I'm actually a little more curious what that guy with the outdoor desk is supposed to be.
I do not see nothing on this picture related to J-20...
For example, F-15 has a higher thrust-to-weight ratio, yet the aircraft flies slower and climb slower than the F-22.
The pic looks funny so I don't know if it's been PSed. 2003?
Where did you get that ?
Current public data (Wikipedia and such ) claims 40,000+ ft/min and 2.24 Mach for F-22 , >50,000 ft/min and 2.5+ Mach for F-15C . Yes , it is probably a clean configuration for F-15 , but nevertheless ....
Are you gonna believe wiki,,,,,,, or the Eng??????? stupid question, my money's on the Eng, the F-22 is still HIGHLY CLASSIFIED.
Well , I usually don't believe anyone , but Wikipedia article has some references to public sources (you can check them at wiki page , I cannot post links - yet ) . On the other side , I would like to see Engineer's sources for his bold claims
This is from an article called that was in Aviation Week.The Raptor's silhouette stood out against the thick wool of clouds building nearly 18,000 ft. up. The two airplanes lined up their noses on an imaginary starting line and accelerated from 250 kt. at an altitude of 13,000 ft.
Inside the F-15, Jacob's body slammed backward and the two fighters stayed even for about 10 sec. The F-15 hit 450 kt. in full afterburner in level flight after 20 sec. The F-22 hit 500 kt. in maximum afterburner and pulled away, ending the race. Jacob laughed. "That's it," he said. "My F-15 can't accelerate any more."
This is from an article called >link removed> that was in Aviation Week.
Also, while F-15 does have a higher top-speed, when afterburners are off the F-22 can indeed fly faster. This is called supercruise which I'm sure you know about already. So like I said in my earlier post, aerodynamics are very important and thrust-to-weight ratio can't be used as the only metric to gauge a fighter's ability.
Well , I usually don't believe anyone , but Wikipedia article has some references to public sources (you can check them at wiki page , I cannot post links - yet ) . On the other side , I would like to see Engineer's sources for his bold claims