4 ms·
Not only that, but the nuclear rocketry program for Mars was making breakthroughs like the nuclear lightbulb hybrid reactor & closed loop rocket engine [1] - th
by akiselev 6y ago
Not only that, but the nuclear rocketry program for Mars was making breakthroughs like the nuclear lightbulb hybrid reactor & closed loop rocket engine [1] - that the public wouldn't see until declassified papers hit JPL's archives in the 2000s. This program was cancelled by Nixon, setting us back at least half a century.
[1] https://ntrs.nasa.gov/citations/19730003970 https://ntrs.nasa.gov/citations/19730003970
- pfdietz 6y agoNot really a setback, because there was no place for that technology. Lack of space reactors wasn't and isn't a roadblock. Had that development continued it would have been largely wasted, and the knowledge gained would have decayed away.
- akiselev 6y agoIt easily functions as a self-breeding terrestrial reactor that reaches criticality with 1/500th to 1/1000th the fuel of existing nuclear reactors (~20kg). The design requires active power that shuts down the reactor on failure, making any accident a complete nonevent. It can even be kickstarted without huge amounts of enriched fuel with the addition of a neutron gun (which they used to test the design without nuclear fuel). The core infrastructure required to support such a reactor are also covered by far less red tape (mostly centrifuges). It would have changed the face of power generation at a critical time for climate change if it was allowed to reach fruition. Instead it was locked away in UTC & NASA archives.
- pfdietz 6y agoThe requirements for a space reactor, and for a terrestrial reactor, are radically different. No space reactor will make sense for terrestrial power generation. The temperatures are different, power density is different, safety cases are different. A 20kg reactor likely needs highly enriched fuel (space reactors are typically fast reactors too, so we're talking about something that's almost a bomb there.) An external neutron source does not greatly change the needed enrichment (since any practical subcritical reactor would still need k fairly high, so it is only a bit subcritical.)
- akiselev 6y agoJust read the papers. There are dozens on that archive covering the design, theory, and testing - all of those issues are covered. 20kg is actually a high number optimized for a certain plasma temperature that radiates in UV without losing criticality. All things being equal (enriched uranium hexafluoride), at higher temperatures and pressures the reactor needs far less fuel but it causes too much degradation to the reactor walls to be economical or useful except in cold boots. The terrestrial reactor and the rocket engine versions are different in how they transmit power from the reactor core to do useful work but not radically so - the core irrotational vortex compressing a high temperature plasma in a single crystal beryllium oxide chamber is the same in both designs and has been tested. The difference is in the cooling gas - hydrogen gas seeded with tungsten nanoparticles to absorb the black body radiation of the plasma for the rocket and water going through a steam turbine for terrestrial power generation.