I'm not dismissing the capacity and capability of STOL - but I do get grumpy when the debate tries to twist the justification into x vs yAust,
Perhaps I can help here, on the subject of launch rates and effort.
There are three ways of launching fixed wing aviation from ships currently available:
CATOBAR (Basic cat and trap), STOBAR (STO launch up a ramp, conventional arrested landing), and STOVL (STO launch up a ramp, vertical landing). (The last might develop into STORVL (STO, rolling vertical landing) on larger ships).
Using the more commonly understood term 'launch rates', a CATOBAR ship can launch one aircraft per catapult about every 60/70 seconds or so - with a very highly trained crew. (the catapult launch evolution is complex). The total launch rate is then driven by numbers of catapults. If you have a 95,000 ton CVN, they will usually have three of their four catapults operational. So you should be able to launch around three aircraft per minute. On anything under that (e.g. CDG), you will launch just about two per minute, as there are only two catapults. You will need around 250 people to be able to do this.
STOBAR - the only ships to date that have used this have two launch stations at the bottom of the ramp, with aircraft taking turns to launch. The aircraft are positioned on the deck, then held by retractable 'chocks' while they run up. I can only guess what the rates for feeding aircraft to the launch spots are, but I'd guess about one per minute. So, about two per minute launch rate. Not more than 50/60 people needed, at a very rough guess. You are right on the money over launch weights, by the way - I would expect a STOBAR launch with any weapons to be followed by a fast trip to a tanker (which I don't think are yet able to be launched from the ship).
STOVL - aircraft taxy forward on to the centreline, stop at a given distance, undergo a few checks, then launch up the ramp. This can be a fast and efficient evolution, with aircraft going around every 20 seconds. About 20 people are needed to do it. I know this, because I have done it many times as the Air Engineer Officer clearing the aircraft for launch. So, about three per minute. The new QE class should be able to do it as fast, if not faster. Moreover, STOVL launches can be, were and are adjusted for load, fuel state, wind over deck, etc. This adjustment is carried out by varying the length of the deck run and changing the angles of the vectored thrust systems after launch. It's much easier than the complex calculations and mechanical adjustments needed for a catapult launch.
I can say without hesitation that a STOVL ship can get its fixed wing aircraft launched as quickly, if not faster, than a CATOBAR ship. And by the way, they can recover aircraft more quickly than a CATOBAR ship can.
However, I don't for one minute want to anyone to think I'm saying that a STOVL launch of 10 smaller STOVL aircraft from a (say) 28,000 ton ship is in any way equivalent in overall mass and effect to a 30/40 conventional aircraft launch from a CVN. Plainly, it's not. But I don't think anyone is trying to suggest that STOVL is a replacement for CATOBAR. I'm certainly not.
However, I do think it's clear that CATOBAR is the exclusive preserve of the USN, and likely to stay that way for some time, purely on cost grounds. The US is the only country on earth that can afford ships of this size, the numbers of people to man them, and the cost of the training to deliver a usable capability.
In my view, STOVL allows fixed wing aviation to be delivered from smaller (and cheaper) ships. Individual countries have to decide whether the amount of capability STOVL can deliver from their ships is a) what they want and b) affordable.
Hope this helps
Best Regards
Engines101
I must confess to using russian STOL lessons as well
The USN had some data published re CATOBAR and STOL trying to put nn amount of ord on a given target - against a non refueled mission in a predetermined range ring - and where refueling to target might also be called upon, that was then determined against organic refueling (buddys) and the with land based air as an alternative
the sortie rates for STOBAR were pretty ugly in comparison
The french did have decent tempo for their rafales on deGaulle - so it would be interesting to see data on a CdG sized platform and its air wing against the largest STOBAR equiv (which makes it incredibly theoretical)
some of the assumptions being made in here earlier were completely divorced from the known limitations of various platforms.
thanks for the extra tech detail - greatly appreciated