Nice. I think my concern was about the realism of getting a uniformly high radiator temperature.

I didn't see input temperature to the radiator, but on second perusal it must be somewhere between 3—17°C, which is colder than I would have guessed.

Helps your point though

This thing says the ISS can reject 70 kW with ~475 m² of radiator, for ~150 w/m², so real world losses look huge (?).

They're doing -40°C at the radiator outlet, which i guess is most of the difference.

Can a DC do better just with the higher (?) source temp?

www.nasa.gov/wp-content/u...

Brave of you to post this here; exposing your soft underbelly.

Auger snails are long thin things that are a foot

The task was limited to 20 minutes, but I don't remember if they actually tracked finishing times. I doubt many would be early though, with so little time.

These obelisk prisons?
x.com/voooooogel/s...

It's just the left side of this per-county chart, but with one RED and therefore SCARY bucket
www.npr.org/2023/06/26/1...