I guess I never paid close enough attention before... It appears they are either "all in" for a launch, or "all in" for a recovery - but can't do both at the same time...?
I wonder how much that forward spots limits gross weight.
They are already limited because they use the 'STOBAR' system that uses chocks to hold the aircraft until it launches instead of catapults, I imagine that the short distance limits that even further.
I noticed that. I assume that's opposed to our holdback fittings? How does the STOBAR system limit gross weight?