Lol, only one of us is known here for blowing hot air and got a nickname for it and it's not me.
You're acting like nobody here knows TWR = Engine Thrust/ Aircraft Weight. You keep hiding behind “just divide two numbers” because your entire understanding of fighter propulsion apparently begins and ends with a middle-school ratio, Congratulations, we’ve now covered high-school algebra. Now lets move onto adult talk, the problem is your entire argument falls apart because static TWR alone does not determine whether an engine-airframe combination is operationally viable, otherwise an unaerodynamic brick with TWR above 1 would fly like a fighter jet. Aerodynamics, lift generation, drag, inlet efficiency, control laws, wing loading, transient thrust response, thermal margins and overall airframe integration matter enormously. That’s why aircraft with similar paper TWRs can have completely different acceleration, climb, sustained turn and takeoff performance in reality. The Sukhoi Su-57 already demonstrated extremely aggressive acceleration and takeoff behavior in hot-and-high Bengaluru conditions while you’re still reducing one of the most complex engineering disciplines on Earth into “bro divide two numbers.” Sorry but aerospace engineering is slightly more advanced than your Reddit spreadsheet.
Big words for nothing. Your argument would have made sense if Izd 30 never existed. Good luck.








