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Any integration info (airframe/engine) on the rocket engine augmentation?


The piece I quoted yesterday from Rear Admiral Gillcrist, also mentioned rocket augmentation.


Also, are we thinking that a J58 for the F8U-3 might be for just higher thrust levels at

Mach 2.6, or are we thinking that a J58 for the F8U-3 would really be for Mach 3?


Interesting question.


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