When nuclear reactors are too blasé and you want to bend physics to your will…
Why not cool a reactor core with a fluid compressed & heated to such extremes that it's no longer a liquid or a gas but something else entirely.
It's the Supercritical Water Reactor thread!
Most reactors in operation today are light water reactors, and there are good reasons for that: Water is both moderator & coolant, they have safe negative reactivity coefficients and decently high power density.
However they are complex and limited by temperature & efficiency.
But you can cool a reactor core with many things: Water, carbon dioxide, liquid sodium, lead, helium, molten chloride salts… the list goes on.
Why not supercritical water?
And what's so special about supercritical water?
Efficiency.
A normal pressurised water reactor (PWR) must keep a liquid phase throughout, meaning that even at 150 bar the core exit temperature is only 325 Celsius. In a boiling water reactor (BWR) that's 285 Celsius.
This means low thermal efficiency, of about 33%.
Complexity.
PWRs cannot boil and cannot run a turbine in their primary cycle, so a pressurizer and a secondary cycle are needed.
BWRs must protect the turbine from droplets, so superheaters and moisture separators are needed.
We can do better!
Supercritical water.
When water is over 374 Celsius and over 220 bar it becomes a supercritical (SC) fluid, containing properties of both gas and liquid, with no phase change as it heats but retaining high heat transfer.
A 675C core exit flow means 45%-50% thermal efficiency!
An SC cycle also allows direct flow from core to turbine and, unlike in a BWR, the homogenous flow doesn't need moisture separators: Simple!
That's not all: SC cycles need ⅛ the coolant of a water based system, are easy to pump & create fewer chaotic steam bubbles.
It gets even better: Supercritical isn't even new!
It's never been used in a reactor core, but it *is* used in power raising cycles in coal & gas power plants, and the structural & metallurgical demands in these applications are well understood.
This all sounds lovely, but the old cynic's question applies:
“If they're so good, why aren't they everywhere?”
Let's explore that with a dive into the design…
Pressure vessel design.
There are two ways to build a SCWR core: A pressure vessel, similar To a PWR/ BWR, or a calandria pressure tube design, similar to the Canadian CANDU.
With liquid water, pressure vessels are generally better, but SC coolant works well in either.
Heat exchanging.
The simple process diagram shown earlier is idealised: In reality it would look a little something like this, with high & low pressure turbines and heat exchanging. Only the high pressure turbine is fully supercritical.
Why? A couple of reasons…
Firstly, there's advantage to using a rankine cycle where water moves between gas and liquid states: Liquid water is efficient to pump & pressurize, while gas is good at expansion in a turbine.
It does lose something in the transition however…
When water is boiling, energy is needed to turn it from a liquid to a gas: It's 1.5kJ/kg in a BWR and zero when supercritical. It's hard to fully recover.
Why not keep it supercritical throughout the cycle? This works poorly with water, but well with CO2
The other reason for reheat heat exchanging in a SCWR is to minimise the enthalpy change in the core.
Why?
Check out the density & thermal conductivity when it gets close to supercritical and remember this is in a core… Why add more change than is necessary?
Moderation.
In a classic light water reactor local boiling can produce similar effects, but that's mitigated as water is also the moderator, so density drops cause self-correcting reactivity drops too.
In a SCWR, the low density fluid makes it harder to use as moderator…
…But not necessarily.
The European HPLWR design, for example, has a three-pass core water flow, only the last two of which are supercritical. This allows the coolant water to serve as moderator, in a fairly conservative design whose exit temperature is “only” 500 Celsius.
This is unusual, but it's implied by design: A SCWR has an enthalpy rise in the core about ten times a pressurised water reactor, so without multiple passes either the core grows vertically or new high temp cladding materials are needed.
There are other challenges…
One of the design challenges of SCWRs is how to manage hot spots and local heating when transitioning to supercritical inside the core.
Ridged or finned cladding such as found in CO2 cooled reactors could be beneficial by enhancing flow mixing and damping excursions.
Corrosion.
In liquid water, electrochemical oxidisation corrosion dominates. In supercritical steam, local chemical oxidisation dominates. In the transition phase both may play a part. On top of stress corrosion cracking and neutron bombardment in the core, this needs research.
Core behaviour.
Managing a reactor core through multiple phase transitions, particularly in power-up and power-down scenarios, poses challenges with SCWRs when fluid density starts to change rapidly through transition points. Feedback loops must be understood and prevented.
Is it worth the challenge?
It would mean more efficiency, a simpler primary cycle, smaller turbines, smaller containment and process heat export.
Get the balance right and it might mean cheaper nuclear power, but first we need to tame an SC water cooled core!
The SCWR must compete with lead, sodium and other reactors, as well as time-worn, fleet delivered GenIII designs, and of course other clean power sources.
It has bags of potential, but first it must understand its own heart,
-Which might be an affair worth having.
Supercritical water… like many new energy concepts it's a bit unearthly.
But powerful nevertheless!
To learn more about the GenIV reactor concepts, and many other things, scroll through the highlights tab on my profile.
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There are approximately 14.6 million working-age people with STEM degrees in the United States, plus arrivals from outside. There are 29 million in the EU & UK.
But this is a sideshow to the real action in the East…
I used Grok Expert to create a series of estimates for STEM educated populations across the world, excluding social sciences, then used population data to predict changes over time. I analysed USA, China, EU+UK, India, Russia & Japan.
Let's get into it…
USA!
14.6 million.
A low volume of engineers at about 3.7-5.6 million (depending on definition) is powerfully made up for in the sciences, particularly biology & biomedical (2.9 million) and computer science & IT (4.1 million).
It's the greatest story never told: It's the story of how a frugal county in the North of England invented the modern world.
Put on a flat cap and call up the whippet, because this is a thread about my home county, and the inventions that came out of Yorkshire!
Steel!
Benjamin Huntsman invented high homogeneity crucible steel in Sheffield in the 1740s, firing with coke to fully melt the steel and homogenise the carbon content.
This became used… everywhere, and supercharged the ongoing industrial revolution.
Steam trains.
Steam locomotion had been in development for some decades by 1812, but arguably the world's first commercially successful steam locomotive was Matthew Murray's Salamanca. To him, we owe speed.
A liquid rocket boost stage needs to pump fuel and cryogenic oxidiser to the combustion chamber at a rate that beggars belief: The 33 engines on the boost stage of SpaceX's monstrous ‘Superheavy’ booster each chew through about 700 kg of propellant every second. Put all those engines together and the flow rate of liquid fuel & oxygen would be sufficient to empty an Olympic swimming pool in under 2 minutes, if you could find an Olympic swimming pool for cryogenic propellant.
Can you think of any conventional lightweight pump that can do this? Me neither. You need something special…
The turbopump comprises a typically-axial turbine powered by hot, pressurised gas flow that powers centrifugal compressor pumps that pump the colossal quantities of propellant required and pressurize it to, potentially, hundreds of standard atmospheres.
It's a handy, lightweight way to provide pumping power, but it does require that you have a source of hot, high-pressure gas to work with.
Now, where would you find that in a rocket engine?
Indeed. In order to burn fuel, we must pump it. In order to pump it, we may have to burn some of it.
Um…
The Gas Generator Cycle.
A small quantity of the pressurised fuel & oxidiser flows are tapped, brought to a small combustor, vaporised, ignited then expanded through a turbine that powers the fuel and oxygen compressor cycles.
Inevitably the gas generator can't run with a completely nominal fuel:oxy mix, as it would get so hot that it would melt the turbine blades, so typically a gas generator will trade off some efficiency and run fuel rich to power the turbopumps.
-Why not oxy rich? Because fuel has a higher specific heat at constant pressure (Cp) and so you need less mass flow through the gas generator if it's fuel rich than oxy rich, meaning more useful propellant goes to the main combustor & nozzle that moves the rocket.
So the upside of a gas generator cycle is relative simplicity and robustness, which is why it's used on the most reliable rocket motors around, the SpaceX Merlin. The downside is that you trade away efficiency by throwing away some of your propellant, meaning that the tyranny of the Tsiolkowsky rocket equation will kick you where the sun don't shine.
Staged combustion attempts to address this, by taking either a fuel rich or oxy rich preburner, operating at a much higher flow volume than a standard gas generator, and routing the hot gases that leave the turbine straight to the combustion chamber so that they're not lost. This not only increases the average propellant exhaust velocity (since none of it is lost) and therefore efficiency, but also allows a lower average temperature in the preburner and turbine, since there's a higher volume throughput instead.
On the flipside you must deal with hugely increased engineering complexity, an increased potential for feedback control problems between the different parts of the engine, and also a much higher pressure preburner, since it will still need to deliver high working pressures to the combustion chamber after the losses of the turbine and injectors.
The Soviets got there first, and some of their genius manifested in the Russian RD180 oxy-rich staged combustion engine, which was bought by the Americans and used in Atlas rockets for many years. Its unique oxy-rich staged combustion cycle was efficient but not without drawbacks, as high temperature gaseous oxygen is brutal to exposed metal surfaces, demanding an enamel coating on many parts of the engine.
Last month Rolls-Royce won the UK's small modular reactor competition to develop and build SMRs in the UK. It could be a new dawn for nuclear power.
But who else was in the competition, what was special about each design, and which is your favourite?
An SMR thread…
What's an SMR?
A small modular reactor is a way of beating the brutally high capital costs of building nuclear power: By simplifying assembly (modularity) and minimising subsystem size so almost all of it is factory built you harvest industrial learner effects and low costs.
Boiling water vs pressurised water reactors.
All designs in this list are either PWRs or BWRs, the most common reactor styles today. I've a thread on the basics if you need it, but otherwise on with the show!
In April on a mountain in Chile the Vera Rubin observatory gathered first light, and this telescope will be world-changing! -Not because it can see the furthest… but because it can see the fastest!
The Vera Rubin telescope thread! The value of speed, and unique technology…
Who was Vera Rubin?
She first hypothesized the existence of dark matter, by observing that the rotation speed of the edge of the galaxy did not drop off with radius from the centre as much as it should. The search for dark matter, and other things, will drive this telescope…
Does it see a long way?
Yes, but it’s not optimized for that: The battle of the big mirrors is won by the Extremely Large Telescope which, yes, is meant to see a long way. Vera Rubin is not that big, but that doesn’t matter because it has a different and maybe better mission.
Rotating detonation engines: Riding the shockwave!
A technology that could revolutionise aviation, powering engines with endlessly rotating supersonic shockwaves. It could bring us hypersonic flight, super high efficiency and more.
The detonation engine thread…
Almost all jet engines use deflagration based combustion, not detonation, but while fuel efficiency has been improving for decades, we're well into the phase of decreasing returns and need some game-changing technologies.
One is the rotating detonation engine (RDE).
To understand the appeal of RDEs, you need to know that there are two forms of combustion cycle: Constant pressure, where volume expands with temperature, and constant volume, where pressure goes up instead.
Most jet engines use constant pressure. RDEs use constant volume.