I don't know where you could have gotten 0.85 from, try this: https://www.engineeringtoolbox.com/radiation-heat-emissivity-aluminum-d_433.html

Heat spreaders and heat pipes are not at all the same thing, and either will result in a delta-T completely missing from your calculations. And minimising that will blow your mass budget.

Re static electricity - yes there are mitigations, such as the aforementioned aluminium enclosure, but that will result in yet another delta-T missing from your calculations.

Radiation: yes, we can check for single event upsets in software and discard them. That's not the main problem with radiation, though. Here's a TL;DR: https://nepp.nasa.gov/DocUploads/392333B0-7A48-4A04-A3A72B0B1DD73343/Rad_Effects_101_WebEx.pdf

https://www.thermoworks.com/emissivity-table/

Aluminum's emissivity varies significantly depending on the surface treatment, and exactly how you are measuring it.

Anyway, as you can see there's lots of materials with emissivities close to 1. This is not a hard problem.

Commercial satellites do in fact use off the shelf chips all the time. Heck, I used to work at a company founded by satellite engineers. Their previous big project was a space telescope that was entirely built with automotive rated electronics. It lasted for years in orbit with no serious problems. You achieve this with redundancy and error tolerant software. Which is easier these days because automotive electronics standards have also created a big market for error tolerant devices, eg cheap microcontrollers with ECC RAM and SEU tolerance.

$100k silicon on sapphire chips just aren't as commonly used as you think they are. It's actually to the point now where for a lot of satellites the engineers actually _prefer_ using automotive rated parts as in many circumstances they're more reliable than the pricey space rated stuff.

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...and LEO is a more forgiving radiation environment than deep space. Okay, I'll grant you your automotive-grade ASICs.

We haven't solved the thermal engineering, not at all. There are many materials with high emissivity, but you also want high thermal conductivity, high electrical conductivity, high toughness and high strength.

Unobtanium.

There are good reasons why aluminium is standard, and whatever the treatment its emissivity sucks at any temperature that automotive-grade electronics can be expected to survive.

Shall we re-run your calculations, as a second-approximation with a plausible emissivity (0.2) and a delta-T budget for heat-spreaders/heat pipes (10C ?).

You obviously didn't read my link. Your just unable to admit you're wrong.

And we haven't even gotten into higher tech solutions like the large variety of specialty coatings that have been developed to optimize radiation (hint: the ISS's radiators aren't black, because they use special coatings to optimize exactly what wavelengths they emit and absorb).

Finally, as I explained in my post, you can pick whatever temperature you want arbitrarily by simply rotating your satellite at an angle to the sun.

Space mining is clearly possible. Whether or not it is actually economical is a question of in-depth cost engineering that none of us are in a position to evaluate without an enormous amount of detailed cost engineering work.

Your link, I'm sorry to say, does not support the 0.85 emissivity you claimed for aluminium. Where did you get that?

Your link also does not give any hint as to what temperature their source measured emissivity at. Anything can be emissive at plasma temperatures.

So no. Use the engineeringtoolbox numbers, which do list treatments and temperatures.

0.2, for heavily oxidised aluminium.

Z-93, as used on the ISS radiators, is rather nice, though. You should have gone with that from the start.

You certainly can rotate your panels away from perpendicular to reduce insolation, but obviously that will reduce power and hash rate, while doing nothing about radiation damage or cost of now-idled capital.

You are correct that we cannot perform a detailed economic analysis without a design, but I stand by my previous conclusion.

We will not be commercially mining bitcoin in free space this century, and without "new physics" we won't be doing it ever. Not even with zero launch costs.

That link is for infrared thermometer readings. Hence, low temperature.

It's bizarre how you are surprised by this. Anodization greatly increases the surface roughness of aluminum. This information is easy to find from lots of sources:

https://www.gabrian.com/anodized-aluminum-heatsinks-what-you-need-to-know/#:~:text=The%20emissivity%20of%20an%20anodized,(which%20utilize%20a%20fan).

Okay, much better, now that one says 0.85.

Day-um, wild if true. Wonder that oxide thickness, and if they've published a paper. Not very important in-atmosphere or when surrounded by other FIR-emitting things, but in space...