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dnauticstoday at 4:28 AM1 replyview on HN

Yes, beyond the three things that are the hard parts it's easy.


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pveierlandtoday at 6:46 AM

As problems go, radiation and cooling seem to have relatively low dimensionality compared to the other problems. It seems to be mostly a question of optimizing within the dimensions of dissipation / structure / deployment / service / cost / weight. When all is said and done, the cooling solution will end up being a module that can deal with some power dissipation, cost X amount, weight Y amount, have structural interface Z. This seems like something a relatively low number of engineers can iterate on largely isolated from other concerns. SpaceX does have 5000+ of them.

Comparing this to scaling the production of compute where they try to work outside the bounds of ASML (~40k employees) and TSMC (~80k+ employees), and where there is a huge number of degrees of freedom in many, many layers of the stack that have complicated interactions.

With radiation and cooling, SpaceX also has plenty of experience with both already given that they've had to solve this on existing satellites. Overall, Terafab just seems like a far harder challenge, and where I'd be more wary on timelines.

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