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Baby Is Healed with First Personalized Gene-Editing Treatment

https://www.nytimes.com/2025/05/15/health/gene-editing-personalized-rare-disorders.html
99•jbredeche•1h ago•48 comments

I Don't Like NumPy

https://dynomight.net/numpy/
171•MinimalAction•3h ago•77 comments

The current state of TLA⁺ development

https://ahelwer.ca/post/2025-05-15-tla-dev-status/
29•todsacerdoti•1h ago•1 comments

Dr. Dobb's Journal Interviews Jef Raskin (1986)

https://computeradsfromthepast.substack.com/p/dr-dobbs-journal-interviews-jef-raskin
17•rbanffy•1h ago•5 comments

Launch HN: Tinfoil (YC X25): Verifiable Privacy for Cloud AI

76•FrasiertheLion•3h ago•44 comments

Improving Naval Ship Acquisition

https://www.construction-physics.com/p/fixing-naval-ship-acquisition
19•Luc•1h ago•12 comments

A Tiny Boltzmann Machine

https://eoinmurray.info/boltzmann-machine
188•anomancer•6h ago•32 comments

The Unreasonable Effectiveness of an LLM Agent Loop with Tool Use

https://sketch.dev/blog/agent-loop
8•crawshaw•30m ago•1 comments

Show HN: Min.js style compression of tech docs for LLM context

https://github.com/marv1nnnnn/llm-min.txt
124•marv1nnnnn•6h ago•36 comments

Malicious compliance by booking an available meeting room

https://www.clientserver.dev/p/malicious-compliance-by-booking-an
229•jakevoytko•6h ago•216 comments

New paradigm for psychology just dropped

https://www.experimental-history.com/p/new-paradigm-for-psychology-just
17•CharlesW•1h ago•18 comments

Fetii (YC S22) Is Hiring

https://www.ycombinator.com/companies/fetii/jobs/QDjleWs-senior-operations-manager-fetii
1•Mattiommi•3h ago

Harvard Law paid $27 for a copy of Magna Carta. It's an original

https://www.nytimes.com/2025/05/15/world/europe/harvard-law-magna-carta-original.html
66•jgwil2•1h ago•16 comments

Onfim's world: Child artists in history

https://resobscura.substack.com/p/onfims-world-medieval-child-artists
25•benbreen•3h ago•5 comments

Coinbase says hackers bribed staff to steal customer data, demanding $20M ransom

https://www.cnbc.com/2025/05/15/coinbase-says-hackers-bribed-staff-to-steal-customer-data-and-are-demanding-20-million-ransom.html
181•gpi•4h ago•187 comments

Human

https://quarter--mile.com/Human
643•surprisetalk•17h ago•249 comments

Lua for Elixir

https://davelucia.com/blog/lua-elixir
156•davydog187•2d ago•59 comments

Internet Artifacts

https://neal.fun/internet-artifacts/
584•mikerg87•2d ago•118 comments

The Scalar Select Anti-Pattern

https://matklad.github.io/2025/05/14/scalar-select-aniti-pattern.html
7•goranmoomin•23h ago•0 comments

Show HN: Real-Time Gaussian Splatting

https://github.com/axbycc/LiveSplat
105•markisus•6h ago•44 comments

The Fastest Way yet to Color Graphs

https://www.quantamagazine.org/the-fastest-way-yet-to-color-graphs-20250512/
28•GavCo•2d ago•8 comments

Model Organisms Are Not Static

https://www.asimov.press/p/model-organisms-are-not-static
23•mailyk•4h ago•4 comments

How we made billing backendless

https://useautumn.com/blog/backendless
24•ayushrodrigues•6h ago•35 comments

Pathfinding

https://juhrjuhr.itch.io/deep-space-exploitation/devlog/945428/9-pathfinding
86•sebg•7h ago•28 comments

Show HN: Undetectag, track stolen items with AirTag

https://undetectag.com/
36•pompidoo•4h ago•46 comments

A Rust API Inspired by Python, Powered by Serde

https://ohadravid.github.io/posts/2025-05-serde-reflect/
46•lukastyrychtr•4d ago•20 comments

Radiance Contrasts at Possible Lunar Water Ice Exposures Seen by ShadowCam

https://iopscience.iop.org/article/10.3847/PSJ/adb8d1
6•PaulHoule•2d ago•0 comments

AlphaEvolve: A Gemini-powered coding agent for designing advanced algorithms

https://deepmind.google/discover/blog/alphaevolve-a-gemini-powered-coding-agent-for-designing-advanced-algorithms/
958•Fysi•1d ago•253 comments

Wavelet Trees: An Introduction (2011)

https://www.alexbowe.com/wavelet-trees/
36•Tomte•4h ago•9 comments

Working on complex systems: What I learned working at Google

https://www.thecoder.cafe/p/complex-systems
210•0xKelsey•2d ago•112 comments
Open in hackernews

In the US, a rotating detonation rocket engine takes flight

https://arstechnica.com/space/2025/05/venus-aerospace-flies-its-rotating-detonation-rocket-engine-for-the-first-time/
65•LorenDB•8h ago

Comments

ColinWright•8h ago
From the article:

"In contrast to a traditional rocket engine, in which a highly pressurized propellant and an oxidizer are injected into a combustion chamber where they burn and produce an energetic exhaust plume, a rotating detonation engine is different in that a wave of detonation travels around a circular channel. This is sustained by the injection of fuel and oxidizer and produces a shockwave that travels outward at supersonic speed."

Nope ... on my way to do web searches to try to figure out what this means.

First stop: https://en.wikipedia.org/wiki/Rotating_detonation_engine

"A rotating detonation engine (RDE) uses a form of pressure gain combustion, where one or more detonations continuously travel around an annular channel. ... In detonative combustion, the flame front expands at supersonic speed. It is theoretically up to 25% more efficient than conventional deflagrative combustion ... Disadvantages include instability and noise."

No images, no animations.

OK ... bookmarked, and I'll chase the references later.

Edit: OK, here's the best reference I've found so far:

https://www.sandboxx.us/news/what-is-a-rotating-detonation-e...

Now back to work.

philipodonnell•8h ago
If I’m understanding this correctly, if you set off one bomb the explosion travels at a certain speed, but if you put a bunch of bombs in a circle and set them off one at a time, the very last explosion will be going a lot faster than the first one?
kd5bjo•7h ago
From my understanding, it's more that the explosion phase of a detonation is more fuel-efficient than the burning phase, but can't last very long under normal circumstances because the flame front is moving so fast-- This is a trick to continue fueling the explosion to sustain it over an indefinite time period.

Think about it in terms of an old-fashioned gunpowder line fuse: If you lay it out in a ring and have some kind of mechanism to continuously place down new gunpowder on the ring in front of the flame, you can keep it going until you run out of fuel.

twic•5h ago
What i've never understood is how detonation can be more efficient than deflagration. What does that mean? Both types of engine take a mix of fuel and oxidiser and turn it into hot combustion products. The hot combustion products then expand through a nozzle to produce thrust. How is that process different between the two? Does a deflagration engine leave some fuel unburnt, that a detonation engine burns? Does the combustion of the same fuel somehow produce more heat? Or less heat but more pressure? Is it something about the expansion?

To put it another way, if you set up a deflagration engine and a detonation engine next to each other, and fed them fuel and oxidiser at the same rate, how would the streams of exhaust gas coming out of them look different? What other external differences would you see?

Symmetry•5h ago
The energy produced by the combustion is the same but different fractions of it are converted into work. Just like efficiency differences in other types of heat engine.
slow_typist•3h ago
η = 1 - ( T_c / T_h )

Carnot-Efficiency is the theoretical limit of the cycle’s ability to get work out of the thermal energy where T_c is the exhaust (coldest) temperature after expansion and T_h the hottest temperature (before expansion). Temperatures given in K (Kelvin), so 100% if you manage to get T_c to absolute zero temperature.

mannykannot•4h ago
This is mentioned in the introduction here [1]. The version I'm looking at is an image, so I cannot easily copy-paste the relevant passage, but it seems to say that the efficiency gain comes from detonation causing the combustion to occur at a higher pressure than in the case of deflagration. Generally speaking, higher peak pressures increase the efficiency of heat engines, as this allows for greater expansion of the working fluid, and thus more work being done for the same fuel consumption.

With regard to your comparison, I guess this means that the detonation engine can have a higher pressure in the combustion chamber, together with a larger bell, a faster-moving exhaust, or some combination.

[1] https://arc.aiaa.org/doi/10.2514/6.2013-3971

xeonmc•3h ago
Just think in terms of the P-V diagram, you want the pressure increase curve to be as vertical as possible to maximize the area enclosed by the cycle
Symmetry•7h ago
You've got the speed at which a detonation progresses within the explosive material and the speed at which the shock wave travels through the air. Neither is going to change based on the bomb's arrangement. But if you detonate a string of bombs so that each goes as the shock front from the first reaches it you can get, through constructive and destructive interference, a shockwave going mostly in one direction. But that's mostly not related to how this engine works.
magicalhippo•7h ago
Integza made a YouTube video[1] where he visited a lab where they had a RDE, and includes some nice explanations, animations and slow-mos of the prototype in action.

His channel has a certain flavor, but at least the video is informative.

[1]: https://www.youtube.com/watch?v=fRMMSyCcTDI

nfriedly•5h ago
> His channel has a certain flavor

It's kind of an anti-tomato flavor.

zelos•7h ago
Scott Manley has a great video about them: https://www.youtube.com/watch?v=rG_Eh0J_4_s
coreyh14444•7h ago
My first thought when I read this: "I bet Scott Manley has a video about this."
pxndxx•5h ago
Steve Mould has a "rotating flame" video which also helps visualize this: https://www.youtube.com/watch?v=SqhXQUzVMlQ
Symmetry•7h ago
Those descriptions are actually both correct, but one is describing the elephant's trunk and another the elephant's ear.
Symmetry•7h ago
To be a bit more clear, the detonation is racing around a circular track in one plane, but the net thrust is in the direction perpendicular to that plane. Fuel and oxidiser are continuously pumped in all along the track, dropping to ~0 after a detonation and rising afterwards until the detonation front arrives again. Since you don't have to pump into a continual high pressure deflagration like in a conventional rocket engine this looks like it should be easier in terms of pump power.

Rocket engine efficiency, like all heat engine efficiency[1], governed by the difference in temperature between hot and cold in the cycle. Because at any given point in a detonation engine the combustion engine only comes in pulses it can reach temperatures that would otherwise melt the rocket engine. That's true of regular rocket engines too, which use active cooling, but seems more true of a detonation engine. And I would guess that the exhaust, already being supersonic, needs less of a chock on the de Laval nozzle to ensure laminar flow.

[1] Strictly speaking this only applies to combustion rocket engines. An ion engine, for instance, is a rocket engine but not a heat engine.

kragen•3h ago
By "chock" do you mean "impact"? In English a chock is a rubber wedge you put under a wheel to keep it from rolling, or various similar objects, or the act of using one to keep something from moving: https://en.wiktionary.org/wiki/chock
Symmetry•57m ago
Oops, that should have been "choke".
yread•7h ago
The first reference in the wiki article has a nice animation

https://www.rtx.com/news/2025/03/04/more-power-no-moving-par...

hammock•4h ago
I imagine an internal combustion engine with a ring of spark plugs firing rapidly in sequence into a nozzle that has fuel/air injected uniformly

That is my naive attempt to grok with an analogue, that is probably wrong.

xeonmc•4h ago
Basically it's a turbine engine but the rotating blades are replaced with orbiting shockwaves instead.
kragen•3h ago
That makes no sense at all. How do you think a turbine engine works?
casey2•7h ago
2 hours? What's the point? It could be 0 minutes with a 0% explosion rate and the total travel time would probably be longer.
zdragnar•7h ago
The point is reduced fuel use and faster response times (either emergencies or warfare).

Maintaining a detonation (as opposed to deflagration) is quite a technical challenge. If nothing else, it pushes mechanical engineering and material science forward.

K0balt•6h ago
At supersonic speeds, the efficiency of an engine like this can be very high, and at high altitudes, travel is very efficient. People don’t seem to get that there is potential for more efficient transport at supersonic speeds/ hypersonic speeds. The ultimate example of this a satellite. How many times does it circle the world every 45 min, all on that initial fuel it took to get it up there? It seems wasteful, but it’s actually the most efficient form of transportation in existence.

Of course, hypersonic transport would not be as efficient as a satellite, but still, at 100k feet, for example, you can go 5000km/h while only consuming the same amount of fuel that you would use to go 300km/h at sea level. The potential for efficiency gains are huge, and the fuel cost of getting to altitude is mostly returned in the descent.

Of course, the technical challenges are also huge, so I don’t expect to see hypersonic airliners any time soon, but when we do get them, they could easily be 6-7x as efficient as existing transports. And it would be nice to have long haul flights be 3x as fast or faster.

People mistakenly assume that this kind of travel only has applications for the military or the elites, and, like air travel in general, that will probably be initially true. But after the rich and the government foots the bill in lives and research to make it safe and economical, it should hold huge gains for society at large.

Science and engineering is one of the only cases where trickle down economics actually kind of works. In knowledge, a rising tide really does lift all boats.

hermitcrab•4h ago
Presumably, you have to be travelling quite a distance before hypersonic/high-altitude flight becomes more efficient than current commercial airliners.
Voultapher•1h ago
What about noise? So far all we have gotten is companies trying to build planes that still are very loud and produce audible booms all the way along their travel path. Pitched to the empathetic heros that are billionaires. And to sway public opinion they fly test planes at slightly over mach one in specific weather and altitude setting that avoids having the sonic booms reach the ground. While marketing and selling the idea of not mach 1.1 but mach 2-3 supersonics. Which is AFAIK completely impossible without the boom issue, even if made less bad - but arguably still bad - by fancy wing shapes. So all I see is selfish people trying to build something at expense of everyone else, including the environment.
alnwlsn•7h ago
Fuel efficiency is the answer for "why would you do this?" That's really important for rockets, since to launch each gram of fuel you have to have some more fuel which you also have to lift.
verzali•7h ago
>Sassie Duggleby and her husband, Andrew Duggleby, founded Venus Aerospace nearly five years ago with the long-term goal of developing powerful rotating detonation engines and building a hypersonic aircraft that could carry perhaps a dozen passengers and travel at astonishingly fast speeds worldwide.

As an engineering project it sounds really cool, but is the application really commercial travel? I would have thought the military would be far more interested and much better funded.

jcims•6h ago
From the bottom of the article:

"We're actively engaged with US defense and national security agencies as well as commercial partners exploring hypersonic applications in logistics, aerospace, and future mobility—including large primes," she said. "The enthusiasm we’re seeing reflects a broad recognition that Venus’s technology can unlock new operational and economic possibilities across multiple markets."

jrmg•4h ago
What are ‘large primes’ here?
cookingmyserver•4h ago
Primary defense contractors. Lockheed, Boeing, Raytheon, etc.
twothreeone•4h ago
M136,279,841 is pretty big..
deelowe•4h ago
It's a smokescreen for hypersonic missile development. It's a common tactic. I knew someone who worked on a novel satellite surveillance system. Their pitch was that it would allow them to engage in futures trading because the resolution of their satellites would allow unique insights into global trade for certain markets using realtime optical imaging.

The guy was former Lockheed. One night at dinner I told him to cut the BS and that their real goal was to target military/government contracts. He said "off the record" this is correct. This an unspoken goal by everyone involved - management, investors, etc.

My understanding is it can be hard to position yourself as a defense company as a start up if you don't already have a foothold in the space.

mrguyorama•2h ago
>Their pitch was that it would allow them to engage in futures trading because the resolution of their satellites would allow unique insights into global trade for certain markets using realtime optical imaging.

I mean, that pitch is an accurate claim if the insights in mind are "We just told the pentagon to blow up these pixels". That tends to affect global trade and futures markets.

Voultapher•1h ago
The amount of times the word "hypersonics" was mentioned should be pretty clear sign they are aiming for DOD money.
aaron695•7h ago
Press release videos - https://drive.google.com/drive/folders/194_lxE-vy_ha7-5V_wFj...

Their YouTube is insanely technical, I think, lots of videos with big equations anyway - https://www.youtube.com/@venusaerospace/videos

growlNark•6h ago
> hypersonic

This is a meaningless term. There's just varying degrees supersonic. "hyper" implies a completely different thing.

EDIT: apparently the military has bastardized the term

HeatrayEnjoyer•5h ago
Hypersonic begins at 5x speed of sound.
lupusreal•3h ago
It's not a new term, and it exists because there are unique practical engineering problems associated with high mach numbers so having a term for this regime is useful even if the distinction seems arbitrary from a pure theoretically perspective.
growlNark•1h ago
Sure, but "hyper"? Is there any reason other than that it sounds cooler than "super"?

What are we going to do when we hit mach 11, start talking about "hyperhypersonic"? "superhypersonic"?

magicalhippo•40m ago
It's a distinct regime, so useful to give it a distinc name. Super and hyper are roughly synonyms, but super was already taken.

There was also some precedence from wave research back in 1938 which suggested hypersonic and ultrasonic for high frequency waves[1].

At this point it's a well-established term, with 60 years of history[2].

[1]: https://www.ias.ac.in/public/Volumes/seca/007/03/0163-0176.p...

[2]: https://secwww.jhuapl.edu/techdigest/Content/techdigest/pdf/...

Havoc•6h ago
Still trying to wrap my head around this. Doesn’t this cause insane stresses with basically all explosions being off axis? Or are there multiple sets of explosions moving at same the on opposites sides?
Tuna-Fish•6h ago
The main drawback is that RDEs need substantially stronger structure to smooth out the forces. It's still worth it, the force of the detonation (it's not separate explosions, it's a single continuous detonation front moving in a circular channel) is small enough to be containable.

There have been tests with multiple detonation fronts, but controlling them is much harder. It's very hard to have them go around the channel at exactly the same speed, so their positions relative to each other remain fixed.

slow_typist•3h ago
Plus if the rocket carries a warhead it doesn’t burn for long.
lupusreal•6h ago
JAXA flew one in 2021, to give a sense of developmental pace.
superkuh•5h ago
This is one of the few hypersonic technologies which could actually be enabling. This is because detonation speeds things up and increases range compared to deflagration (burning) without necessarily needing air-breathing added. This means the craft can remain a simple tapered cone traditional rocket and avoid shockwave imgingement sites on the craft air intakes and the thermal load of that that is so far infeasible to maintain for more than a minute or two.
pgruenbacher•5h ago
https://youtu.be/QR6iFVj_xHw?feature=shared Here's a good webinar with some visualization if you're interested in learning more.
ashoeafoot•3h ago
How do you restart after flameout?