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it will not have any kind of TVC because it has similar exhaust nozzles like YF-23 which wont allow TVC to fitIt's a test maneuver. With 2D thrust vectoring it is more agile than F-16.
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it will not have any kind of TVC because it has similar exhaust nozzles like YF-23 which wont allow TVC to fitIt's a test maneuver. With 2D thrust vectoring it is more agile than F-16.
it will not have any kind of TVC because it has similar exhaust nozzles like YF-23 which wont allow TVC to fit
NO, Not a chance to have had TVC, because below the nozzles were ceramic tiles to shield the nozzles from below (to reduce IR signature) ,F-23 was not have had TVC either, because nozzle design was not permitted to have 2D TVCYF-23 demonstrator did not have TVC but the production F-23 would have had TVC.
NO, Not a chance to have had TVC, because below the nozzles were ceramic tiles to shield the nozzles from below (to reduce IR signature) ,F-23 was not have had TVC either, because nozzle design was not permitted to have 2D TVC
And engine geometry comes with heat shield just like B-2 have (design of rear of YF-23) and it was the finalize design by the company (approved by USAF/Pentagon), if they (USAF/Pentagon) want to change engine geometry they needed to re-designed whole rear part of the YF-23The TVC comes with the engine, not the plane itself.
If not 2D TVC, what wonders is this then.NO, Not a chance to have had TVC, because below the nozzles were ceramic tiles to shield the nozzles from below (to reduce IR signature) ,F-23 was not have had TVC either, because nozzle design was not permitted to have 2D TVC


No this not proof that it has 2D TVC , in fact it supports my claim that J36 doesn't have any kind of TVC , it has similar nozzle geometry of YF-23 which can't allow to have a 2D TVC, and post the pictures of above engine nozzle, that clearly shows J36 will not have 2D TVC of any kind,If not 2D TVC, what wonders is this then.
View attachment 113296
Why have separate pieces for the exhaust vanes?
View attachment 113297
NO, Not a chance to have had TVC, because below the nozzles were ceramic tiles to shield the nozzles from below (to reduce IR signature) ,F-23 was not have had TVC either, because nozzle design was not permitted to have 2D TVC
Not an HIGH agility but showing STANDARD agility, nothing special about it
It seems like a sideway turn which is very challenging especially for a fighter without tail fin.
If the J-36 do indeed include a true, controlled sideway turn (and sharp!), it would be a testament to the remarkable advancements in Chinese aerospace technology, particularly in flight control systems and potentially thrust vectoring for tailless aircraft. It would suggest a level of agility and maneuverability that is at the cutting edge of fighter jet design.
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