Supersonic Electric Flight

https://caseyhandmer.wordpress.com/2020/11/18/supersonic-electric-flight/

by paulsutter • 6 years ago

125 82 6 years ago

caseyhandmer.wordpress.com

DJBunnies• 6 years ago

...and having batteries with 500 Wh/kg could...

This seems to be the big if, but I don't speak battery. How close are we to such things?

Shivetya• 6 years ago

Two stories I found, that both provide insight

https://cleantechnica.com/2020/06/10/usas-battery500-initiat...

https://www.nasa.gov/sites/default/files/atoms/files/650_whk...

ejolto• 6 years ago

There is a company called Sion Power that claims to have 500 Wh/kg batteries [0]. "With supply dates beginning in mid-2021 for UAV markets. Broader distribution for the Licerion-HE is scheduled for early 2022."

[0] https://sionpower.com/2020/sion-power-demonstrates-key-elect...

Tade0• 6 years ago

We're there:

https://www.amprius.com/technology/

Just not at scale and naturally such batteries are expensive.

simonebrunozzi• 6 years ago

Commercially and at a reasonable cost? Probably at least 8-10 years from now.

semi-extrinsic• 6 years ago

I think Musk recently said they are going to have 400 Wh/kg in 3-4 years. So maybe 2030.

elihu• 6 years ago

I believe lithium iron phosphate tends to be around 120-150 Wh/kg, pretty decent regular lithium ion tends to be around 150, fairly recent Tesla battery packs are a bit over 200.

(These are types of batteries that have been around for years that you can easily buy as a normal person for a reasonable cost. There's probably a lot of fancy/new battery technology that is somewhat better but either not mass-produced yet or otherwise prohibitively expensive, or trades off some other desirable quality like safety or durability to get more capacity.)

jacobush• 6 years ago

Sounds like SpaceX light. San Francisco to LA in 5 minutes. Neat.

NovemberWhiskey• 6 years ago

Any time someone says they have a design for a prototype that includes aerodynamic aspects, and at the end they say "now scale up by 10" ... there is reason for a strong degree of skepticism.

jvanderbot• 6 years ago

Skepticism which, admittedly, author pre-loaded for us in the first few paragraphs.

scottlocklin2• 6 years ago

The underlying reason that I believe electric aircraft can break the sound barrier is that electric motors can deliver far higher power-to-weight ratios than piston engines, jets, or turbines.

That's a completely worthless figure of merit (I assume he means thrust to weight; because electric helicopters have abysmal power to weight ratio -shit like this matters) and no reason to believe in this nonsense. By the same reasoning, one could build a piston engined supersonic aircraft because there are piston engined helicopters. Another thing that has a high thrust to weight ratio; those water rockets I used to play with as a kid.[0] Pretty sure you can't go supersonic with those either unless you fire them out of a howitzer.

Electric airplanes are a terrible idea without battery technology comparable to hydrocarbon power to weight ratios. Even then, they're a terrible idea unless the motivating technology is lighter than a jet engine and tanks for reasons that should be obvious to anyone with high school physics educations.

[0] https://en.wikipedia.org/wiki/Water_rocket

jeffreyrogers2• 6 years ago

This guy has a physics PhD from CalTech, so his sloppy reasoning is doubly shocking.

scottlocklin2• 6 years ago

So much for my CalTech fanboyism: https://news.ycombinator.com/item?id=25118150

Cipolla was right

Law 1: Always and inevitably everyone underestimates the number of stupid individuals in circulation.

FlyMoreRockets4• 6 years ago

By the same reasoning, one could build a piston engined supersonic aircraft...

Now that's a thought provoking engineering problem! Assume a supersonic propeller is required. Using the Thunderscreech as a baseline, which admittedly didn't quit go supersonic, but it gets us close. Its powerplant produced nearly 6,000 horsepower. That is certainly doable with a piston engine, top fuel dragster engines produce roughly 10,000 horsepower. For about ten seconds.

If this plane burned nitromethane, it wouldn't even need much atmospheric oxygen, nitromethane required roughly one tenth the amount of oxygen per mass of jet fuel. Of course, this means it has to carry a lot more fuel

https://en.wikipedia.org/wiki/Republic_XF-84H_Thunderscreech...

https://en.wikipedia.org/wiki/Top_Fuel#Performance

jasonwatkinspdx• 6 years ago

Burt Rutan was interested in going after it with the Pond Racer, but they didn't get past their test program before one of the engines threw a rod and ended the project. Apparently the math said it'd have been capable of just barely going supersonic when level.

NikolaeVarius6• 6 years ago

The underlying reason that I believe electric aircraft can break the sound barrier is that electric motors can deliver far higher power-to-weight ratios than piston engines, jets, or turbines. The F-4 Phantom is a textbook example of high thrust, being able to (just) achieve a vertical climb. In contrast, for $100 I can buy a racing drone that can accelerate vertically at 10 gs. There are other factors at play but a power-to-weight ratio of 10 screams possibility.

You can't just ... assume that

Gravityloss3• 6 years ago

Jet engines have a thrust to weight ratio of about 10. The power is not so interesting as a lot of the thrust comes from heating the air. Ie the compressor might work at 40 MW and turbine also then of course extracts 40 MW from the airflow.

I'm not sure why one couldn't build an electric supersonic aircraft. It would have very short range. The design presented, could be made more aerodynamic by fairing the motors. Leave a hole in the tip for cooling air. Add a compressor for low speed cooling if needed. Alternatively have liquid cooling.

You could also have a design where the airflow is slowed down in a duct, compressed by a fan and then expanded. The duct would be heavy though. But it might obviate some problems with the free stream propeller.

NikolaeVarius6• 6 years ago

Where are you getting this 10 number from.

Wikipedia shows Eurofighter Typhoon as the highest T/W for a Jet airplane at 1.15 and The Concorde at 5.4

https://en.wikipedia.org/wiki/Thrust-to-weight_ratio

You WANT wings for supersonic flight (For a normal non missile aircraft). Sure it sucks that its hard to optimize for supersonic flight and subsonic, but you go Supersonic at extremely high altitudes to reduce drag on the plane. This requires a shit ton of power to go forward, without even counting the effort to stay in the air vertically.

jjk1665• 6 years ago

Yeah, big difference between a plane that has to carry a person, weapons, and enough fuel to be useful and a toy which is basically 4 motors, a tiny battery and a few grams of plastic. You take just the F-4's engine and 2 minutes worth of fuel and that thing will accelerate very quickly.

WalterBright2• 6 years ago

You take just the F-4's engine and 2 minutes worth of fuel and that thing will accelerate very quickly.

The design concept of the F-104 Starfighter!

nradov• 6 years ago

The F-4 Phantom can't sustain a vertical climb.

chrisweekly• 6 years ago

An F-15 sure can though.

baq2• 6 years ago

For reference, the Merlin rocket engine in the Falcon 9 has a TWR of 185.

Gibbon1• 6 years ago

I have no numbers for the Rutherford engine on the Electron rocket. Amusing idea would be take a page from that and design a ram jet with an electric turbine to get it going.

mnw21cam• 6 years ago

As has been pointed out in another post, that doesn't follow.

My body has a thrust to weight ratio of 1, sitting in this chair. A helicopter has a thrust to weight ratio above 1. But neither is capable of supersonic flight. The key is the reaction mass velocity - you can give something a high thrust to weight ratio using very little power by using a large reaction mass and pushing it slowly. For instance, my body is using the whole earth as its reaction mass, and is using zero energy pushing it downwards at zero speed. A jet is much more impressive because it gets that high thrust to weight ratio while using a small reaction mass ejected at a high speed. That is what is required to push an aircraft up to supersonic speeds. A racing drone is closer to a helicopter than a jet aircraft.

However, if the numbers do work out, then I am wondering if it might be possible to fly supersonic much higher than jets, because there is no reduction in engine power. I don't know how high you have to go before your sonic boom no longer reaches the surface, but might there be a possibility of boom-less supersonic flight?

NikolaeVarius6• 6 years ago

My body has a thrust to weight ratio of 1, sitting in this chair

No it doesn't. Its 0

For instance, my body is using the whole earth as its reaction mass, and is using zero energy pushing it downwards at zero speed

That is not how gravity works. There is nothing happening.

A jet is much more impressive because it gets that high thrust to weight ratio while using a small reaction mass ejected at a high speed. That is what is required to push an aircraft up to supersonic speeds

I wouldn't call it a small reaction mass. A shit ton air is needed to feed the compressor. A jet sacrifices efficiency to get as much mass thrown out the back as fast as possible.

if it might be possible to fly supersonic much higher than jets, because there is no reduction in engine power.

Why would there be no loss in engine power. If you are using standard propellers, you are limited by air density. If you are using some electric engine to turn a turbine, you have the exact same issue. What magical engine is this electricity powering?

dTal• 6 years ago

Yes, that's very silly. It's entirely a question of scale, which is handwaved. You can also buy a gloplug fossil-fueled model airplane which can also accelerate vertically at ridiculous speeds.

mrfusion4• 6 years ago

Interesting point that VTOL actually lets you design your wings only for supersonic flight and avoiding the larger wings (and drag) you’d need for traditional landing and take off.

I hadn’t considered that before.

marvin• 6 years ago

You might not even need wings. You could just shape the fuselage like a wing. Not sure if that would be the ideal for all applications, though. Maybe the smaller cross-section of small wings and a more narrow fuselage would be better in some situations.

jeffreyrogers2• 6 years ago

This is like the lifting body aircraft NASA worked on in the 60s[0]. Their downside was high landing speeds which made them dangerous and hard to fly safely, but with VTOL that problem is mostly eliminated.

Edit: That said, I just read the article and his proposal seems completely infeasible to me barring some sort of massive technological breakthrough. I don't think supersonic electric flight is impossible, but I don't think it would look like what he described and I don't think it has any commercial relevance given the current state of technology and its likely future developments.

[0] https://www.nasa.gov/centers/armstrong/news/FactSheets/FS-01...

skykooler• 6 years ago

A big reason that jet turbines are useful for supersonic aircraft is that their exhaust speed is (pretty much) constant regardless of airspeed; this allows a jet to continue accelerating until the drag force exceeds its thrust. An electric fan could perform similarly if it could provide enough static pressure to achieve supersonic flow through a de Laval nozzle. If that could be done (whether it can is something I'd love to see data on!), the best electric power source would probably have what looks like a regular jet engine intake on the front, a subsonic fan, and a de Laval nozzle in the back like a rocket engine.

bob1029• 6 years ago

Couldn't you just use an electrically-driven turbo compressor to produce a source of hot, high-pressure gasses? Not saying the efficiency or mechanics would play out at scale, but hypothetically you should be able to generate any arbitrary source flow required to feed through this type of nozzle.

larrydag• 6 years ago

I think this sounds like a ramjet or something similar

TylerE• 6 years ago

In theory? Maybe, but the motor would probably weight more than the whole plane does now. A typical jet engine is producing the equivalent of tens of thousands of horsepower.

WalterBright2• 6 years ago

The only reason that jet turbines work for supersonic flight is the inlets to the turbines slow the air to subsonic.

jjk1665• 6 years ago

There's a big difference between a propeller with supersonic tip speeds and a supersonic propeller. A supersonic propeller is not strictly impossible, but even after decades of active research remains elusive. You can't simply handwave that you'll use a 3 meter propeller spinning at mach 3 just because it's technically below the limit where it would tear itself apart from centrifugal forces. It doesn't matter what battery energy density you can achieve if the propellers you're using to drive them don't work.

FlyMoreRockets4• 6 years ago

You should check out this: https://en.wikipedia.org/wiki/Republic_XF-84H_Thunderscreech

Yes, an aircraft employing a supersonic propeller first flew in the 1950's. It wasn't terribly efficient, but it was terribly loud .

0_____0• 6 years ago

Coupled with the already considerable noise from the subsonic aspect of the propeller and the T40's dual turbine sections, the aircraft was notorious for inducing severe nausea and headaches among ground crews.[11] In one report, a Republic engineer suffered a seizure after close range exposure to the shock waves emanating from a powered-up XF-84H.[18]

Holy hell

jjk1665• 6 years ago

That's not a supersonic propeller, that's a propeller with supersonic tip speeds. A supersonic propeller is a propeller that can work in a supersonic airstream. The XF-84H had a top theoretical speed of Mach 0.9, though in testing it was evaluated to be more like Mach 0.83, and even that's disputed, with another estimate being Mach 0.7. It never achieved these speeds.

The only plane to fly with a propeller at supersonic speeds was the XF-88B, though that was actually a jet aircraft that just had a propeller on the front for testing purposes - the vast majority of the thrust was still coming from the jet engines.

mrfusion4• 6 years ago

Would a ducted fan work better?

How about heating the air and pushing it out?

redis_mlc• 6 years ago

Would a ducted fan work better?

This comment is ironic because it initially sounds naive, but is probably the most insightful comment.

You could make a supersonic propeller-driven airplane by mounting the propeller(s) in a shroud, using a powerful engine (possibly geared), and slowing down the airstream to subsonic speed in the shroud (the same way a jet engine is designed.)

The result would be a propeller system that outwardly looks like a jet engine, but internally still has propeller(s) on a shaft(s).

The advantage would be better efficiency at low altitudes if a piston engine was used, since piston engines burn about half as much fuel as jet engines.

Nobody will build this unless high-altitude flight is banned, and thus need the efficiency of piston engines.

Rotax uses essentially a geared lawnmower engine in aviation piston applications that is half the weight of a Lycoming or Continental (because of the gearing.) So hey ... there is room for innovation.

You're not going to get a supersonic helicopter (that looks like a conventional helicopter) without retracting the blades for several reasons, starting with the advancing blade being higher speed than the retreating blade, which makes transsonic and supersonic flight with horizontal blades impractical and risky.

Current fast helicopters have stubby wings, so behave like an airplane, which is kind of cheating. To create a supersonic helicopter would mean either ducted fans instead of blades, or an entirely new technology.

Source: I study aerodynamics.

dghughes• 6 years ago

Heating it would require an enormous amount of power.

kikokikokiko• 6 years ago

Why he hell was the comment that responded to you downvoted? The guy has a background in the area and gave a thoughtful response. I seriously don't know what tha HackerNews mods think sometimes.

jjk1665• 6 years ago

Ducted fans still run into the same issues if the airflow reaching the blades is supersonic. However with a ducted fan you can have the inlet slow the air down to subsonic speeds. In this way ducted fans are used in nearly all supersonic aircraft today. It should be noted though that these turbofans for supersonic use are way smaller than those in use for subsonic aircraft. A 3 meter diameter fan is close to the current limit for such subsonic flight fans, scaling up a supersonic fan that large is still non-trivial.

As for heating up the air and pushing it out, that concept is known as an airbreathing arcjet, which is really just a ramjet. While preventing the electrode from eroding is something of a technical challenge, it's comparatively mild. The main issue here is just power: batteries tend to discharge slowly so to get enough instantaneous power you need a very large number of batteries discharging in parallel, which are very heavy. However if you're just looking to set a speed record and not actually fly any useful distance, this may not be too much of an issue. Personally an arcjet would be my strategy of choice.

ajuc2• 6 years ago

Supersonic electric flight could be a propeled glider that goes stright up, hides the propellers and engines bhind some aerodynamic covers and glides at supersonic speed, then repeats the procedure as many times as needed.

Another idea is to make a turbo-jet engine heated by electricity instead of fuel.

FlyMoreRockets4• 6 years ago

Another idea is to make a turbo-jet engine heated by electricity instead of fuel.

I was going to decry the inefficiency, then remembered that a resistor is only device with 100% efficiency.

ajuc2• 6 years ago

You were right though - much better to use a heat pump ;)

blunte• 6 years ago

I guess it could depend on your definition of "glide", but I doubt that anything gliding at supersonic speed would have a very good glide ratio. Thus, it wouldn't really cover much ground even thought it might travel quite a bit vertically.

If we consider the reason one wants to travel at supersonic speeds, we might arrive at something involving the value of a human's time. Given that, slow but ultra efficient, luxurious (and internet-connected - "workable") travel might be something. Then gliding, floating, etc. with ample space and creature comforts could be the focus.

Ekaros• 6 years ago

I actually wonder if it is even possible to reach sufficient height with electric power... Ofc, it is possible with lift like balloon.

And if it were, wouldn't it be just more efficient to glide at lower speeds?

avmich• 6 years ago

When I read "supersonic electric flight", I assumed something propeller-less, like this - https://news.mit.edu/2018/first-ionic-wind-plane-no-moving-p... .

FiatLuxDave• 6 years ago

I'm surprised that no one is discussing electrohydrodynamic engines for this application, for example as used by https://en.wikipedia.org/wiki/MIT_EAD_Airframe_Version_2. These don't have the same limitations as rotors do with vectoring relative to high speed gas flow. Most of the ones which have been built are small, but that is not an intrinsic limitation; mainly its the battery weight that is the limiting factor.

Of course, the whole idea of electric field is depending on the battery breakthrough, but assuming you have that and want to go supersonic, I'd figure you would go EHD.

pluto93• 6 years ago

For reasons I can't entirely recall, there are pretty serious limitations on the thrust these can generate. I believe it has something to do with the air becoming "saturated" with ions. The limit on the density of charged particles limits how much mass you have to push on. The aircraft in your link has a top speed of 17km/h.

Heating the air with microwaves or an electric arc could work, since it would just be replacing burning fuel with another heat source. It would still require moving parts though (unless it's only used as a ramjet), since a jet engine has to compress the air before heating it.

handol2• 6 years ago

It would still require moving parts though (unless it's only used as a ramjet), since a jet engine has to compress the air before heating it.

You could use a tesla valve for an electric pulse jet, that would make for no moving parts.

gusgordon• 6 years ago

Here's a fairly in-depth analysis of supersonic electric VTOL aircraft: https://github.com/gusgordon/electric_jet

tldr; they become "practical" with a battery specific energy of around 1500 Wh/kg. However, if you just want to do a demonstration, they are practical now (as this post suggests).

blackrock• 6 years ago

Is it possible to have a liquid hydrogen and liquid oxygen airplane?

Essentially a rocket on wings. The fuel (hydrogen and oxygen) can be produced electrically from renewable sources.

dragonwriter• 6 years ago

Is it possible to have a liquid hydrogen and liquid oxygen airplane?

Yeah, you just usually don't carry oxygen with you when you can get it free from the atmosphere, since it subtracts directly from your payload capacity.

trhway• 6 years ago

you don't need wings. For high-speed long distance the most efficient trajectory is ballistic - thus passenger variant Starship carrying 100-500 passengers at $2-5M/launch (thus $5-20K/ticket) will, i think, be the next transcontinental mode of transportation (less than 1 hour SF-Melbourne).

Olumde• 6 years ago

Electric supersonic flight you mean.

Supersonic Electric Flight

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