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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?"

45 of 172 comments (clear)

  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 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.

    3. 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
    4. 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...

  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 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.

    3. 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.

    4. 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

    5. 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'
    6. 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....

  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 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.

    2. 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.

  4. 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 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.

    2. 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.
    3. 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.
    4. 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)

    5. 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.

  5. 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?

  6. 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 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.
  7. 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.

  8. 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 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'
    2. 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?

    3. 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.
    4. Re:Misleading Title by trout007 · · Score: 2

      Hydrogen has 14 times the heat capacity of air.

      --
      I love Jesus, except for his foreign policy.
    5. 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...
  9. 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.

  10. 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.

  11. 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.

  12. 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.
  13. 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....
  14. 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.

  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. 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 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!

    2. 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
  17. 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!
  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 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.

  20. 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