Catapult assisted take-off but arrested recovery ‘CATOBAR’ puts an increased pressure on the aircraft compared to a conventional runway ‘CTOL’. Meaning that a carrier based aircraft needs to be made sturdier than the conventional alternative. The Carrier based F35 weigh about 19% more than the airfield based variant, mostly due to it’s wing area being 47% larger. Presumably the structure of the airplane is sturdier as well adding weight.
This might shift again come next generation Jet aircraft in 3-4 decades. As the US is adopting an electromagnetic catapult system on its newest carrier. At current pace it will take 40-50 years for the US to have an all electromagnetic catapult carrier fleet, assuming the US wishes to maintain the same amount of carriers in the future.
Also, it is not always true that WW2 naval aircraft were lighter than land based ones. Going off the US. The F4F was lighter than the P40, but the F6F was heavier than the P51. Significantly heavier even. But both naval aircraft had a larger wing surface area.
An easier comparison is the British Spitfire vs the Seafire, since the Seafire is a land based fighter adapted for carrier use as opposed to the US fighters where they made aircraft specifically designed for carrier use from scratch. But here is often the same story, the Seafire is generally a bit heavier than the Spitfire in a loaded configuration. Although there are many variants of both,
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