Supersonic passenger jets might make a comeback
latimes.com
latimes.com
Be good to see what engineers can come up with using current technology to make things stronger, faster and lighter.
Always intrigued by the fluctuations in the airline industry. I remember a time when it was said 'smaller aircraft were dead, and it is the time of the super jumbos', and now the reverse is true with airlines shunning huge aircraft for smaller aircraft that can do regional hops.
Given that the R&D and deployment process for a new aircraft type is measured over decades, it would be incredibly difficult to build a plane today that will fit the market in 10 years time. Hats off to Boeing, Airbus, Embraer et al for their efforts.
A complete replacement programme was just too expensive, and what they had worked, so they stuck with it. Had Concorde been a profitable aircraft, then it might have been a different story...
All commercial x-ray sources use tubes, for example. The magnetrons that power our microwave ovens are vacuum tube oscillators.
And by their nature, tubes are much faster than semiconductors, which has its uses.
http://www.sciencemag.org/news/2012/05/return-vacuum-tube
These links will get you started.
But these articles are from 2014 and 2012 and they contradict easily looked up facts. The 2012 article claims that this technology promises speeds of up to 460GHz, which seems to have already been topped by regular semiconductor transistors, even by 2003: See https://en.wikipedia.org/wiki/Milton_Feng#World.27s_fastest_... for a really old example.
So to me it seems that this research is in a very early stage and no one knows whether the finished product (if it is ever finished) will be faster than semiconductors. Of course the researchers working on this must make big promises or they wouldn't get grants, but that's how the grant system works today, and it doesn't tell you anything about how viable the product is.
edit: Not to sound to negative here, I am really looking forward to this new technology and hope it will turn out alright. But it looks very much like fundamental research, so I take issue with broad claims like "by their nature, tubes are much faster than semiconductors, which has its uses", when apparently nothing has left the laboratory yet.
Here's a more recent link, specifically regarding terahertz research, you might find interesting.
http://iopscience.iop.org/article/10.1088/1361-6463/50/4/043...
I want to emphasize an important distinction: that vacuum-based amps have higher potential switching speeds than semiconductors is not a novel thing, nor is it early stage research. It is part and parcel of the nature of semiconductors. What is cutting-edge is miniaturization of vacuum-based systems using conventional fab processes. That's the exciting stuff!
[0] https://paulross.github.io/pprune-concorde/docs/AICU_-Air_In...
It's incredible interesting and various pilots and engineers turn up to share their stories.
Warning: Grab a LARGE cup of coffee and bag of popcorn and be prepared to lose many hours reading through that (massive) 99 page thread.
There are two editions of the book. The first edition is super cheap (eg. 29p + postage: https://www.amazon.co.uk/d/cka/Concorde-New-Shape-Sky-Ken-Ow...). There was a second edition written after the 2000 accident in France, which is supposed to be a better version, but I have not read it because it's out of print and considerably more expensive.
Two things I remember: the statement that by the end of the engineering effort "everyone was exhausted and nobody was really in control" (paraphrasing slightly from memory)
and a curious interview with a (British) engineer who was very concerned about keeping technologies proprietary at the national level--he seemed to be happy for UK firms to share know-how (as I believe is traditional, up to a point, in engineering culture) but god forbid it should be shared with another country's engineers. Shades of the Brexit mentality.
[1]http://www.independent.co.uk/news/science/climate-change-gam... [2]https://www.quora.com/How-much-fuel-do-airplanes-flying-acro... [3]http://www.smithsonianmag.com/innovation/is-a-lack-of-water-...
I'd like to see a moratorium on space tourism too. That's unlikely to be a popular view on Hacker News though, and it's got zero chance of happening anyway.
Furthermore, everyone will be given a standard monthly food ration consisting of rice, dry beans and powdered milk.
Each resident can own up to 3 "luxury" items selected from a standard catalog.
Each resident is permitted to travel no more than 150 miles from their residence each month, and personal cars are banned.
Imagine how quickly we could heal the environment if everyone could agree to these common sense restrictions!
Engine manufacturers have spent a TON of R&D on fanjet engines and making them several orders of magnitude more efficient than the engines of 20 years ago even, but supersonic flight needs more than a fanjet - they need to look at turbojets, with afterburners etc. There is not much scope to play with with those unfortunately. What works at subsonic speeds at 30,000 feet won't at Mach 2+ at 80,000 feet.
But there are other aspects to conserving energy. When Concorde lands, then energy expended by the braking systems on the rollout is the same as that used to power an average family house for a day.
If they could improve kinetic energy recovery systems (as they do on Formula 1 cars and some electric cars), then that energy could be fed back in some way, to power on board avionics etc.
Surely that's an exaggeration? (If not - I'd love links to explain what's changed... 100 to 1000 times improvement since the mid '90s seems unlikely to me though...)
Looking at actual figures:
Concorde got about 5MJ per passenger-km.
A modern 747-400 gets about 0.9MJ per passenger-km.
Meanwhile trains vary enormously but US trains appear to get about 2.7MJ per passenger-km, while Portugese ones are about 0.07MJ; but I don't know if that's comparing like with like (the data is unclear). Cars seem to get about 1.2MJ per passenger-km. A big cruise ship seems to get about 5.9MJ per passenger-km, plus you need to spend lots more energy on, essentially, life support because they're so slow.
These numbers were brought to you by https://en.wikipedia.org/wiki/Energy_efficiency_in_transport... and the 'units' command, which is awesome. Also, someone who isn't me needs to overhaul that page to use consistent units everywhere.
I'm with you, there has to be some flaw with differing methodologies going on here. It's way too discordant.
I'm surprised at the 2.7 figure; are trains really more than twice as worse as individual passenger vehicles? I can't imagine so. Especially not the trains I use most often, electric-powered urban subways.
The only US commuter train I've seen was the SFO Caltrain, which was very not electric. Are there many electric trains there?
Yes. For example, Amtrak's Northeast Corridor is electric as is light rail for the most part (entirely?). There's also an electrification project underway for Caltrain. I'm not sure about how much commuter rail in the US is electric in general.
Planes are efficient, ones they are high up in the sky because there is less air there.
Unfortunately, they need lots of energy to get up in the low pressure regions, and we do not have ways to recover that energy in landing.
Moving slower also increases the per mile efficiency, as air resistance grows faster than linear in speed.
Net effect (highly simplified) is that trains beat high speed trains irrespective of distance, high speed trains beat planes on shorter distances (up to a few hundred miles), but planes beat high speed trains if the distance covered in one hop is large enough.
Hyperloop aims to change that by being a train riding at low atmospheric pressure (planes don't only burn fuel to go from A to B, they also burn fuel to stay up; hyperloop wouldn't need to do the latter) (edit: ideally, it also would recover energy on braking)
Also, that's a little bit of an apple to oranges comparison - I wonder what the numbers look like comparing a Concorde-vintage 1976 (or 1969?) 747 with a modern 747? Or even an A380 (Which I guess is the nearest modern counterpart of a mid '70s 747?)
Whether you fly subsonically or supersonically, thermodynamic efficiency will be driven by engine pressure ratio and turbine inlet temperature. The advanced turbofans flying today have very impressive gas generator cores (high-pressure compressor, low-emissions combustors, high-pressure turbines) that would be equally applicable to supersonic airframes. The low pressure part of the cycles will definitely optimize to a different point for subsonic vs. supersonic applications, with supersonic cruise preferring higher fan pressure ratios and lower bypass ratio. Like Concorde, you are going to want to size the engines such that you do not cruise in afterburner (assuming you are staying roughly below Mach 3; above 3 - 3.5, the ramjet cycle starts becoming more favorable). However, this is all within scope for what the aeropropulsion vendors know how to do. The big issue is that the specific engine configuration you are going to want for a supersonic cruiser is unique to that application. Originally, Aerion was going to use JT8Ds, which they later shifted away from.
My point here is it's not principally an R&D issue, it's that if you want to minimize supersonic fuel consumption, you are going to want a specific configuration for which there will not be a huge engine market. Contrast with the market for something like a CFM56 or V2500. Being able to leverage the ADVENT three-stream/variable cycle work (and GE YF120 before that) will also help, but the point still stands.
Just tax the heck out of them to offset whatever damage they cause to the environment, they're price insensitive anyway.
There are some "nice things" that money shouldn't be able to buy because they have too much downside for everyone else. Regardless of how much money you have, you still have to share Earth with everyone else.
When you first read a paragraph like this without experiencing what airplane noise pollution actually means you say to yourself: "How bad that can actually be? The airplanes fly at an altitude of 10,000m, I'm sure it can't be that bad. Right?"
Wrong. Since the Ukrainian Civil War started lots of large airplanes have been diverted to fly above my parents' country house, somewhere in Eastern Europe. The closest airport is located at about 140 km, but it doesn't matter, because at least once every hour you can hear those damn big "birds" flying 10km above you. It's even more unsettling when you notice them at 5 in the morning, as you had quickly woken up ready to fall asleep again but you now can't because there's that nasty airplane noise making its way through the house's concrete walls.
Supersonic flying over populated areas would increase that shitty noise exponentially.
It is not the same as being rich enough for general aviation transportation, but if I wanted to get a pilot's license, I could do that too.
As has now been demonstrated fully in the US, rich people hardly control politics. They do support one "team" or the other, but I would not mistake that for control.
2) Americans at least have been described as "temporarily embarrassed millionaires." The odd entertainment value of gawking at rich people as celebrities is really a thing.
3) There is an eternal struggle between the Coase Theorem and Pigou taxation.
4) The people who self-select for wealth may not consume as much as people who do not self-select for wealth. I heard the quote on the show "Vikings", but I imagine it is not original with them - "power is only given to those who will lower themselves to pick it up."
It's kinda shocking that a major newspaper can cover such a topic without even mentioning climate change at all.
Sources: https://data.giss.nasa.gov/gistemp/graphs/ https://data.giss.nasa.gov/gistemp/graphs/graph_data/Global_...
[1] http://www.realclimate.org/index.php/archives/2012/04/evalua...
I would much prefer if focus where on high-speed rails that (if my memory is correct) has the lowest climate effect of all forms of travel except biking.
Agreed on HSR though - here in Australia HSR has been a pipe dream for decades...
The desire for cost savings by way of using less fuel already means that huge effort is devoted to improving jet engines (and planes, the 787 is quite different than previous jumbos). Even after all that, slower planes are more efficient than jets.
[1] https://aero.larc.nasa.gov/files/2012/11/Low-Noise-Subsonic-...
But it's also clear that current VR or even "telepresence" robots (ie. ipads on sticks) are awful and there's a huge opportunity to make virtual interaction at virtual conferences great.
Air travel makes up about 2% of human CO2 emissions. Certainly you can make an argument that a lot of it is pretty wasteful since a lot of people on airliners don't need to travel, but there are far better areas to worry about if you want to curb emissions.
The units that really matter are tons of co2 equivalent.
If you want to cut CO2, your efforts are best spent on electricity generation, heating, and road transportation.
[1] http://www.businessinsider.com/contour-aerospace-factory-des...
From financial perspective the cost of a first-class ticket is much higher proportionally than the space occupied by that seat. Full-fare first-class passengers subsidize coach passengers on a promotional or discounted ticket, enabling air travel for many.
Remove the subsidy, and average cost per coach ticket might increase, which is why Southwest (which does not have first-class in its fleet) is just sometimes, but not always, the cheapest option.
Would there be a public source for any of this data? Or anyone with in insight in these numbers that want to share anything?
It seems against any airline's self-interest to have those numbers in the open, this analysis uses the availability of free upgrades (unsold first-class seats that are given away to airline customers with preferred status) as a reasonable proxy https://skift.com/2016/08/27/the-state-of-airline-upgrades-f...
I'd imagine it's harder to get behind the carpet-bombing of a place that you've been and people you've met. Let's have more air travel, not less.
Joining the military (or a terrorist organization) should not be anyone's best chance of seeing the world. Yet sometimes it is.
This is not a piece of software app that you can just launch whenever you feel ready full of bugs. You can't pull an Uber and say, hey fuck regulations, we will just do it (https://www.theguardian.com/technology/2016/dec/19/uber-self...). Yeah, sure, if you want to fly between Inner and Outer Camelstan then you might get away with the very fashionable "disrupt" shit but if you want to fly airspaces controlled by the FAA, EASA, CASA -- and let's face it, the money is in New York, London and Sydney -- then you need to do better.
This is going to cost 5-10 billion dollars at least just based on the very fact that the C Series costed 5B and I can't see what here would make it cheaper. And it's not easy to see how are you going to recuperate that much money, this is not a big market and while obviously time is money, it's a very big question of just how much money. Gulfstream delivers 140 planes a year https://www.wsj.com/articles/general-dynamics-profit-rises-9... with about 2-2.5b profit a year. I absolutely can not see how these numbers will stack up. Is this another venture capitalist fueled hype? VC invests, hypes it up, gets rid of the stock, small investors at the end get to hold the bag.
(Still waiting for the rest of the promised street cars here in Toronto, years behind schedule)
Obviously they aren't hitting all their delivery targets, and that's worrying, but what struck me is that Bellemare said shortly after he took over the company was only a few weeks from bankruptcy.
It seems he has managed to put them somewhat back on track, TTC deliveries aside of course...
Agreed. This is due to fawning "enthusiast" type reporters with little understanding of the technical issues or the history. But then, which field is free of this phenomenon when reported by non-specialist press? Even specialist press (e.g., Aviation Week) tends to be overly credulous. The big publications that captured my imagination growing up, like Popular Mechanics and Popular Science, are really not any better.
The people with the longest head start and most interesting technology are the Aerion crowd, and they have been gestating for years without a lot of hardware to show for it. Boom, Spike, and others are receiving too little skepticism, IMO.
It's not impossible, but the market is small. The total number of known private jets in the world above $100m is about 10. There's one guy with a private Airbus 380, and a few Boeing Business Jets, including Trump's. Boeing has about 12 more Business Jets on order, but most of those are 737-based.
I thought they might not just dwindle away because they announced a cooperation with Airbus, but alas, getting enough funding probably is impossible if it's not pushed by a big corp like Airbus/Boeing and governments.
my understanding is that Concorde engines are among the most efficient built to date - they had something like 70:1 compress ratio. It is juts the nature of high speed flying that you have to burn much more fuel.
>modern jet engines are so much more efficient
because of high-by-pass. Wouldn't work for supersonic.
From https://en.wikipedia.org/wiki/Thrust_specific_fuel_consumpti... :
"For example, Concorde cruised at Mach 2.05 with its engines giving an SFC of 1.195 lb/(lbf·h) (see below); this is equivalent to an SFC of 0.51 lb/(lbf·h) for an aircraft flying at Mach 0.85, which would be better than even modern engines; the Olympus 593 was the world's most efficient jet engine.[2][3] However, Concorde ultimately has a heavier airframe and, due to being supersonic, is less aerodynamically efficient, i.e., the lift to drag ratio is far lower. In general the total fuel burn of a complete aircraft is of far more importance to the customer."
Which is why most military aircraft have to hook up to a tanker after take off to fill the tanks so they can continue on their mission. Concorde (and other passenger aircraft) don't have this luxury due to the risks involved, so I am thinking that most of the high cost of fuel vs passenger load that is being discussed in this thread is because of the voracious thirst that the plane has in the early stages.
Most supersonic aircraft are quite efficient in the cruise stage. The Lockheed SR-71 for instance, derives a fair percentage of thrust just from the shape of the airframe, so the pilots actually throttle back a little once they reach Mach 2+!
Ben worked alongside Kelly, and said that the guy had an unerring knack for designing aircraft. Ben (an aerodynamics engineer) would spend days designing an intake, and Kelly would come along and take one look at it and say "That is 20% too big", and sure enough, when Ben went back over his calculations, he would find it to be about 18% oversized.
Another great book is "Sled Driver" by Brian Shul - probably one of the best aviation books I've read (and I am a former pilot).
Sadly, I believe both books are out of print now, but you may be able to find a copy somewhere second hand. I've seen "Sled Driver" on eBay for about $3000 from time to time!!
It's great that you brought up "Sled Driver", I'm actually currently saving up to buy a copy. Brian Shul still has new copies available on his website for $250[2]. I think the copies that go for very high prices on eBay are the first editions or some of the special commemorative versions.
May I ask your opinion on the print quality of "Sled Driver"? I know Shul is a photographer, in addition to being a former SR-71 pilot, so I assume the photographic print quality is quite high. Have your read his companion book "The Untouchables"?
[1]https://www.amazon.com/Skunk-Works-Personal-Memoir-Lockheed/...
The photos in there are nice, but I would say it is on par with most coffee table style books that I've seen. Wonderful photos, but the print quality is about the same as most books of that era. To be honest, I got so caught up in the stories he tells in there that I can't recall a lot about the photography - I will have to revisit it and check it out.
Great that he has started republishing the books again. I remember about 10 years ago when it was out of print, copies were going for about $6000+ on eBay !! o_O I thought I was sitting on a goldmine. :D
I haven't read "The Untouchables", but will put a copy on my wishlist for this year. Can't get enough of books about great planes and great pilots.
To reduce structural loads the aircraft took off with a very light fuel load and refuelled in flight.
Rather interestingly, the modern fascination with SR-71 stories and facts has turned a rather mundane "weeping" of fuel into the much more exciting image of fuel almost gushing out of cracks in the fuselage at such a rate it had to be refuelled immediately after takeoff!
The trouble was they just didn't have good materials for the seals. Things have gotten a lot better in that department.
That sounds...unlikely. Do you have a source for this?
I have a suspicion you might be conflating the "turboramjet" aspect of the engine design, with the air-frame actually generating thrust.
Personally I'm of the mindset the inlet and exhaust nozzles are an integral part of the installed engine, particularly in this case given the rather unique intake/engine/exhaust design.
There is more then an order of magnitude of complexity between designing a vehicle that can travel at Mach 2, and one that can travel at Mach 22. Personally, I'd pass on the risks of hypersonic re-entry for my SEA->NYC flight... And on having to pee into an astronaut diaper.
Space travel (And a ballistic suborbital hop is 90% of the way there) is, as a mode of transportation, incredibly dangerous.
With suborbital flights, neither breathing nor descending more quickly would be an option.
Just take a look at the typical orbit of a SpaceX second stage over the Atlantic: https://youtu.be/zBYC4f79iXc?t=32m13s - A suborbital flight that just barely goes back deep enough into the atmosphere over Africa to slow down would look almost exactly the same and wouldn't even be 100 m/s slower.
Compare that to the tiny ballistic arc of the first stage. That's how your suborbital flight would look like if you want to hit the atmosphere at a speed that doesn't require a heat shield.
A rocket could be fuel-efficient only if it accelerates very quickly, passengers won't survive.
Hopping up into space, and then back down to where you came from is only ~1,600 m/s.
Hopping up into space from New York, and landing in London requires closer to ~6,000 m/s.
Here are some specs for an ICBM. It has a range of 6,000 miles, and has to reach ~7 km/s (Mach 23) to do so. [2]
The mathematical reason for why suborbital flights that take you somewhere require so much velocity is because all ballistic trajectories are actually elliptic orbits. When you throw a baseball into the air, it is in an elliptic orbit - a very small orbit, with most of it passing through the space occupied by the earth. The Earth's center is one of the two centers of the ellipse.
This means that in order to send a ballistic rocket to the other side of the world, you need to 'almost get into orbit'. At this point, it takes very little energy to turn your orbit into a circle... But it also means that you had to expend orbital-levels of energy to get to the point that your suborbital hop takes you somewhere. [3]
Knowing that sub-orbital ballistic trajectories are ellipses, with one of their centers at the center of the Earth, you can calculate the velocity requirements yourself by using Kepler's second law.
[1] http://www.orbspace.com/Background-Information/Suborbital-vs...
[2] https://fas.org/nuke/guide/usa/icbm/lgm-30_3.htm
[3] http://lh3.ggpht.com/_1wtadqGaaPs/TF0zyBaNisI/AAAAAAAANLc/uU...
[1] https://www.amazon.com/Orbital-Mechanics-Applications-Tom-Lo...
• Comfort • Speed • Price
I wonder how post-Concorde passenger jets would fit in, assuming they ever made it down to our level.
> A flight from Los Angeles
> to Tokyo would take about
> five hours, compared with
> almost 12 hours today
Beating JAL or ANA first class, even with a seven hour reduction, will take some doing.As you say, even cutting out 5 to 6 hours isn't that big a deal.
I hate to say it, but American is way better in this regard.
But to your broader point. Modern lie-flat business class is far more comfortable with personalized entertainment options (and plugged in via WiFi if you want) than first class on PanAm ever was. Long flights are still kinda boring but I'm not sure they're painful enough that any but a vanishingly small sliver of people who aren't already flying in private jets would pay a huge premium for them.
This is why it only ever flew transatlantic. It was originally envisioned to also fly across the US, e.g. NYC to LA, but this was banned due to noise concerns.
Had the Concord been permitted to fly over the continental US, it could have been much more successful than it was.
How much that was because of the sonic boom is a matter of some debate.
No, it's actually not a matter of debate at all. See FAR 91.817 [0]
No person may operate a civil aircraft in the United States at a true flight Mach number greater than 1
* http://www.sciencemag.org/news/2016/11/average-us-family-des...
*https://en.wikipedia.org/wiki/Environmental_impact_of_aviati...
Apparently it was an unusually safe aircraft with no accidents for 30yrs until this incident. I won't ruin it but what caused it is also interesting from an engineering perspective.
Once the powerful are hooked there will be no going back.
You'd think with advancements in telecommunications - the internet, etc - there'd be even less reason to need to be physically present in a place.
Even among executives/investment bankers/international lawyers, there really isn't that much demand to go back and forth from the US East Coast to Western Europe in a day which was a big pitch from the Concorde. A faster plane starts to look more interesting Trans-Pacific but that's a whole other set of tech challenges. (It's greater than the Concorde's range.)
After BA upped the ticket prices and the wealthy customers just kept paying, the service quickly became profitable for them, and remained so until the crash.
For any new entrant to this market, it will need to remain an expensive niche.
After BA had been privatised they bought themselves out of that agreement, ending the subsidy but pocketing the profit directly. They then proceeded to operate the fleet for another 20 years.
So, in a British context, on an operating basis Concorde absolutely was economically viable. On a program basis, considering all the development costs, it was not; but then again the Boeing 787 program is > $30 billion in deficit right now and is unlikely to ever clear that.
I'm full of admiration for Concorde as a technical achievement, but it's certainly easier to make a profit if you don't have to pay for your aircraft or initial stock of spares, let alone the development costs of the plane...
I don't mind paywalls, but _this_ is egregious to me. Fuck the LA Times.
This is a comment system. I had a comment.
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Enjoy.