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Re:NASA completes full-power tests of small, portable nuclea... by jcims on Thursday May 03, 2018 @05:49PM (#16990286)
Seems like this would be limited in space applications by how much you could radiate away. Wouldn't you need to get rid of ~2x the desired output power? So to get 1kW you'd need to dissipate ~2kW?
Re:NASA completes full-power tests of small, portable nuclea... by inamberclad on Thursday May 03, 2018 @09:54PM (#16991638)
The upper limit of any heat engine (turning heat into useful work) is called the Carnot efficiency and is limited by the temperature differential. It's usually not more than 70%, though for a Stirling engine, a few percent would be considered excellent efficiency.

A Stirling engine easily needs to radiate 20 times as much heat as it produces as power.

Re:NASA completes full-power tests of small, portable nuclea... by taejo on Friday May 04, 2018 @05:22AM (#16993248)
> for a Stirling engine, a few percent would be considered excellent efficiency.

Wikipedia says "Stirling engines have a high efficiency compared to internal combustion engines, being able to reach 50% efficiency," which seems to contradict that. What's the discrepancy?

Re:NASA completes full-power tests of small, portable nuclea... by hatsunearu on Friday May 04, 2018 @05:49AM (#16993333)
Yeah, even thermoelectric piles (Peltier effect devices) can easily get ~~double digit efficiencies. Not sure what that guy is talking about~~.

Thermoelectric piles are basically the worst form of generating electric power with heat (it has 0 moving parts, so it's used in various places), and it's still not that bad.

edit: Never mind, apparently they are worse than what I thought they were, at 5~8%. But they are still the least efficient way to turn heat into electricity, and yet they can achieve what that guy said.

Re:NASA completes full-power tests of small, portable nuclea... by ajross on Thursday May 03, 2018 @07:50PM (#16991034)
Yes. Though cooling sails are relatively feasible. Assume you can cool to ~250K: the back of my envelope and a Stefan-Boltzmann constant cribbed blindly from wikipedia tells me that such a sail would radiate ~200W/m^2, which is very doable for a spacecraft with a 1kW power budget.