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British Skylon Engine Passes Its Tests

An anonymous reader writes "The BBC reports that the SABRE hybrid (part air-breathing jet, part rocket) that is intended to power the Skylon single-stage-to-orbit space plane has passed its final technical demonstration test, and is now looking for money (only £250m!) to prepare for manufacturing. If this goes ahead, travel into orbit from local airports (ideally, those close to the equator) will be possible. And quite cheaply. But might it have the same legal difficulties flying from U.S. airports as the Concorde did?"

172 comments

  1. Only £250m! by bdevoe · · Score: 5, Interesting

    I sense a Kickstarter in the offing...

    1. Re:Only £250m! by ackthpt · · Score: 4, Funny

      I sense a Kickstarter in the offing...

      What's the incentive for my $25? A free ride on cuise missile?

      YEEEEE HAAAAAA!!!

      --

      A feeling of having made the same mistake before: Deja Foobar
    2. Re:Only £250m! by Anonymous Coward · · Score: 0

      Or a space lottery.
      Oddly enough, the USPTO granted a patent on space lotteries.
      http://www.google.com/patents/US20040176970

    3. Re:Only £250m! by CodeheadUK · · Score: 5, Insightful

      Nothing odd about it. The USPTO would grant a patent on the look and feel of dog eggs as trade dress if it were submitted.

      A chimp flinging turds with 'Approved' printed on them would be a better and more selective system.

    4. Re:Only £250m! by Anonymous Coward · · Score: 0

      More like $100k for ride.

    5. Re:Only £250m! by NatasRevol · · Score: 2

      Can't the chimp throw lot's of unlabelled crap too? just so the submitters know it's crap.

      --
      There are two types of people in the world: Those who crave closure
    6. Re:Only £250m! by a_hanso · · Score: 3, Interesting

      I'm more worried about this thing violating Apple patents. I mean... just look at those black, rounded edges...

    7. Re:Only £250m! by twokay · · Score: 1

      I can see it now. "Method for connecting to a Wi-Fi network from a mobile device... IN SPACE".

      --
      Wannabe nerd.
  2. One problem by 0123456 · · Score: 2

    Last I read, developing Skylon was going to cost about ten billion pounds (or maybe dollars, though it's a big number either way). So there's a big jump from having an engine to being able to fly into space from your local airport.

    1. Re:One problem by osu-neko · · Score: 2

      Last I read, developing Skylon was going to cost about ten billion pounds (or maybe dollars, though it's a big number either way). So there's a big jump from having an engine to being able to fly into space from your local airport.

      But how much of that has already been spent?

      --
      "Convictions are more dangerous enemies of truth than lies."
    2. Re:One problem by Bearhouse · · Score: 1

      Indeed. Even if the engine/rocket motor works as advertised, they would still need to reuse some kind of space shuttle tech to get back down. Whilst I admire (some) of the space shuttle tech, the jury is long ago in - massive expensive fail.

    3. Re:One problem by Mr.CRC · · Score: 4, Informative

      The propulsion system is completely different. The space shuttle was designed in the 70s and used the materials and design techniques of 40 years ago. There is no comparison.

    4. Re:One problem by Anonymous Coward · · Score: 2, Interesting

      The propulsion system is completely different. The space shuttle was designed in the 70s and used the materials and design techniques of 40 years ago. There is no comparison.

      ^ This. Also, the original space shuttle design was completely borked by military demands to increase its size. The shuttle basically suffered major bloat and feature creep, which was largely responsible for its ineffeciency and unreliabilty.

    5. Re:One problem by Anonymous Coward · · Score: 4, Informative

      Because of the low ballistic coefficient, Skylon would be slowed at higher altitudes where the air is thinner. As a result, the skin of the vehicle would only reach 1100 Kelvin (K). In contrast, the smaller Space Shuttle is heated to 2000 K on its leading edge, and so employs an extremely heat-resistant but extremely fragile silica thermal protection system. The Skylon design need not use such a system, instead opting for using a far thinner yet durable reinforced ceramic skin

    6. Re:One problem by Anonymous Coward · · Score: 1

      The space shuttle was an unpowered glider during re-entry so needed a much bigger wingspan. Skylon being single-stage, can presumably carry extra fuel to power it during re-entry as well. With powered landing you need a smaller wingspan which means less heat shields.

      P.S. give it up with the space shuttle already, it was a huge achievement in its time but no comparison to what's being developed these days.

    7. Re:One problem by HornWumpus · · Score: 2

      Wingspan will be based on (more or less) wing loading, which will be based on (more or less) landing speed.

      Power gives you an option to go around. But any orbital space plane will carry plenty of energy as a glider.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    8. Re:One problem by Anonymous Coward · · Score: 4, Informative

      Actually, the precise military design requirement that borked it was that the shuttle craft had to be capable of re-entry and landing entirely over the US continental area. They didn't want to overfly Russia, China or Europe.

      That meant that it needed to have a steep descent profile, which in turn meant a hot flight, which meant expensive and sophisticated heat protection which ended up not working very well.

      The Skylon is entirely commercial, and will have a much more sensible re-entry profile. It will be able to slow gradually in the upper atmosphere and even, with it's unique engines, start up again and fly back into orbit should it wish....

    9. Re:One problem by dwye · · Score: 1

      The shuttle basically suffered major bloat and feature creep, which was largely responsible for its ineffeciency and unreliabilty.

      False. The original shuttle design was to be capable of High Earth Orbit and powered landing (i.e., could go around again if needed, just like a jet, rather than doing a dead-stick controlled crash as the shuttle-as-built did), but was Proxmired into what we got. The Dyna-Soar (the military shuttle-like design that was cancelled in favor of NASA's) was much smaller.

    10. Re:One problem by Maury+Markowitz · · Score: 1

      "Actually, the precise military design requirement that borked it was that the shuttle craft had to be capable of re-entry and landing entirely over the US continental area. They didn't want to overfly Russia, China or Europe."

      That is incorrect. Quite the opposite, in fact.

      There was not one requirement, but two. The easier one was the need to launch a new generation of very large spy sats with an expected weight of 40,000 lbs. These had to be placed in polar orbit, so the Shuttle wouldn't have got the boost from launching to the east. As a result, the system required the more commonly quoted figure, 65,000 lbs from Kennedy.

      The second was the requirement for what is now known as "Abort, once around". The idea was to launch the Shuttle into a polar orbit, deploy, and then land, all in one mission. As the Shuttle's orbit takes about 90 minutes, that means that when it returned to the US, the launch pad is now 1,000 miles to the east of where it was on launch. This meant that the Shuttle had to manoeuvre in the atmosphere (which is way cheaper than using rockets to do it) and to get that sort of "cross range" performance they had to move to a delta wing.

      And thus the Shuttle that we all know. It's about 3 times as big as the original design, and has more wing than it needs.

      If you want to cry, look up the SERV on the wiki

    11. Re:One problem by DerekLyons · · Score: 1

      Last I read, developing Skylon was going to cost about ten billion pounds (or maybe dollars, though it's a big number either way).

      But how much of that has already been spent?

      Something shy of about two or three million IIRC...

    12. Re:One problem by cthulhu11 · · Score: 1

      Let's compare then to other English-built engines, like the ones in Jaguars and the early Sterlings. Phear!

    13. Re:One problem by Anonymous Coward · · Score: 0

      Or it was cancelled because it was called "dinosaur".

  3. The odd thing about the Skylon by Anonymous Coward · · Score: 5, Funny

    Is the strobing red light on the front. Seriously, what the frak?

    1. Re:The odd thing about the Skylon by Synerg1y · · Score: 1

      If you're a commercial airliner and see that red strobe coming, you're in for one hell of a ride.

    2. Re:The odd thing about the Skylon by Anonymous Coward · · Score: 4, Funny

      Is the strobing red light on the front. Seriously, what the frak?

      It is actually a white light, but the doppler shift makes it appear red.

    3. Re:The odd thing about the Skylon by Daniel+Dvorkin · · Score: 1

      And the way it's always looking for Sarah Connor.

      --
      The correlation between ignorance of statistics and using "correlation is not causation" as an argument is close to 1.
    4. Re:The odd thing about the Skylon by mackai · · Score: 3, Informative

      Wrong direction. Approaching would show a blue shift. Red shift means it is already passed and going away. In practical terms, one might not be able to tell the difference.

    5. Re:The odd thing about the Skylon by epSos-de · · Score: 1

      This new engine is actually cool for the British economy. Suddenly they have their own unique technology that Germany would be envy about. I am German and I am envy already.

  4. What about India? by Sperbels · · Score: 1

    Several years ago I heard that India was working on a similar engine. Never heard anything more on it, I guess it didn't work. I hope the ESA has better luck.

    1. Re:What about India? by Anonymous Coward · · Score: 0

      Nothing to do with the ESA, This is a commercial venture.

    2. Re:What about India? by ceoyoyo · · Score: 1

      Funded in part (and they hope a lot more) by the ESA.

    3. Re:What about India? by mgcarley · · Score: 1

      Yes, because things get done here on time and under budget. Oh, wait...

      Most likely reality? Money raised. Pockets opened. Cash disappeared. News censored.

      --
      Founder & COO, Hayai India (hayai.in) / USA (hayaibroadband.com) // t: @mgcarley
  5. Screw US Airports by some+old+guy · · Score: 2

    And their legal (read: environmental) difficulties.

    Launch from somewhere accessible to the market via other modes, but with sane local regulations.

    Problem solved.

    --
    Scruting the inscrutable for over 50 years.
    1. Re:Screw US Airports by h4rr4r · · Score: 1

      You will need a specially strengthened runway, so any legal trouble would be sorted out before that is built.

      A normal airport would not be useful for skylon.

    2. Re:Screw US Airports by Anonymous Coward · · Score: 1

      I'd guess a significant proportion of the users of this service would be USers, mostly rich, so if you don't plan a US air(space?)port and state that it's because of the stupid legislation you will suddenly find that the stupid legislation melts away.

    3. Re:Screw US Airports by Anonymous Coward · · Score: 0

      I too find that statement very strange indeed. What do US airports have to do with this? Americans are becoming more and more closed to outsiders, they prefer their own homegrown products over foreign ones, and they've got a healthy space travel industry of their own anyways.

      Most likely UK/ESA will look towards Latin American nations, or Asian countries like India to purpose-build airports. Then it's just a matter of hopping over to that airport (spaceport?) from wherever in the world and catching the flight out. Americans can stay in their country and use their own products, and the rest of us will continue to interact across our borders as usual. Win-win.

    4. Re:Screw US Airports by Spy+Handler · · Score: 2

      Well you wouldn't launch from just *any* airport... you always launch eastward to gain speed from earth's rotation. And you wanna be as close to the equator as feasible, and you want lots of ocean or non-populated wasteland to the east of your launch site in case your rocket blows up. Which is why we launch from the east coast of Florida or Texas.

      It would take at least a few minutes from liftoff to Mach 1, by which time the spacecraft will be over empty ocean anyways. So TFSummary about concorde noise is nonsense.

    5. Re:Screw US Airports by Anonymous Coward · · Score: 0

      I'd imagine that Branson's spaceport in (?)Arizona(?) will do the trick...

    6. Re:Screw US Airports by PPH · · Score: 3, Informative

      The US "legal troubles" were a stalling tactic* back when Boeing was trying to build their own SST. The original grass roots "ban the bang" campaign was British.

      *Do you really think Congress wouldn't have lifted the landing ban had the US version made it off the drafting board?

      --
      Have gnu, will travel.
    7. Re:Screw US Airports by tibit · · Score: 2

      Far from advising xenophobia, I'd still like to point out that US is a fucking big country. Most people in Europe, for example, have no idea what a "fucking big country" is. Even supposedly well of Germans. Given the scale of things, a "homegrown" product in the U.S. may be equivalent from something made elsewhere in Europe for someone from there, for example.

      --
      A successful API design takes a mixture of software design and pedagogy.
    8. Re:Screw US Airports by jcr · · Score: 1

      Launch from somewhere accessible to the market via other modes, but with sane local regulations.

      So, if I want to go SFO->HKG, I'd need to hop a flight to Mexico first?

      I think that would still be a win, actually.

      -jcr

      --
      The only title of honor that a tyrant can grant is "Enemy of the State."
    9. Re:Screw US Airports by Anonymous Coward · · Score: 2, Informative

      New Mexico thank you, in the unfortunately named Jornada del Muerto basin.

      http://en.wikipedia.org/wiki/Spaceport_America (wikipedia)

    10. Re:Screw US Airports by Catbeller · · Score: 2

      "Well you wouldn't launch from just *any* airport... you always launch eastward to gain speed from earth's rotation. "

      Actually, it takes off - and flies - like a jetliner, so orientation of the runway is not a factor. The pilot can turn the plane eastward after takeoff, and then gun the engine.

    11. Re:Screw US Airports by osu-neko · · Score: 1

      Launch from somewhere accessible to the market via other modes, but with a lack of sane local regulations.

      FTFY

      Why is something so rare called "common" sense?

      The more interesting question is, why do so many people who clearly lack it complain about the lack as if it's not their own problem?

      --
      "Convictions are more dangerous enemies of truth than lies."
    12. Re:Screw US Airports by some+old+guy · · Score: 1

      Read the last line of the OP.

      --
      Scruting the inscrutable for over 50 years.
    13. Re:Screw US Airports by Anonymous Coward · · Score: 0

      It has no pilot.

    14. Re:Screw US Airports by Anonymous Coward · · Score: 0

      East coast of Australia.

      Think about it.

      Pretty close to the equator, stable First World country, UK/US ally, technologically advanced and LOTS of empty space where you could go all sonic boomy if required and no-one would even care...then head out over the South PAcific.

      Perfect!

    15. Re:Screw US Airports by Anonymous Coward · · Score: 0

      Having seen the combination of Congress' shenanigans and the FAA's hostility to aviation in 20 years in the industry, yes, I believe that Congress wouldn't have lifted the ban.

    16. Re:Screw US Airports by dave420 · · Score: 1

      It does have a pilot, just not in the craft itself.

  6. .mil only by vlm · · Score: 1

    If this goes ahead, travel into orbit from local airports (ideally, those close to the equator) will be possible. And quite cheaply.

    Misdirection. Ballistic aka spacex and competitors is always going to be cheaper. This only has .mil purposes. Excellent PR work, guys!

    --
    "Science flies us to the moon. Religion flies us into buildings." - Victor Stenger
    1. Re:.mil only by h4rr4r · · Score: 2

      Citation needed.
      Why would throwing away half the craft and having to carry many tons of oxidizer, which the skylon does not need, be cheaper?

    2. Re:.mil only by UK+Boz · · Score: 1

      Calling bullshit on this one without anything to back it up

      --
      www.boznz.com Simple solutions to complex problems.
    3. Re:.mil only by 0123456 · · Score: 3, Interesting

      Fuel is cheap: rocket designers dream of a future where fuel will be the primary cost of launching things into space. Developing a space plane is not, and you have to invest all that money before you even know if it will work.

      SpaceX estimates for launches on a reusable Falcon are similar to the estimates for Skylon, and they can build up to it, starting with expendable versions that are proving the technology and making money. Skylon has the tricky 'give us ten billion and it will probably work' hurdle to jump over.

    4. Re:.mil only by phayes · · Score: 1

      All very good points. In addition this is NOT the time to be needing a 10 billion handout from either the UK or the EU. SpaceX is progressing incrementally to reusable staged rockets and does not need any more money than they are getting from their current workload. With the Skylon precooler only just exiting proof of concept tests & really being a barely tested hurdle, I don't see it going any further in today's economic environment.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    5. Re:.mil only by khallow · · Score: 2

      Fuel is cheap: rocket designers dream of a future where fuel will be the primary cost of launching things into space.

      That will only happen, if you're not throwing away a vehicle every time you launch. Else you have to add the cost of the vehicle to the launch. This is where Skylon comes in. It's a completely reusable vehicle. What it doesn't have currently is a market which justifies spending ten billion dollars or euros. You have to have a lot of launches before the development costs become a small part of overall launch costs.

    6. Re:.mil only by Cyberax · · Score: 2

      Wrong!

      Rockets can't be cheap. They are not reusable (you can try to reuse certain parts, but you're going to disassemble and reassemble them in any case) and that is ALWAYS going to put a high lower limit for their price. In the best case, you'll be paying millions of dollars for person to get to a lower orbit.

      Skylon spaceplanes can, in theory, lower that to perhaps several tens of thousands dollars. Definitely to the level of hundreds of thousands.

    7. Re:.mil only by Anonymous Coward · · Score: 1

      Wrong for one basic reason: Any craft using this type of engine would be able to fly from a regular civilian airport. Expendable rockets need a special launch facility in the middle of nowhere. That is a huge difference for scaling the system: SpaceX can launch from about three locations in the world, while a hybrid jet/rocket plane would be able to launch and land anywhere including near population centers. Therefore the potential customer base for the latter would be several orders of magnitude larger and bring economies of scale with it. This of course assumes there's going to be a market for fast intercontinental passenger/parcel service, or passenger service to space.

    8. Re:.mil only by 0123456 · · Score: 2

      That will only happen, if you're not throwing away a vehicle every time you launch.

      Sure. But if Skylon meets the launch cost estimates I've seen, fuel will still be only a few percent of that cost.

      As I understand it, they want to use air during launch to allow them to carry a bigger payload in an SSTO, not to save money.

    9. Re:.mil only by 0123456 · · Score: 1

      If you're paying $200,000 for a flight into space, the cost of a flight to the nearest suitable airport is noise in comparison. I'm far from convinced there's enough of a market for $200,000 London to Sydney flights to justify it as a high-speed airliner.

    10. Re:.mil only by Anonymous Coward · · Score: 0

      So what world do you live in where 250 million means 10 billion?

    11. Re:.mil only by 0123456 · · Score: 1

      So what world do you live in where 250 million means 10 billion?

      The world where space planes don't magically appear for free once you have engines for them?

    12. Re:.mil only by Anonymous Coward · · Score: 1

      All very good points. In addition this is NOT the time to be needing a 10 billion handout from either the UK or the EU.

      If you had read the article, you'd have discovered that development has been 90% privately funded so far, and Mr. Bond intends to keep the same ratio of private and public money in future. In addition, all that money is not going to be up front: there are stages of development to get through. Still, what a long, strange trip it's been since work on the HOTOL spacecraft was suspended in 1988. I have great respect for Bond's peristance, engineering skills, and fundraising in the years since then.

      -Gareth

    13. Re:.mil only by osu-neko · · Score: 1

      That will only happen, if you're not throwing away a vehicle every time you launch. Else you have to add the cost of the vehicle to the launch.

      Right, and since disposable products are always so much more expensive than reusable ones, reusable has the cost advantage.

      Oh, wait...

      --
      "Convictions are more dangerous enemies of truth than lies."
    14. Re:.mil only by osu-neko · · Score: 1

      Rockets can't be cheap. They are not reusable (you can try to reuse certain parts, but you're going to disassemble and reassemble them in any case) and that is ALWAYS going to put a high lower limit for their price.

      That's a weird conjecture, given that for every other manufactured thing in existence, disposable versions have a much lower limit on their price. Making things reusable always puts a high lower limit on their price. It's a lot cheaper to make something that doesn't have to last, often so much cheaper than it's cheaper than the maintenance costs of the reusable thing, even discounting the reusable items much higher initial cost.

      --
      "Convictions are more dangerous enemies of truth than lies."
    15. Re:.mil only by Cyberax · · Score: 3, Insightful

      How's that going for disposable cars and airplanes?

      Things are disposable _because_ they can be made very cheaply. Not the other way, generally.

    16. Re:.mil only by tibit · · Score: 1

      You might be onto something. Copenhagen Suborbitals is doing "damn simple" designs using common materials like steel. Sure they have different goals, but something disposable and cheap might be another approach.

      --
      A successful API design takes a mixture of software design and pedagogy.
    17. Re:.mil only by HornWumpus · · Score: 1

      How's the reusable condom holding up?

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    18. Re:.mil only by vlm · · Score: 2

      But if Skylon meets the launch cost estimates I've seen, fuel will still be only a few percent of that cost.

      Doesn't matter. Lets say you blow $10B on R+D for a launch platform. Over the life of that platform, no matter how low the fuel cost, you MUST gross more than $10B revenue before you can dream of profit.

      Competitor? Traditional tech means $2B in R+D for a launch platform. Over the life of that platform, no matter how low the fuel cost, you MUST gross more than $2B revenue before you can dream of profit.

      Normally, in aerospace, you spend more money on R+D than on vehicles. So the vehicle cost doesn't really matter. Maybe the $10B project will actually be $10.5B because they build 5 reusable vehicles each costing $100M delivered, and, the $2B project will actually be $3B delivered because they build 100 disposable rockets each costing $10M delivered. Side by side competition, the disposable rocket platform earns a profit for every penny of revenue after $3B and the reusable gets no profit until after $10.5B

      --
      "Science flies us to the moon. Religion flies us into buildings." - Victor Stenger
    19. Re:.mil only by Catbeller · · Score: 1

      There will never be an economic environment that will satisfy people who don't want us to go to space. There will always be a fiscal crisis caused by people who don't want to pay taxes, worlds without end, amen. The human race also, on the vast whole, doesn't believe we are living on a planet. We're talking people, the majority, who think Jesus or Mohammed or the Messiah or the great wheel of destruction and creation is coming to end the world. They don't believe in an actual *world* - they think reality is temporary and really a rather shoddy piece of work.

      Between people who don't believe in science or planets in the quietude of their own minds, and the majority who pray, in fear or with bitterness or with hate that the world be destroyed and remade any minute now, the governments of the world aren't going to finance anything more than tax breaks for rich people, roads for more cars, and whatever other large-scale projects people think they need to make sure the world of tomorrow is exactly like the world they grew up in.

      Space travel requires imagination. The idea to construct space colonies require entire encyclopedias of knowledge even space scientists don't believe in acquiring - they are trained to think small. We are being sold Space on the business class plan - someone makes money, ergo it is good.

      But we need to diversify our civilization's base. Staying on this planet, only here, is suicide. Mathematically certain as a meteor strike.

      Ten billion is what we spend in Afghanistan and Iraq every what, five days?

    20. Re:.mil only by Nefarious+Wheel · · Score: 1

      The junkyards are full of disposable cars and airplanes. Like the disposable razor, they last for a while then stop being useful. At that point, they're no longer economically repairable. It's just the time frame that's different.

      B-52's don't fit the mould, however. I think they'll be around for the heat-death of the universe, or they run out of ECNs, whichever comes first.

      --
      Do not mock my vision of impractical footwear
    21. Re:.mil only by Cyberax · · Score: 2

      "The junkyards are full of disposable cars and airplanes. Like the disposable razor, they last for a while then stop being useful."

      No, cars are not disposable - almost all cars work for more than 10 years (average age of a car in the US is 8.5 years). And planes most _definitely_ are not disposable - they can easily have 30-40 years of service. Most rocket components, on the other hand, are used exactly once.

    22. Re:.mil only by phayes · · Score: 1

      Go ahead & rant against the Luddites & socialists who refuse anything new or refuse to spend on space "until X is fixed here on earth", but do note that your rant is only slightly related to my post.

      Skylon is a British/European endeavor. How much the US spent on Afghanistan (or the much larger amounts spent every year on entitlements) has nothing to do with how much the UK/EU is willing to spend on a project. It's rather how much funding is left after tossing billions down the Greek sinkhole or the cuts in the UK budget to try and stem the red ink. It is in that light that funding is unlikely at present in Europa for a project with a price tag in the billions and no guarantee of success.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    23. Re:.mil only by Anonymous Coward · · Score: 0

      This whole exchange is misguided.

      You're thinking of this as a single rocket - a competitor to SpaceX or Araiane. It isn't.

      What Bond has invented is an air-breathing engine capable of working in a thick atmosphere all the way out to a vacuum. That's a leap ahead comparable to the invention of the Jet engine (which I believe the Brits also had something to do with). The Skylon plane will probably be a first demonstrator - but people are going to be tying these engines to all sorts of things. We have been trying to make ramjets go fast in the air - this engine will allow a military sprint craft to take off, climb to vacuum, go fast and then re-enter and maneuver. There will be all sorts of things which the technology will improve - space-flight is only one.

      As I recall, the Brits gave us the jet engine, together with radar, for nothing. Perhaps they'll give us this too, if we throw a bit of money at it...

    24. Re:.mil only by mjwx · · Score: 1

      The junkyards are full of disposable cars and airplanes. Like the disposable razor, they last for a while then stop being useful. At that point, they're no longer economically repairable. It's just the time frame that's different.

      Cars and airplanes aren't made to be single use or have single use components like all space launch vehicles today. Imagine what a car would cost if you needed to replace the camshaft after every trip (or even every 100KM), that's what cars would look like if they were designed like the space shuttle (yes, we'd have mass produced, drop in cam's, but they'd make motoring hellishly expensive).

      What you are talking about is ordinary wear and tear. Whilst it cant be avoided but it's not a big problem as cars tend to run for decades. In Australia it's not unusual to see an 80's car on the road, 90's cars are common. Most of the cars in our junkyards are there because they don't work any more, the majority of them are that way due to crashes. In the US, your old cars aren't junked because they are worth money in poorer RHD countries. The US exports those old clunkers to places like the Philippines where it is more economical to repair and retrofit them due to the prohibitively high price of new cars. Japan does the same thing with places like Thailand and India... Which is why it's easier to get a good JDM sports car in Thailand than it is in Australia or the US.

      Look up an Australian TV series called "Bush Mechanics" to find out just how long jury rigged and retrofitted cars can run.

      --
      Calling someone a "hater" only means you can not rationally rebut their argument.
    25. Re:.mil only by davydagger · · Score: 1

      "As I understand it, they want to use air during launch to allow them to carry a bigger payload in an SSTO, not to save money."

      it can still save money and resources.

      if very least, cary more into space and make less trips.

      In any case it will still do more with less. which is good from all perspectives concerned.

      Its like saying the burn rate in modern auto engines is higher because they want more horsepower to weight rather than fuel economy, while they get both.

    26. Re:.mil only by tehcyder · · Score: 1

      But we need to diversify our civilization's base. Staying on this planet, only here, is suicide. Mathematically certain as a meteor strike.

      Being able to get a few people into oribt and living in space stations is not going to save the human race when a meteor destroys all life on Earth. The prospect of our being able to visit and colonise planets in the forseeable future is...slim.

      What we would need would be some breakthrough on the level of acquiring FTL travel in order to make the idea of travelling outside of our solar system to find habitable planets feasible.

      --
      To have a right to do a thing is not at all the same as to be right in doing it
    27. Re:.mil only by ceoyoyo · · Score: 1

      Fuel is not cheap when you need to carry it partway into orbit.

    28. Re:.mil only by Anonymous Coward · · Score: 0

      dunno.
      but if you have to haul 100 tons to orbit you will prolly use a rocket.
      on the other hand if you want a rather comfortable ride to the
      100+ tons interplanetary "ocean" cruiser you'd prolly
      book a flight ... with meals and without having to wear a spacesuit and
      go thru cosmonaut/astronaut training ... when you're 80+ years old?
      dunno .. dunno ... it has wings?

    29. Re:.mil only by khallow · · Score: 1

      If you're doing very few launches, disposable has the cost advantage since it has lower fixed costs. If you're doing a huge number of launches, say a hundred a year or more, then reusable has the cost advantage.

  7. No by Anonymous Coward · · Score: 0

    But might it have the same legal difficulties flying from U.S. airports as the Concorde did?"

    No. For orbital trips, the folks who can afford it will fly their private jets to the piss poor Equatorial country and then fly into orbit from there. They governments will have been bought and paid for and as far as the people, well no one will dare say anything. And if it doesn't work out for whatever reason, why you just move! All you need is a standard strip and those are easy to come by.

    It's good to be super rich!

    That's the score these days.

  8. leaves me out by frovingslosh · · Score: 1

    travel into orbit from local airports (ideally, those close to the equator) will be possible

    Shucks, none of my local airports seem to be near the equator. And I don't fly since the TSA started assaulting and irritating travelers.

    --
    I'm an American. I love this country and the freedoms that we used to have.
    1. Re:leaves me out by Jafafa+Hots · · Score: 1

      Just wait until commercial space flight begins and the TSA gets authority.

      No more than 3 ounces of oxygen allowed per passenger. Must be sealed in a 2 quart size Ziplock.

      --
      This space available.
    2. Re:leaves me out by Jeremi · · Score: 1

      Shucks, none of my local airports seem to be near the equator. And I don't fly since the TSA started assaulting and irritating travelers.

      I guess the previous poster should have written "will be possible for those who are willing to make an effort".

      --


      I don't care if it's 90,000 hectares. That lake was not my doing.
    3. Re:leaves me out by nitehawk214 · · Score: 1

      travel into orbit from local airports (ideally, those close to the equator) will be possible

      Shucks, none of my local airports seem to be near the equator. And I don't fly since the TSA started assaulting and irritating travelers.

      So take the train to orbit?

      --
      I'm a good cook. I'm a fantastic eater. - Steven Brust
  9. That name by ThatsNotPudding · · Score: 2

    Good show, old chaps, but change the name. Sooner or later, a Skylon will turn on you.

    1. Re:That name by Synerg1y · · Score: 1

      rofl +1 if I had mod pts today, nice BSG reference.

    2. Re:That name by Antony+T+Curtis · · Score: 5, Informative

      Good show, old chaps, but change the name. Sooner or later, a Skylon will turn on you.

      No worries. The UK Ministry of Defense communication satellites are already called "SkyNet".

      --
      No sig. Move along - nothing to see here.
    3. Re:That name by Anonymous Coward · · Score: 0

      ...And don't even get me started on the satellites owned by the Ministry of Love.

  10. Misleading Title by trout007 · · Score: 5, Informative

    The engine doesn't exist yet. This was a test of the pre-cooler. It is a critical component and it was important.

    --
    I love Jesus, except for his foreign policy.
    1. Re:Misleading Title by Anonymous Coward · · Score: 1

      It was actually the MOST important test, because the rest of the engine is based on current tech.

      This was new, and absolutely required in order to make the hybrid work. Without the pre-cooler, there was no point in moving forward in developing the rest of the engine.

      Now, developing the rest isn't trivial - it will take significant amounts of capital, manpower, and time - but from the physics and tech standpoint, the concept is sound.

    2. Re:Misleading Title by DerekLyons · · Score: 1

      It's a critical component, granted, but only one of several.

      As an automobile analogy - this is like proving air flows through a spiffy new carburetor. Way cool, and very critical... but very, very far from a complete test of the carburetor, let alone of the complete engine.

      Sabre remains a very long way away from being proven to work.

    3. Re:Misleading Title by HornWumpus · · Score: 4, Interesting

      This test used a large tank of liquid nitrogen as a heat sink.

      Replacing your oxidizer tank with a coolant gas tank isn't a huge net gain. Any heat taken out of input air has to be put into the cooling system. Which is yet to be developed. The engine has to cool both the O2 and the inert parts of the air. My gut says: net loss for simply carrying coolant vs. simply carrying O2. A heat pump to fill this roll in flight is a major engineering challenge. It would require a metric assload of energy to operate.

      Also note any space plane will need cooling for leading edges of flight surfaces. SR-71 did this by using pre-cooled fuel and running the fuel through heat exchangers on the leading edges just before burning.

      They short circuited a huge engineering challenge by using a liquid nitrogen boiler as a heat sink.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    4. Re:Misleading Title by Vulch · · Score: 3, Insightful

      Hmmm, let's think. A space plane fueled by liquid hydrogen. Very cold liquid hydrogen. And lots of it. I wonder what they could use to cool the incoming air?

    5. Re:Misleading Title by HornWumpus · · Score: 1

      Hint: The Air and hydrogen mix a fixed ratio. There will be much more air then Hydrogen (it's not pure O2). There will be more heat in the incoming air then the Liquid H2 can absorb.

      Also note: in may (most) rocket designs the cold fuel/oxidizer is used to cool the combustion chamber. Already at a delicate balance.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    6. Re:Misleading Title by radtea · · Score: 1

      My gut says...

      It's the 21st century, hundreds of years into the Age of Reason.

      WHY for the love of everything sane does anyone think what their gut says is remotely interesting or germane to any discussion of anything?

      Announcing that you've not done any numerical analysis or quantitative reasoning regarding a purely quantitative question is a really, really bad way of convincing anyone rational you have anything interesting to say.

      And as other posters have pointed out, because the people who are doing this are Not Idiots(TM) they have already considered your point and are planning to do the actual cooling using the liquid hydrogen fuel.

      --
      Blasphemy is a human right. Blasphemophobia kills.
    7. Re:Misleading Title by trout007 · · Score: 1

      Hydrogen has a very high specific heat and heat of vaporization. From reading the wiki it says there is more hydrogen used for cooling than is needed for combustion. But part of the engine design has a part of the air bypass the compressor as well. The hydrogen is mixed and burned with this air outside the combustion chamber to recover some of these losses.

      --
      I love Jesus, except for his foreign policy.
    8. Re:Misleading Title by HornWumpus · · Score: 1

      So wiki agrees with my gut. Using extra fuel as coolant.

      Air is about 21% O2. That leaves 79% inert gases being cooled. Also note: H2, having low atomic weight, should have relatively low specific heat vs most of the gasses in the atmosphere.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    9. Re:Misleading Title by tibit · · Score: 3, Informative

      Let's see. Air at atmospheric pressure has roughly 1kJ/(kg*K) heat capacity. It doesn't matter that they ram-compress thinner air, what matters is that after the ram the air will have roughly atmospheric pressure. We can assume that just to get a ballpark figure. There's about 23% by weight of oxygen in the air. When you burn hydrogen in oxygen, you join 2 mass units of hydrogen to 16 mass units of oxygen. You end up using only 2.9% of hydrogen by weight compared to weight of air, if you want a stoichiometric burn. They supposedly cool the air down by 1140K.

      So for each kg of air, you have to remove 1.1MJ of heat, and you've only got 29 grams of hydrogen to boil off. Vaporization heat of hydrogen is 0.45kJ/mol, or 0.45kJ/1g. So the boiling hydrogen can sink about 13kJ of heat, about 1% of what you need to sink. That's a no-go. It will be a no go even if all they get after the ram is 2% of atmospheric pressure, so we can be pretty sure it's no go period.

      We get 286kJ/mol for combustion of hydrogen with oxygen, so we have available about 8.3MJ of heat from burning enough hydrogen to use up oxygen from a kilogram of incoming air. That may work out. Feel free to look at the Sabre cycle and fill in the blanks as to required flow rates and temperatures, even in an idealized fashion. It should give an idea of the project's feasibility. I'm sure real engineers have already done the legwork on all that. Just that it's not as simple as "lots of very cold liquid hydrogen".

      The real thing is their proprietary and at the moment confidential frost control. They've got those long tubes, they could put acoustic waves into them, hmm.

      --
      A successful API design takes a mixture of software design and pedagogy.
    10. Re:Misleading Title by HornWumpus · · Score: 1

      And as others have pointed out, they will be wasting extra fuel because the air is hotter then the fuel is cold. Weather it is a net gain (carrying extra fuel/coolant and drag for air scoops vs. just tanking the Oxidizer) is not obvious. These people aren't idiots, but they aren't betting their own money ether.

      Gut at an engineering level is about high level thought without running all the numbers. Particularly when you don't have all the numbers, but only a conceptual framework. For example: My gut tells me that perpetual motion is BS, I don't need to see the details. This engine is perpetual motion with heat.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    11. Re:Misleading Title by trout007 · · Score: 2

      Hydrogen has 14 times the heat capacity of air.

      --
      I love Jesus, except for his foreign policy.
    12. Re:Misleading Title by Anonymous Coward · · Score: 0

      ..this is like proving air flows through a spiffy new carburetor. Way cool, and very critical... but very, very far from a complete test of the carburetor, let alone of the complete engine.

      Umm... the only new bit IS the carburetor. A closer car metaphor would be that this is like the first proof of a fuel injector technique. A completely new way of putting the fuel/air mix into the engine. The rest of the engine can stay the same - it's well understood technology.

      You also don't seem to appreciate what this technique offers. Aircraft want to fly fast, but it's very inefficient to do this in thick air. But if they fly high, where there is little or no air, their engines don't work. This engine lets you take off conventionally, climb to a near-vacuum altitude, go hypersonic, then slow down and land conventionally.

      That's what the aim of the hypersonic ramjets we have been trying out was. The Brits are just going about it a different way...

    13. Re:Misleading Title by Man+Eating+Duck · · Score: 1

      My gut says: net loss for simply carrying coolant vs. simply carrying O2.

      I'm no rocket scientist, but it seems that the big savings is achieved by using passing air as reaction mass in an efficient manner. From the wiki:

      Because the engine uses the atmosphere as reaction mass at low altitude, it will have a high specific impulse (around 2,800 seconds), and burn about one fifth of the propellant that would have been required by a conventional rocket.[34]

      The page for the SABRE engine lists an ISP of 3600.

      --
      Are you a grammar Nazi? I'm trying to improve my English; please correct my errors! :)
    14. Re:Misleading Title by Man+Eating+Duck · · Score: 1

      ... big savings is achieved by using passing air as reaction mass ...

      Oh man, bad choice of words. Sorry.

      --
      Are you a grammar Nazi? I'm trying to improve my English; please correct my errors! :)
    15. Re:Misleading Title by HornWumpus · · Score: 1

      The point of this discussion is where will they sink the heat of the incoming air. H2 fuel will not have anywhere close to enough cooling capacity. So they have to boil off something to cool the air (which is only 1/5 O2). Might as well just tank the O2 and skip the complications.

      They could dump some more heat into the remaining fuel and oxidizer (to be used later in pure rocket mode). I still don't think it will have enough heat capacity.

      As I said, it seems like perpetual motion with heat.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    16. Re:Misleading Title by HornWumpus · · Score: 1

      Per tibits calculations below (which make sense as far as he goes), you use about 2.9% hydrogen by weight.

      16*2.9=46.4%. Vaporization heat isn't enough to matter 0.45kJ/mol. As tibit says that's 1%.

      So you'd have to start with much colder hydrogen, and oxidizer (near to absolute zero), and use the remaining tanks of fuel and oxidizer as heat sinks, and design one amazing trick heat exchanger to cool the helium loop, and find a way to cool the combustion chamber when you're feeding it relatively hot hydrogen and compressed air.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    17. Re:Misleading Title by deimtee · · Score: 2

      Hydrogen gas, because of it's low molecular weight, has a very high ISP. Given that extra fuel will exit in the engine exhaust, just chucking in enough to cool the airflow to operating temp may still be a net win.
      Also, your calculation only allows for heat of vaporisation. The H2 will also be increasing in temp by about a hundred degrees, which will absorb a lot of heat also.
      .029 g x 100K x 14 kJ/kg.K = about 40 kJ/kg. So it is going to be absorbing about four times as much heat as you calculated.

      --
      I'm guessing that wasn't on their radar screen...
    18. Re:Misleading Title by tibit · · Score: 1

      I've made a mistake, BTW, the 0.45kJ/mol is the *molecular* heat of vaporization, so that's really 0.28kJ/1g.

      --
      A successful API design takes a mixture of software design and pedagogy.
    19. Re:Misleading Title by tibit · · Score: 1

      Fixing my earlier mistake, it's even more: 6 times :)

      --
      A successful API design takes a mixture of software design and pedagogy.
    20. Re:Misleading Title by Issarlk · · Score: 1

      Quick, you must simply tell this to the Skylon team. These poor guys have been working for years on something that's doomed to fail!

    21. Re:Misleading Title by trout007 · · Score: 1

      A separate helium loop is used for the cooling. Looking at the diagram it also shows the helium being used to run several turbo pumps. Each of these removes energy and converts it to mechanical work.

      --
      I love Jesus, except for his foreign policy.
    22. Re:Misleading Title by dave420 · · Score: 1

      Luckily the people working on this aren't as arrogant as you and your gut.

    23. Re:Misleading Title by dave420 · · Score: 1

      It would help you to understand what you're talking about before attempting to shit on it.

  11. Dumb Question by avandesande · · Score: 1

    Why does the input air need to be chilled? Does this have something to do with using hydrogen in a turbine engine?

    --
    love is just extroverted narcissism
    1. Re:Dumb Question by Shoten · · Score: 1

      Why does the input air need to be chilled? Does this have something to do with using hydrogen in a turbine engine?

      Design considerations. The front of the engine intake is where they keep all the Coors Light.

      --

      For your security, this post has been encrypted with ROT-13, twice.
    2. Re:Dumb Question by Anonymous Coward · · Score: 1

      Air with hypersonic speed hits the intake and the shockwaves
      that form heat the air to 1000 decrees celsius. That's too hot
      for the latter stages, so the air must be cooled.

    3. Re:Dumb Question by maroberts · · Score: 1

      Why does the input air need to be chilled? Does this have something to do with using hydrogen in a turbine engine?

      Design considerations. The front of the engine intake is where they keep all the Coors Light.

      Its a British engine - all our beer is warm! We're actually trying for the worlds fastest ice cream van....

      --

      Donte Alistair Anderson Roberts - hi son!
      Karma: Chameleon

    4. Re:Dumb Question by roc97007 · · Score: 4, Informative

      Why does the input air need to be chilled? Does this have something to do with using hydrogen in a turbine engine?

      Covered here. It's actually an interesting read. Put succinctly, as speed increases, the temperature of the air increases, reducing efficiency.

      --
      Oliver's law of assumed responsibility: If you're seen fixing it, you will be blamed for breaking it.
    5. Re:Dumb Question by Kaitiff · · Score: 2

      clip from online article regarding this intercooler:
      But its success depends on the Sabre engine's ability to manage the very hot air entering its intakes at high speed.
      These gases have to be cooled prior to being compressed and burnt with the onboard hydrogen.

      Skylon would do the job of a big rocket but operate like an airliner from a conventional runway
      REL's solution is a module containing arrays of extremely fine piping that can extract the heat and plunge the inrushing air to about -140C in just 1/100th of a second.

      Ordinarily, the moisture in the air would be expected to freeze out rapidly, covering the piping in a blanket of frost and dislocating their operation.

      But the company's engineers have also devised a means to control the frosting, permitting the Sabre engine to run in jet mode for as long as is needed before making the transition to full rocket mode to take the Skylon spaceplane into orbit.

      It is the innovative helium cooling loop with its pre-cooler heat-exchanger that REL has been validating on an experimental rig.

      "We completed the programme by getting down to -150C, running for 10 minutes," said Mr Bond. "We've demonstrated that the pre-cooler is behaving absolutely as predicted."

      --
      If I sound stupid, it's not me talking....
    6. Re:Dumb Question by raxx7 · · Score: 1

      It's not a particular problem with hydrogen or even turbine engines. Pretty much all thermal engines benefit of having a cold air intake
      Broadly, two reasons:
      - Colder air is denser and it takes less effort to feed more air into the engine, in order to be able to burn more fuel.
      - Higher temperatures (can) yield higher efficiencies, but the engines are limited by what engine materials can whistand.

      Turbocharged petrol or diesel engines usually have a intercooler to cool down the air between the turbocharger and the engine itself. Some gas-turbine electric plants in hot locations pass the air through a room full of ice before intake.

      What these guys did was, taking advantage that they use liquid hydrogen (very cold) as fuel, they cool the air down before the intake, making life easier to everything that comes next.
      The tricky part really was designing the heat exchanger.

    7. Re:Dumb Question by HornWumpus · · Score: 1

      Coors light is not beer.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    8. Re:Dumb Question by HornWumpus · · Score: 1

      Most rocket engines take advantage of the cold liquid H2 to cool their combustion chambers.

      If the H2 is already heated the combustion chamber will melt.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    9. Re:Dumb Question by tibit · · Score: 1

      Because otherwise, once you further compress the air to pressures needed for rocket propulsion, it'll be way too hot to handle by any known materials.

      --
      A successful API design takes a mixture of software design and pedagogy.
    10. Re:Dumb Question by tibit · · Score: 1

      Boiling of the liquid hydrogen, if you don't want to dump any unburned H2 overboard, will absorb about 1% of the heat needed to be removed from the incoming airstream :)

      --
      A successful API design takes a mixture of software design and pedagogy.
    11. Re:Dumb Question by Beryllium+Sphere(tm) · · Score: 1

      Reducing efficiency, and imposing limits on materials.

      What limited the speed of an SR-71 was that the compressor inlet temperature could not exceed 427 Celsius. Try to go too fast, and the inlet compression will heat up the incoming air too much.

    12. Re:Dumb Question by Anonymous Coward · · Score: 0

      Limits on materials? Where? This is Slashdot, we will 3D print new materials, or use gluons from the LHC to build new materials. We don't believe in no stinkin' Periodic Table of the Elements, or no limits on no materials. We have a species to propagate, and a galaxy to colonize.

    13. Re:Dumb Question by florescent_beige · · Score: 1

      In your basic gas turbine thermodynamic cycle, the Brayton Cycle, combustion takes place on incoming gas that has been compressed. That's what your compressor stage is for in a jet engine. In a ramjet the kinetic energy of the air is converted to pressure by a converging-diverging compression shock nozzle. (We notice Sabre has a ramjet-type compression inlet). The process is so fast its adiabatic (no heat goes in or out). The more compression you can get before combustion the higher the efficiency.

      Adiabatic compression equals heating (ref. Charle's Law). At hypersonic speeds it gets so hot before you even start combustion the materials freak out. You can't make it much hotter by burning your fuel. Low efficiency.

      By cooling the air you can get enough compression to yield a decent efficiency. It's not a Brayton Cycle any more though because that features adiabatic compression by definition. Sabre is all about removing heat in the compression stage.

      --
      Equine Mammals Are Considerably Smaller
  12. SkyActiv by AndyKron · · Score: 1

    My SkyActiv beats your Skylon HA!

  13. life immitates art? by roc97007 · · Score: 1

    Hmm. Looks like kinda a mash-up of Serenity and the Pan Am Space Clipper.

    (Is it too late to say "geek alert"?)

    --
    Oliver's law of assumed responsibility: If you're seen fixing it, you will be blamed for breaking it.
  14. Funding and Progress by Anonymous Coward · · Score: 0

    Skylon been around long time, this is lasted version. I'm glad their making progress building the thing, getting most critical part of it done.
    I think it will be challenge though to get completed, specially with fiancial difficulties everyone having including the goverment.

    Maybe Kickstart would help, but that bit too much for Aerospace effort like a single-stage-to-orbit Space Plane.

    As for airports, i wasn't under the impression this will be airline/Sub-Orbital Liner, this was suppose to be a space shuttle/plane type. Hope it works out.

  15. The problem with this Brit engine is... by Anonymous Coward · · Score: 1

    ...Getting the oil stains out of the concrete hangar floor.

  16. They need money? I have two words for them. by NoSalt · · Score: 0

    Richard Branson

  17. Who cares about US airports! by WGFCrafty · · Score: 2

    Why should we care about it being able to fly at US airports if it needs to launch from the equator?

    This is a very neat concept, and it has implications in regular jet travel as well as space travel. The ability to cool air and compress it that much in a regular jet engine could increase efficiency astronomically! The fact that this concept works could mean we see more economical jets before we see this in space travel.

    1. Re:Who cares about US airports! by dave420 · · Score: 1

      It doesn't need to launch from the Equator.

  18. I want the pre-cooler ... by Skapare · · Score: 1

    ... for use in global warming summers to get cool air. -140C sounds terrific.

    --
    now we need to go OSS in diesel cars
  19. Way Cool! by Anonymous Coward · · Score: 0

    Way Cool!! In indeed.

  20. 250 million just to design it. No prototype by gedw99 · · Score: 1

    250 million just to design it according to the article. then a bucket load more. About 10 billion to build it.
    And whats the chance it works. Elon Musk poo poo ed in his last interview 1 day ago on video.

    1. Re:250 million just to design it. No prototype by stevelinton · · Score: 1

      I wonder if the engines could be useful even without the plane?

      Strap a bunch of them, some disposable LH2 tanks and a parachute onto the side of a Falcon and drop them when you hit Mach 5. Should improve the mass ration no end.

  21. Simple, possibly by fireylord · · Score: 1

    My understanding of this issue is that the liquid hydrogen fuel will be used to carry away the excess heat, on it's way to the engine to be burnt (obviously they're not going to be wanting to suddenly start pouring heat into a tank of superchilled liquid hydrogen).

    This craft will certainly NOT fly from normal aviation facilities due to the fack that having tens of tons of cryogenic hydrogen about could turn out to be rather dangerous in a busy airport...

    1. Re:Simple, possibly by HornWumpus · · Score: 1

      As I said above. Clearly more heat in the air then heat capacity of cold liquid H2. Also liquid H2 is typically used to cool the combustion chamber.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
  22. Geronimo! by Anonymous Coward · · Score: 0

    See right here.

  23. You mean Russia? by Roger+W+Moore · · Score: 3, Insightful

    Far from advising xenophobia, I'd still like to point out that US is a fucking big country. Most people in Europe, for example, have no idea what a "fucking big country" is.

    You mean like Russia that is actually in Europe (at least the part that fits given that it is so large it spreads over two continents), contains 10 time zones, and has a land area almost twice that of the US?

    1. Re:You mean Russia? by HornWumpus · · Score: 0

      Way to miss the point. Their are American states bigger then many European countries. Many Europeans are terrible at geography. They like to tell us to 'just build trains' without a fucking clue.

      Russia is whole different issue. Calling Russia 'part of Europe' is, at best, a half-truth.

      Hell Russia is more like the USA then it's like Europe. After all Russia and the USA had to save Europe from itself (and it's love of government power).

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    2. Re:You mean Russia? by Anonymous Coward · · Score: 2, Funny

      His point was that Europeans know about Russia, and that makes them acquinted with a "fucking big country".

      Actually, it's mostly Americans who have no clue how big their country is, rich in natural resources, not densily populated and unscathed by wars, so they attribute their economical superiority merely to them being "American". Europeans know that only the EU as a whole compares to the USA.

      As for your Godwin, what you call "love of government power" should be called "imperialism". Currently the only country in the world which can be called imperialistic is America, so congratulations on defeating that evil!

    3. Re:You mean Russia? by Anonymous Coward · · Score: 1

      Their[sic] are American states bigger then many European countries.

      Yes, and there are American states smaller than many European countries. So?

    4. Re:You mean Russia? by HornWumpus · · Score: 0

      You can call anything, anything. The fact that morons throw fascist and imperialist around without knowing their history or meaning is on them, not me.

      Do you care when some fox watching moron calls you a 'socialist'? So you understand how I feel when you call me (imperialist/fascist/racist)?

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    5. Re:You mean Russia? by HornWumpus · · Score: 0

      Only shitty ones.

      Texas is 696,200 km, bigger then any European nation.

      California is 424,000 km, only Sweden, Ukraine, Spain and Germany are bigger. (WTF is Turkey doing in the list? Asia) Also not sure about how much of Russia is in Europe.

      Let's not even discuss Alaska.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    6. Re:You mean Russia? by Anonymous Coward · · Score: 1

      Perhaps I phrased it unclearly, but of course I meant that the semantic aspect of your statement should be changed, not simply the wording.

      And I didn't call you anything?

      I get the impression that you may systematically fail to identify the moron in the discussions you participate in.

    7. Re:You mean Russia? by Anonymous Coward · · Score: 0

      You are also not sure how much of Turkey is in Europe, apparently.

      Anyway, Florida wins this pissing contest by virtue of looking the most like a dick.

    8. Re:You mean Russia? by Anonymous Coward · · Score: 1

      Only shitty ones.

      Texas is 696,200 km, bigger then any European nation.

      Hmm, the european part of Russia is way bigger, almost 4.000.000km, which is well over twice Alaska. That's about 40% of Europe, and almost one quarter of Russia.

      California is 424,000 km, only Sweden, Ukraine, Spain and Germany are bigger. (WTF is Turkey doing in the list? Asia) Also not sure about how much of Russia is in Europe.

      Not Germany (~357.000km), but France (~550.000km). Germany is really small for ~82 million people.

      Let's not even discuss Alaska.

      FTFY

    9. Re:You mean Russia? by tehcyder · · Score: 4, Funny

      Many Europeans are terrible at geography.

      Oh, the fucking irony.

      --
      To have a right to do a thing is not at all the same as to be right in doing it
    10. Re:You mean Russia? by tehcyder · · Score: 1

      No, you equated Nazi Germany (defeated by the USSR and USA) with "love of government power", thereby implying that anyone who wasn't anti-government like US libertarians was a Nazi. Quite how this fits in with the fact that (a) the USSR was pretty big on government power too and (b) both the USSR and USA required governments to finance and organise their militaries, I don't know.

      --
      To have a right to do a thing is not at all the same as to be right in doing it
    11. Re:You mean Russia? by Eunuchswear · · Score: 1

      California is 424,000 km, only Sweden, Ukraine, Spain and Germany are bigger.

      France (551,695 km2) isn't in Europe now?

      In fact if you include all of France, not just metropolitan France it's not much smaller than Texas (674,843 km2 compared to 696,241 km2 for Texas)

      --
      Watch this Heartland Institute video
    12. Re:You mean Russia? by ceoyoyo · · Score: 1

      "(and it's love of government power)"

      The geography statement was ironic. So is this one, referring as it does to one country with one of the few successful centrally planned totalitarian regimes and another with one of the largest governments in the present world.

    13. Re:You mean Russia? by Anonymous Coward · · Score: 0

      ahh, perhaps they mean like the 1700 km train ride I took from Amsterdam to Rome in 10hr, which would have been more like 6 or 7 without the Alps in the way. using the same ancient Italian high speed train would bring one from denver to nyc in the same time. yea, american is way too big, americans need cars so they can drive individually in 24 hours from denver to nyc they do every other week. makes total sense, they need airports so they can travel more uncomfortably with more limitations and for more money, and save 30% off the time compared to a 20 year old train. haha, yup. its the Europeans who are clueless.

  24. Depends by Roger+W+Moore · · Score: 1

    Well you wouldn't launch from just *any* airport... you always launch eastward to gain speed from earth's rotation.

    That depends on what the purpose of your flight is. If you want to get into orbit you are correct but if you just want a sub-orbital hop between two points on the Earth's surface it doesn't really matter and given the current lack of large passenger destinations in orbit I would guess that this is the most likely initial application.

  25. The direction space travel should've taken by GodfatherofSoul · · Score: 4, Interesting

    Many years ago in high school I think, I wrote a report on the X-15 rocket plane. The impression I got was that, while vertical rocket technology got us further faster in the short term, a more gradual development of hypersonic planes would've been better in the long run. We might have had a whole generation of space planes lobbing satellites and even space tourists capsules cheaper, more safely, and with faster turn-around time. I'm not an engineer, so I could be completely full of crap, too.

    --
    I swear to God...I swear to God! That is NOT how you treat your human!
  26. Re:What about the SGC? by elfprince13 · · Score: 1

    Didn't they start building these into F-302s back in 2002?

  27. Yes, finally by Anonymous Coward · · Score: 0

    we have the technology to go nowhere! How exciting, maybe we can visit that tree fort for adults, the ISS. Yay!

  28. Re:What about the SGC? by Sperbels · · Score: 1

    Nah, those used a hyperspace window generator

  29. Re:What about the SGC? by elfprince13 · · Score: 1

    They had a hybrid propulsion system with 4 distinct subsystems employing different technologies. Traditional jets, aerospikes, traditional booster rocket, and a hyperspace window generator.

  30. posters are losing their touch by cellocgw · · Score: 1

    Nobody posted "....oops I thought it said 'Cylon' ..." yet.
    fooey

    --
    https://app.box.com/WitthoftResume Code: https://github.com/cellocgw
    1. Re:posters are losing their touch by Anonymous Coward · · Score: 0

      Low hanging fruit.

  31. Get real for a second by gelfling · · Score: 1

    The FAA won't certify airplane engines to run on unleaded fuel because of the potential hesitation and reliability problems. They're not going to certify this. Oh maybe in a hundred years.

    1. Re:Get real for a second by ceoyoyo · · Score: 1

      The FAA has started certifying rockets.

  32. Skyfall 2012 TS XViD UNiQUE by skeeto · · Score: 0

    Skyfall 2012 TS XViD UNiQUE http://thepiratebay.se/torrent/7818787/Skyfall_2012_TS_XViD_UNiQUE [thepiratebay.se] magnet:?xt=urn:btih:6d7882c59d6555283745f31e0492ac8d041132a1

  33. Re:What about the SGC? by Anonymous Coward · · Score: 0

    An aerospike isn't a propulsion system, it's an expansion nozzle. The Lockheed X-33 was the new hotness when this episode was written and the writers didn't do the research.

  34. legal difficulties flying from U.S. airports by dakra137 · · Score: 1

    re: But might it have the same legal difficulties flying from U.S. airports as the Concorde did?"
    Yes, international laws and laws of physics. Consider, "travel into orbit from local airports (ideally, those close to the equator)..." It would violate international laws to extend the borders of the USA to the vicinity of the equator. In the absence of that, the laws of physics make it harder to launch from the USA's latitude closest to the equator, namely Hawaii for a state, maybe the US Virgin Islands for a territory.

  35. Press release by Keith+Henson · · Score: 4, Informative

    On another list someone asked me to explain the press release. Here is my try.

    Hypersonic engines are up against hard physics. The ram air heats so much in the inlet that it's hard for combustion to add much energy to make it go faster out the back.

    The idea behind the SABRE engines is to cool the ram air before it is compressed. The heat exchanger to do this is what the press release is all about. With not much more than a ton of mass, it sucks 400 MW of heat out of the incoming air, dropping the temperature from 1500 C to -150 C in a few inches of heat exchanger that looks much like fabric because the tubes are so tiny.

    The engine cycle also uses the temperature difference between the ram air and the LH2 to run the compressor. It takes close to 2/5th of the energy from burning hydrogen to liquefy it. The engines recover much of this by running a helium turbine on the temperature difference between the ram air and the liquid hydrogen flow to the engines. The turbine powers the compressor stage that raises the pressure of the -150 C air to rocket chamber pressure.

    The design is extremely clever thermodynamics which also avoids most of the metallurgical problems of high temperature. Fabricating the air to helium heat exchanger was a very hard task. They have miles of tiny tubing, tens of thousands of brazed joints and they don't leak!

    Using these engines and breathing air, the vehicle reaches 26 km and about a quarter of the velocity to orbit giving an equivalent exhaust velocity (back calculate from hydrogen consumption) of 9 km/s. That's twice as good as the space shuttle main engines. It is expected to go into orbit with 15 tons of payload out of 300 or 5% even though the rest of the acceleration is on internal oxygen that only gives 4.5 km/s exhaust velocity.

    Leaving out the oxygen and using big propulsion lasers to heat hydrogen reaction mass, such a vehicle would get 25% of takeoff mass to LEO, reducing the already low cost by a factor of 5. That's enough to change the economics of power satellites from being too expensive to consider to a cost substantially less expensive than any fossil fuel.

    But try explaining any of this in a press release.

    --
    End MGM. Get prospective parents of boys to Google: Men do complain
  36. D'oh the humanities by Roger+W+Moore · · Score: 1

    Many Europeans are terrible at geography.....Russia is whole different issue. Calling Russia 'part of Europe' is, at best, a half-truth.

    This is probably the most unintentionally ironic post I've every seen on on Slashdot. Since I am guessing that you won't understand why anyone is saying that have a look at this. Now I'll grant you that the boundary between the Asian and European continents is not well defined but even allowing for sizeable error bars on the boundary you will notice that actually quite a large part of the European continent belongs to Russia. So saying that "Russia is part of Europe" is not a half truth but the complete truth: literally a part of Europe is Russian. Oh, and just in case your geography knowledge exceeds your English ability you might also want to look up irony.