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Fluidic thrust vectoring, high bypass turbo fan with EGD.

So, the high temp core might comes from RR but the rest of the tech more from Japan.


Fluidic since Japan specifically flight tested directional actuation of thrust via petals

EGD (ElectroGazDynamics Generator) since I have not seen much moving forward in that domain from  UK  in the last decade.1


Notice that I wish the bypass tubes were turbo ramjets a-la Blackbird but the tube section are more in-line with a high pressure jets diverter.


For the radar, I remember Japan working on a 3D nose mounted radar. Is that sidelined?


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