... am still interested in a reaction to what I asked
Today at 7:40 AM
In my view your question was rather pointless and why I did not address it initially. Since you are insisting, I would be direct.
Whether it is trillion or billion of flops is irrelevant to me. It has no perspective regardless of the answer. It is a rather myopic view of a subject driven by ignorance of a technical subject we can hardly claim to understand. The source of the F-35 EW capabilities is not because its GPU can handle billions or trillions of calculations. It is a sum of its different sensors and its fusion supported by a databus architecture (Mil-Std-1394) processed by dedicated FPGAs, signal processors and directed by the millions of line of codes. All the leading edge stuff cost money and time and why it ended up with a $60 plus billion development budget and nine years behind schedule. Leading edge capabilities don't come cheap. If you want development on the cheap go to Russia. There is general 2 of 3 rule in acquisition. Fast, cheap and good. Pick any of two. If it is fast and cheap it is not good. if it is cheap and good it is not fast. If it is fast and good it is not cheap. In other words, you get what you pay for.
The F-35 basically went for a completely new leading edge bus architecture because sensor fusion requires high data throughput and nil latency in data exchange. Mil-Std-1553 just can't deliver that. High end development require tons of money.
There are a bunch of things to consider ; deterministic behavior, weight, power, volume, latency, topology robustness, software impact, hardware development risk, Failure Modes and Effects Analysis (FMEA) risk assessment, tech refresh path, both non-recurring and re-occurring costs in any design. It is just not a case of calculations per sec.
If you are claiming how capable your avionics and sensors are and my first question would be what is your avionic databus? It is not how many trillions of calculations your GPU can perform. The fact is the SU-35 is still using Mil-Std-1553 and the J-10 is using ARINC 429 speak for itself.