Earlier quoted context omitted.
As problems go, radiation and cooling seem to have relatively low dimensionality compared to the other problems. It seems to be mostly a question of optimizing within the dimensions of dissipation / structure / deployment / service / cost / weight. When all is said and done, the cooling solution will end up being a module that can deal with some power dissipation, cost X amount, weight Y amount, have structural inter…
Radiators are raised because it's a known constraint and we know that Stefan Boltzmann implies a lot of radiator mass to be launched even at 100% cooling efficiency and there are also theoretical limits to launch efficiency which Starship is rapidly approaching. Nobody is saying orbital datacentres can't be cooled, they're saying people arguing launching the mass of the required radiators into space is a better, more…
Of course the major exercise becomes about total cost efficiency, but I think a large attraction is that once you've solved space deployment sufficiently, you don't need to keep dealing with local circumstances and power production adaptations to every new site you're dealing with on Earth, as it's more about producing a set of modules you can keep launching without individual adaptation - not about "space being cold".