I mean weight also affects drag you know. Can’t really discount it as a factor. Also aren’t these values just as good as stat card values? It’s not like the Su-30 would fall out of the sky the moment it hits max speed
We are talking about what speed it can reach, not structural limit.
Different equipment (HUD, MFD, RWR, IFF etc) can at most result in a couple of hundred kg of weight difference (if even that; And usually they try to minimize the weight difference to make the change easier).
A couple of hundred kgs of internal weight isn’t gonna change the top speed of a 25 ton aircraft very much …
We are not talking about whether it falls or doesn’t fall
We are talking about how much the top speed is … I.e. how fast it can go before it doesn’t accelerate anymore … I.e. Thrust = Drag
Find me one example where someone lists speed on max dry thrust as “maximum flight speed” without explicitly specifying it … It’s just not how it works …
BTW, that shows you how much the plane is over performing …
It reaches speed at max dry thrust that it should (or shouldn’t) reach with max afterburner thrust
su32 has the same mtow , same engines , same service ceiling as SU-34E , can you explain how the SU-34E is much worse than SU-32 ? even the airframe is the same. i feel like its 1100kmph with the given loadout. (2xr77 + 2xr74m + 6xAB-500 + 2 jamming pods)