Again thrust to weight ratio has nothing to do with cruising speed.The F-22 won't be able to meet it's thrust to weight ratio on one engine without going to burner at it's transonic cruise speed... that's my point that you never acknowledge. It would never reach Mach 1 even with the burner lit. Whatever point your making is moot because it has no basis in reality.
The SR-71 weighs twice as much as the F-22 and has the same thrust. So the thrust to weight ratio of the SR-71 is half that of the F-22 yet it can reach Mach 3 let alone Mach 1. The concorde only has a third of the thrust to weight ratio of the F-22 yet it can reach Mach 2, let alone Mach 1.
What information are you basing this on that the F-22 cannot reach Mach 1 with 50% dry thrust?
If the F-22 has a combined dry thrust of around 50,000lb and can reach Mach 1.5~1.6. Then the F-22 with 25,000lb of dry thrust can reach Mach 1.
Every drag formula and graph on aerodynamics says that it will be able to reach mach 1. Can you please explain why the F-22 cannot hit Mach 1 with 25,000lb of dry thrust?
Once it is acknowledged that the F-22 with only 25,000lb of dry thrust could in fact hit Mach 1 then my original post that the F-35 can also hit Mach 1 with 25,000lb of thrust will be correct. Considering the F-35 is slightly smaller and actually has more than 25,000lb of dry thrust further drives home the fact that the F-35 will be able to cruise around Mach 1~1.1. I'll repeat again this is NOT supercuirse.
This argument started because i said the F-35 will most likely have equal or greater speed than the Suhkoi's yet people disagreed. I believe i've put forward enough facts to prove that the F-35 will atleast reach the cruising speeds of the Suhkoi, which is also around Mach 0.9~1.1 depending on the engines and weapons used.
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