manqiangrexue
Brigadier
Uh... ok, technically true that nobody is ALWAYS 100% of the times wrong (he said J-20 carries more fuel than J-31 and that was correct), but if someone is wrong 8 times out of 10 on main points, I'd just use "always." Are you saying you agree with his assessment here that in order for J-10 to meet enemy aircraft approaching its defense zone, J-10 must use so many of its hardpoints/so much of its payload on fuel tanks that it can only carry 2-4 missiles? Cus that's the main point here.Nobody is always wrong. And even though b787's style of posting can at times be annoying it in no way means he is always inaccurate.
Plus, do you now the max speed of the J-10B/C? The mach 2.2 value is for the original J-10 with the variable inlet. Specifications for the J-10B/C including max speed in unknown. The original flanker top speed was Mach 2.35 but the Su-35S despite having far more powerful engines is limited to Mach 2.25. The reason speculated here is the modification made to the inlet to reduce RCS.
Yes, I understand that the mach 2.2 number is for J-10A but it's the best we've got for now to go off of. I believe (not sure) that the reason Su-35 suffered a speed loss is because they employed some sort of internal cover in the intake to diminish the exposed compressor fan's susceptibility to radar. I've not heard of this strategy being used on any other jet and I wouldn't for that reason take it as convention to downgrade the speed limit on other upgraded models (for which the limits are unknown) based on just this precedence. And even so, the loss of speed is not great, only mach 2.35 to mach 2.25.
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