Comment Re:Cooling (Score 2) 64
As a point of reference, the current ISS cooling system can reject 75kW of heat, from a combined area of 84.864m^2. Those radiators are only part of the system, the External Active Thermal Control System, and they are continuously rotated to optimise heat loss from them.
Ref: https://en.wikipedia.org/wiki/... and the cited https://www.nasa.gov/pdf/47348...
So that ballparks 2GW requiring ~2250m^2 of radiators. Remember, it needs mechanisms for rotating, and to be placed so that they're mostly not radiating at each other, plus all of the plumbing and pumps for the transfer of heat to thrm.