I suspect a lot of reworking of the structure materials and systems for heat issues if you wanted to make full benefit of the different engines across the flight regimes.
Particularly down low.
Would not putting the Olympus 593 instead of the Mk 320's cause a total redesign of the TSR-2 because of the different design between the engines? It was the same thing with the Vulcan and Concorde Olympus engines.
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