The trick here was that they didn't say simultaneous launch and recovery is a major cause of the "60%", or even necessarily related to it at all. They said:
Which is technically true.
Though, there's also this part:
Also fyi, for anyone unaware, the Nimitz class ships had their JBD interfering with the safety line of the landing zone, meaning they also couldn't conduct simultaneous launch and recovery. This wasn't changed until the Reagan subclass.
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I am more saying that mentioning simultaneous launch and recovery in the first place as if it is a routine standard, is not a great look.
(Considering they say "Both of the catapults are situated close to the middle-front section of the landing area, so either the J-15 or J-35 (China’s two carrier-based fighter jets) would roll over the catapults when they land, temporarily preventing them from being used for launch operations and thus affecting the takeoff efficiency of the fighter jets," I am also unsure if that is or isn't factored into their 60% number)
Given CV-18 is a smaller ship, conventionally powered, with one fewer catapult and one (or two) fewer elevator/s, with a bigger island, it definitely should go without saying that its sortie rate will be lower than a contemporary US CVN, which I think any observer would have baked in as assumptions to begin with.
The rest comes down to design choices/parameters, airwing configuration etc.
Whether it's 60% or a different number, is largely immaterial, but a higher effort article would have had the foresight to account for size, configuration, powerplant, to actually squeeze out benefits or compromises of "changeable" design choices.