The F/A-18E/F Super Hornet has a significantly reduced radar cross section compared to the F/A-18A-D Hornet even though it is a physically larger aircraft. The airframe design of the Super Hornet is based on that of the Hornet, it does have larger LERX and redesigned engine inlets, but other than that is largely similar to the Hornet. I know the box inlets help with RCS but since the airframe design is so similar, I'm wondering how the Super Hornet has such a dramatically lower RCS?
I've read that it's because of how all of the joints and access panels are designed and manufactured on the Super Hornet. Does anyone know if this is true?
I've read that it's because of how all of the joints and access panels are designed and manufactured on the Super Hornet. Does anyone know if this is true?
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