I flew S-3 Vikings, a rather large vert stab and rudder. Turns out it was designed to be short enough to fit on a mid deck elevator, which dictated the rather larger than average tail. Then, it was too tall, so they then made it foldable. Classic example of cascading effects.
Also made the plane a little unique in that because the tail was so large, the plane CAN NOT spin! Rather, as it continually gained airspeed, it was a high speed spiral. As such, never needed “anti spin” controls to recover. Of course we had “anti spin” controls and procedures, which of course are a recipe for a spin the other way... As such, the only two ejections ever initiated because of an inability to recover from a “spin” by the prescribed altitude, just happened to be observed by another aircraft in the operating area. Both times the vacated jet recovered by itself! Then crashed....
Just a funny thing. My guess is the large ugly (to some) rudder is indeed a necessity of HEAVY and SLOW and short enough to maneuver in the ground on narrow runways.
Tools
PS. The folding rudder caused a funny situation for me once. After landing on the carrier you got the signal to fold wings as necessary. The right seater, a NFO, did that. For some reason you lost all the artificial feel in the rudder pedals with the rudder folded (shouldn’t ever need to taxi that way anyway, so no biggie) . My NFO (coincidently the squadron commander) inadvertently folded the rudder instead of the wings once... I damn near lost control of the jet, swinging around like mad with ZERO resistance in the rudder pedals and FULL nose wheel steering authority, and I was BIG since the wings weren’t folding... I’m screaming at him, driving like drunk Irishman, handlers are diving for cover, the boss is yelling at me... what a mess!