Ultima Thule
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@ Asok didn' t find my answers you kid![Biggthumpup :enjoy: :enjoy:](/styles/default/xenforo/smilies/cute/biggthumpup.gif)
Then Ws-15 has thrust of 210 Kn
And then WS-15 has a TVC nozzles
Differential tail surface is not a new tech first used in yf-23 and pak-fa
Please answer my above questions but you have no answer for me kid you insane kid you have no knowledge of fighter jets and its aerodynamic go kid this place is not for yours go play your toys![Biggthumpup :enjoy: :enjoy:](/styles/default/xenforo/smilies/cute/biggthumpup.gif)
![Lol :lol: :lol:](/styles/default/xenforo/smilies/lol.gif)
![Biggthumpup :enjoy: :enjoy:](/styles/default/xenforo/smilies/cute/biggthumpup.gif)
First you prove me J-20 is using WS-15I already listed my reasons or proofs for my assertions in my numerous previous posts.
"Your j-20 has extremely maneuverable and agile, with Delta canard design. Those European is not maneuverable and agile, with a same layout. What a bogus logic, you have. You sh!t head. You have brain of 8 year old kid. You insane"
I am fine, thank you. I am not insane.
Looks like you don't have any proofs that "rafale, ef-2000, grippen, and j-10 all have great maneuverability and agility at supersonic trans- sonic flight regime". and just want to vent your frustration.
I said it takes a lot more than "Delta canard design" for superior supersonic maneuverability, comparable to that of F-22. That's why I don't believe J-10, Rafael and Typhoon has that.
I believe the current J-20 has superior supersonic maneuverability, comparable to that of F-22, because,
1.) it has the agile, differentially moving, "Delta canard design", PLUS,
2.) two powerful WS-15 engine, that has at least 210kN of thrust each, PLUS,
3.) a huge internal fuel storage of 12 tons, to support long Supersonic Cruise, PLUS,
4.) 3-D differential turning TVC nozzles, PLUS,
5.) all moving, differentially activated, tails, PLUS,
6.) a long slender body for superior supersonic state, PLUS,
7.) adjustable DSI air intake that could be optimized for subsonic, as well as supersonic speed.
If that doesn't do it for J-20. I don't know what will.
Then Ws-15 has thrust of 210 Kn
And then WS-15 has a TVC nozzles
Differential tail surface is not a new tech first used in yf-23 and pak-fa
Please answer my above questions but you have no answer for me kid you insane kid you have no knowledge of fighter jets and its aerodynamic go kid this place is not for yours go play your toys
![Biggthumpup :enjoy: :enjoy:](/styles/default/xenforo/smilies/cute/biggthumpup.gif)
![Lol :lol: :lol:](/styles/default/xenforo/smilies/lol.gif)