"It really seems like anyone with some renders and a white paper written by someone being gassed up by an overly agreeable AI can get VC funding these days."
That gives you a heat rejection capacity of less than 140 kW (mind you, that is total heat rejection, incl. heat from the sun, support systems etc., only a part of that can be used to cool servers) So you settle for laughably low compute to keep radiator size somewhat reasonable, yet still massive and heavy.
The ISS is rated for 84kw but is run max at 70kw, probably for margin of error and whatnot since its for human saftey, which these will not be. They can also probably run hotter, (edit reducing the size).
Via radiation into space. All you need is a radiator, the weight of a battleship (or worse). Yes, the idea is crazy.
Around or less than twice the size of the ISS radiator.
That gives you a heat rejection capacity of less than 140 kW (mind you, that is total heat rejection, incl. heat from the sun, support systems etc., only a part of that can be used to cool servers) So you settle for laughably low compute to keep radiator size somewhat reasonable, yet still massive and heavy.
The ISS is rated for 84kw but is run max at 70kw, probably for margin of error and whatnot since its for human saftey, which these will not be. They can also
probablyrun hotter, (edit reducing the size).The compute is 125kw avg per dish. 150 peak.