pauldun170
Diamond Member
- Sep 26, 2011
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range is always an issue
that doesn't mean it couldn't have been better
the benefits are more thrust and less development expense
also the F135 has a huge bypass ratio (for a fighter engine) which might be efficient for cruise but isn't great at rapidly changing thrust scenarios
no matter how much you squint, the F-35 is NOT the F-16. It is a heavy plane. It's empty weight is more than an F-15C! It would work better with more thrust and bigger wings. It would also provide more growth potential.
What does your twin engined, large winged fighter with an internal load look like and how much will it cost to manufacturer and support over several decades.
F-135 is in LRIP and cost are continuously dropping.
Assuming that your theoretical design were to be be built, GE would revamp the G414 into a new design.
Take a Super Hornet. Add internal bays. Add internal fuel capacity in the 15K-20K lb class. Design it to handle estimate fuel consumption of dual engined design and drag associated with an aircraft that has internal bays and massive fuel storage.
Picture a giant J-31 being sold at F-15K\Rafale\EF2000 prices
