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Gentleman, your input and knowledge is requested if I may?
I have a question if I may, in relation to the Fairchild A-10A/B Thunderbolt II
If the A-10’s General Electric TF34-GE-100A turbofans were to be replaced by General Electric F404 non afterburning turbofans, as I’ve heard proposed before, would the existing engine pods accommodate the F404? Or would the engine pods have a different shape – length, diameter etc?
Can someone take a guess (or better calculate) with their knowledge of TF34-GE-100A and F404 fuel consumption/fractions, as to how the range and loiter time of the A-10 would vary with each engine design?
Thanks in advance
Regards
Pioneer
I have a question if I may, in relation to the Fairchild A-10A/B Thunderbolt II
If the A-10’s General Electric TF34-GE-100A turbofans were to be replaced by General Electric F404 non afterburning turbofans, as I’ve heard proposed before, would the existing engine pods accommodate the F404? Or would the engine pods have a different shape – length, diameter etc?
Can someone take a guess (or better calculate) with their knowledge of TF34-GE-100A and F404 fuel consumption/fractions, as to how the range and loiter time of the A-10 would vary with each engine design?
Thanks in advance
Regards
Pioneer