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If the aircraft is software limited too 6.5G's, then why is that not reported in any of the JPO statements? Also, how would increase the G limit improve energy management? There is no requirement in this dogfight to go up to 9 G's, because the pilot cannot even operate at 6.5. Increasing the G limit would have changed nothing.


As for hardware changes, what can be done to fix poor Energy Management? Remember, that is the heart of the test pilots complaint. He could not access the high AoA without losing unacceptable amounts of energy.


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