(I mean I still think it's mind blowing, because I think landing a rocket is also mind blowing)
(I mean I still think it's mind blowing, because I think landing a rocket is also mind blowing)
but things would have to get pretty extreme in the "routine" dimension for that to be very useful. If there are 20 first stages and 5 land/launch towers, for a first stage that only spends an hour in flight in between inspections.... well are you going to keep them parked on a scarce launch tower for maintenance? The towers with fill/launch infrastructure (such as reinforced concrete, fuel tanks, cold filling system, deluge water system) become the bottleneck. It's more likely then that the 1st stage lands, is safed, then is taken a couple hundred yards away for inspection and maintenance while the next in line is moved to be stacked for the next launch. The inspection / maintenance would have to be truly minimal (think airliner) to keep it right there on its own relaunch tower.
"No landing gear" is more key, compared to Falcon 9 - because of the effort toward minimal launch cost.
That's what they are aiming for, eventually.
The big advantage of catching it with the tower is that it'll (eventually) allow them to put another Starship on top, refuel and launch again within hours, as opposed to the weeks it currently takes for Falcon 9.
Super heavy can hover and even go down by throttling down more. This gives them more control for the landing and don’t have to time it exactly perfectly
Plus it's really big https://images-bonnier.imgix.net/files/ill/production/Starsh...
https://upload.wikimedia.org/wikipedia/commons/7/7b/SuperHea...
Landing via tower catch versus on a pad is advantageous because the weight of adding retractable landing legs to such a large rocket would be significant.
Which means that the weight savings are nontrivial with the "catch the rocket!" landing method.
This video goes into details pretty well: https://m.youtube.com/watch?v=OYvWYp0--bQ&t=832s