Comment by abalone
2 months ago
I am skeptical as well BUT on the cooling question, which is one of the main concerns we all seem to have, the article is doing a bit of an apples-to-oranges comparison between the ISS and a cluster of small satellites.
It cites the ISS's centralized 16kW cooling system which is for a big space station that needs to collect and shunt heat over a relatively large area. The Suncatcher prototype is puny in comparison: just 4 TPUs and a total power budget of ballpark 2kW.
Suncatcher imagines a large cluster of small satellites separated by optical links, not little datacenter space stations in the sky. They would not be pulling heat from multiple systems tens of meters away like on the ISS, which bodes well for simpler passive cooling systems. And while the combined panel surface area of a large satellite cluster would be substantial, the footprint of any individual satellite, the more important metric, would likely be reasonable.
Personally I am more concerned with the climate impact of launches and the relatively short envisioned mission life of 5 years. If the whole point is better sustainability, you can't just look at the dollar cost of launches that don't internalize the environmental externalities of stuff like polluting the stratosphere.
In theory rocket launches sound bad, with burning fuels all the way up to the top layers of the atmosphere, but it's not clear right away that we're significantly increasing the "burnt up stuff" vs say, the ~100 tons of meteorites that hit every night.
Arguments re: Methane as a non-renewable resource are of course right, except that we technically can synthesize methane from CO2 + electricity (e.g., terraform industries), but the pollution angle is presented as-is, without a systematic analysis, right?
What's the actual atmospheric burden here?
This essentially says "We dont know"
https://news.climate.columbia.edu/2025/03/04/rockets-affect-...
Starlink v2 Mini has about 35 kW of solar power at peak irradiance. 2 kW is quite far from the limit of how much juice we can pack into modern mass produced satellites.
Got any guesses about energy used for propulsion, cooling solutions (energy used for them as well as overall capacity), communications and how those might degrade over time in a real environment rather than just academic theory?
That's not even considering the increase in exposure to radiation outside of the Earth's atmosphere (absorbing materials) and weakened at distance protective EM field.
Some of the proposals are much much bigger than this. Five GW, and 16 square kilometres.
It’s amusing that the article points out how large the radiators will have to be, when the proposals already include building giant radiators. Or that the satellites will have to be vastly larger than the ISS; surprise, surprise, that’s also part of the plan.
There’s a weird thing in discussions about space. Lots of people just don’t like space, it makes them think they’re being blasted with science fiction.
So much criticism of space seems to fall into a few categories:
Space based data centers are probably not going to happen in the next decade, but most criticism (including this article) just reads as head-in-the-sand criticism, not serious analysis. I’m still waiting for more serious cost-benefit analysis assuming realistic Starship mass budgets.
If I worked for SpaceX, I imagine I’d focus more on just getting more Starlink mass in orbit for at least 3-4 years, but after that, we might have spare capacity we might want to spend on orbital power loads like this.
Things like Golden Dome ruin it for everyone..
I mean why not just have a whole bunch of floating buoys doing computation on the ocean? They can probably get energy both from solar and from the tidal wave energy. Cooling certainly won't be an issue.
Communication might be a bit rough.
I think the interest in outer space comes from the lack of an atmosphere to absorb the sunlight/power.