F135の熱問題を既に克服済みって、F136ってF135より遥かに優れたエンジンだな


The F136 produced 28,000 lbf (125 kN) of thrust in military power and 43,000 lbf (191 kN) in full afterburner, same as the F135 but with greater temperature margins due to the higher air mass flow, resulting in longer hot-section parts life and greater potential for future growth. In the STOVL