You would need to launch so ridiculously much into orbit. The ISS is rounded up 200 kW of solar power. 0.2 MW. Say you want the equivalent of a gigawatt data center. 1000 MW. Yeah, that’s about 5000 ISS sizes objects. It needs a bunch more cooling, and a data center doesn’t need habital zones, so a pretty barebones ISS. Launch 3 roughly ISS sized objects per day and you’re done in 4.5 years. Somehow I don’t really see that as a realistic plan.
The current solar panel system of the ISS weights about 8 tonnes, the Falcon Heavy can deliver 63 tonnes to LEO. That’s about 715 launches of the Falcon Heavy, assuming space solar panel W/kg hasn’t improved since then, that Starship never becomes commercially viable, and doesn’t include batteries, cooling, or the working components. This still isn’t in the range of feasible for a data center, but could be an option for microgravity industry. The value of a more successful or precise silicon crystal production method, for instance, may make it worthwhile.
You would need to launch so ridiculously much into orbit. The ISS is rounded up 200 kW of solar power. 0.2 MW. Say you want the equivalent of a gigawatt data center. 1000 MW. Yeah, that’s about 5000 ISS sizes objects. It needs a bunch more cooling, and a data center doesn’t need habital zones, so a pretty barebones ISS. Launch 3 roughly ISS sized objects per day and you’re done in 4.5 years. Somehow I don’t really see that as a realistic plan.
The current solar panel system of the ISS weights about 8 tonnes, the Falcon Heavy can deliver 63 tonnes to LEO. That’s about 715 launches of the Falcon Heavy, assuming space solar panel W/kg hasn’t improved since then, that Starship never becomes commercially viable, and doesn’t include batteries, cooling, or the working components. This still isn’t in the range of feasible for a data center, but could be an option for microgravity industry. The value of a more successful or precise silicon crystal production method, for instance, may make it worthwhile.