) to power future JF-17 variants, we should be able to create a foundation in this domain and support a minimal independent capability.