Have you ever wondered about nuclear aircraft propulsion? Boy do I have the thread for you! I spent valuable time reading papers that are not relevant to my thesis, because sometimes I like to procrastinate by doing more work. Enjoy! 🧵1/23
In the US we started looking into nuclear propulsion for aircraft as early as 1948. The USAF wanted nuclear powered nuclear armed bombers to fly deterrent patrols of the USSR. Using nuclear energy they could stay aloft for days, weeks or potentially months! 2/23
Nuclear propulsion also allows for easier supersonic flight since there is no flame to keep lit and no real concerns about fuel consumption. This is very appealing for the sorts of bombers we were considering before the ICBM was developed. 3/23
There were 3 large programs of note: 2 for bombers and 1 for a cruise missile. There were also various smaller investigations and white papers looking at all manner of odd ball concepts. I have even seen mention of flying supercritical PWRs! 4/23
Of the bomber propulsion programs, one looked into direct cycle propulsion and one into indirect cycle. Direct cycle is when the air flows into the reactor and directly over fuel elements. This is highly efficient, but can leak fission fragments and activate the air briefly. 5/23
Indirect cycle is when the reactor heat is extracted with a working fluid and then it heats the air via heat exchanges or just runs a turbine that spins a propeller. This is a heavier and more complex option, but is more palatable to the public. 6/23
The direct cycle program was in Idaho and cumulated in the Heat Transfer Reactor Experiment 3 (HTRE3). This nuclear jet engine can still be seen today at the EBR1 museum in Idaho! The program ran until 1961 when it was cancelled. 7/23
The reactor used UO2 fuel elements and reached temperatures as high as 1121 C for hours, but typically ran <870 C to not melt the jet turbines. I have been told that they did damage the turbines at least once though! The reactor also suffered a meltdown! 8/23
It is notable for starting the turbines under nuclear heat (first ever) and having a radiation shield that was rated for flight. The hours of run time also provided confidence that the next step reactor, the XMA-1, would work. 9/23
The XMA-1 was specced to provide >40 hrs flight time at Mach 0.9 and then sprint to the target at Mach 2.5! Both ceramic and metal fuels were considered, with metal being favored. It would use chemical power to get up to spring speed and for assistance during take-off. 10/23
This program was going to cumulate in the XNJ140E engine for a planned Convair nuclear bomber. This dual propulsion (chemical+nuclear) project was on schedule and had parts ordered when the program was canceled. 11/23
Additional studies were being on done BeO homogenous mix (see below), folded flow reactors (like later NTRs looked at) and even fast reactors! Turbo-props were also considered and combined with fast reactors would provide a lot of lifetime in the air... 12/23
The other nuclear bomber engine project was the famous Aircraft Reactor Experiment (ARE) and PWAR-1 project at Oakridge. This is the famous serious of molten salt reactors that have helped ignite a current day craze over the technology. 12/23
These were air cooled and ran up to 760 C, but future plans would include versions that operated at 1000+C. The fuel is a molten NaF-ZrF4-UF4 salt and moderated and reflected by beryllium. 13/23
For aircraft engines, the heat would be extracted via enriched liquid lithium and then taken to a heat exchanger. There was a future design for a 575 MW, ~8 kW/kg (with shield and engine and reactor), Mach 3 capable version! 14/23
A water cooled and moderated reactor was also flown on a modified B-36. It didn't power the aircraft, but was there to test shielding materials and nuclear aircraft handling techniques. A lot of problems were found and being addressed when these programs were canceled. 14/23
The final major program was Project Pluto, the infamous nuclear cruise missile from LLNL! This terrifying machine was a Mach 3, direct cycle, low flying missile loaded with 10-20 nuclear weapons and meant to loiter for weeks before being given the order to go! 15/23
The scary part is this all would have worked! The engine testing was effectively done, the guidance system had been proven and the airframe was being built. The program was cancelled in 1964 for both a lack of real need (ICBMs are better) and for being too provocative! 16/23
A series of engine testing in the "Tory" program out in Nevada showed the ability to build, start, and operate nuclear ramjets like was needed for the SLAM (the missile name) weapon. This cumulated in the Tory-IIC engine shown here. 17/23
This direct cycle engine used a really innovate beryllium oxide/uranium dioxide homogenous mix design. The fuel/moderator elements were extruded into very thin tubes and then arranged into the final configuration. A lot of work went into lowering the U requirement for cost. 18/23
The final results were stunning though, with easy operation for 5 minutes at 461 MW and a fuel temp of ~1300 C. No issues were ever reported with the reactor as far as I can tell, and it was considered to be an easy to run machine. The fuel was undamaged! 19/23
One big downside though, was the fission fragment leakage. It is estimated that 0.2% of the fission fragments escape during operation, which is a lot of nasty stuff coming out of the tail pipe! I can't find good values on the isotopes or I would give you an activity number. 20/23
Sadly the xenon does seem to stay in the fuel though... One interesting bit was that a substantial amount of fission fragment loss is estimated to come from uranium near the edge of the homogenous fuel since the fragments can directly leap into the air at that point! 21/23
Project Pluto was thankfully canceled in 1964, but the amazing tests done showed the incredibly capability of nuclear powered flight. There have been talks of revitalizing this idea to explore Jupiter! 22/23 arxiv.org/ftp/arxiv/pape…
Nuclear aircraft propulsion is a very interesting, if niche use, concept that I honestly think could do with a fresh look due to materials, reactor and computational advances. Hopefully next time around we focus on peaceful rather than deadly uses though! 23/23
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So in when talking about nuclear power in the long term, seawater extraction often comes up. A slightly less often discussed aspect is the Energy Return On Energy Invested (EROI) of this process. This tell us if the whole thing is even worth thinking about. 1/6
There are a wide variety of claims, but this DOE report seems like the best researched and most balanced. It's a bit behind on the tech, but still the numbers are painful. We lose ~10X for LWRs! 2/6 www-pub.iaea.org/iaeameetings/c…
It's interesting to consider how other fuel cycles handle this though. We can see that different reactor technologies and even going for limited recycling, like France does, doesn't really help! The only two options seem to be the full breed/burn or... the humble CANDU! 3/6
The UK making a major blunder here. Not only do they not have anywhere to bury this stuff, but it's a MASSIVE waste of already extracted plutonium! The reprocessing was already done! For some perspective this is ~3100 TWh of energy already usable. world-nuclear-news.org/articles/uk-op…
That assumes just burning the Pu though. If you instead make MOx and use it in an LWR like France does, the UK could get ~842 TWh of electricity! That is 2.66 years of total UK power, about 20 years of their nuclear fleet, or ~60 years of their French imports.
So at worst, give it to France! The UK could also use this fuel for some of the advanced reactors that everyone is interested in. Pu/U mix could substitute for HALEU and be a big help for folks interested in reactors that need that kind of fuel.
So nuclear uprates are in vogue again due to increased demand and gov incentives. An interesting historic thing to note is that BWRs historically have received HUGE uprates with the US fleet running at ~121.5% of installed capacity! 1/6 gevernova.com/nuclear/servic…
I was looking around for what else could be done and found (again) this cool document about the Resource renewable BWR (RBWR) concept from Hitachi. The idea is that we could substantially alter the cores of current BWRs and make them net waste burners! 2/ hitachihyoron.com/rev/pdf/2014/r…
The concept relies on loading two zones of the fuel with transuranic elements (TRUs) and then putting the fuel rods closer together. The neutron spectra is hardened in these regions, thus allowing for burning of the these troublesome TRUs. 2/6
Ok last time I posted a thread about making antimatter, now let's talk about using it in a rocket! Antimatter rocket concepts cover the full gamut in performance from launchers off Earth to interstellar speed machines and everything in between! 1/22
We should first talk about why antimatter? The interest is in the extreme energy density, which then could allow for rockets with very, very high specific impulse. This is like the gas mileage for a rocket and means that we don't need much antimatter to go very fast! 2/22
Antimatter should also allow for reasonably high thrust to weight ratios (TWR), which means the rocket can accelerate up to speed on a reasonable time scale. Once again it comes back to that awesome energy density of ~9E10 MJ/kg, about 1000X fission and 300X fusion! 3/22
So one fun thing sci-fi fans like to talk about a lot is antimatter (specifically antiprotons) production for starships. The fun part is that we already make antimatter right now! But to get enough antimatter for any uses, we need to do a LOT better. 1/17
The standing record for antiproton production is from @Fermilab during the Tevatrons final years. They hit ~2 nanograms/yr using a spinning iconel target getting bombarded with a 120 GeV proton beam! The target did not live long.... 2/17
@CERN uses a similar approach now, but they are not as incentivized for high production rates since their collider doesn't use antiprotons like the Tevatron did. However, they have really been pushing the science of antimatter storage forward! 3/17
Since I have seen this article make the rounds a couple times now, I wanted to address how silly the arguments against this HEU fueled test reactor are. Here is a little thread about HEU fueled reactors and why these complaints are BS!🧵 1/11 reuters.com/world/us/us-ur…
So first of all, what is HEU? Highly Enriched Uranium (HEU) is any uranium with more than 20% U-235, which is the naturally occurring fissile isotope. Natural uranium is 0.7% and typical reactor fuel is 3-5%, but some very small reactors use higher enrichment. 2/11
Above 20% enrichment it is legally classified as HEU. We can quibble about the exact number, but the reasoning is that at this point it is much easier to further enrich the fuel to get to "bomb grade", which is ~90%. So everything from 20% to 99.9% U-235 is treated equally. 3/11