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British Spaceplane Skylon Could Revolutionize Space Travel (ieee.org)

MarkWhittington writes: The problem of lowering the cost of sending people and cargo into low Earth orbit has vexed engineers since the dawn of the space age. Currently, the only way to go into space is on top of multistage rockets which toss off pieces of themselves as they ascend higher into the heavens. The Conversation touted a British project, called Skylon, which many believe will help to address the problem of costly space travel. According to IEEE Spectrum, both BAE Systems and the British government have infused Skylon with $120 million in investment.

226 comments

  1. When I see "could" in a headline ... by Hognoxious · · Score: 2, Insightful

    When I see "could" in a headline, I add "but it probably won't/doesn't" to the end.

    I think fundamentally this is closely related to Betteridge's law.

    --
    Confucius say, "Find worm in apple - bad. Find half a worm - worse."
    1. Re:When I see "could" in a headline ... by turkeydance · · Score: 4, Funny

      "could" and "might" and "?" are standards in the click-bait tackle box.

    2. Re:When I see "could" in a headline ... by dinfinity · · Score: 1

      And quotation marks:

      Headline: "British spaceplane will revolutionize space travel"
      Intro: Some obviously biased guy somewhere said his spaceplane will revolutionize space travel.

      Translation: we're terrible 'journalists' who lack the competence, fortitude and integrity to come up with a headline we actually stand by. If not, we'd have written a headline like: British company developing spaceplane.

      We need more than Betteridge's law. We need Betteridge's law book.

    3. Re:When I see "could" in a headline ... by thinkwaitfast · · Score: 3, Insightful

      It could blow up and kill a lot of people. It could fail to make it to orbit and crash into NYC. It could make early investors billions. It could do a lot of things.

    4. Re:When I see "could" in a headline ... by LWATCDR · · Score: 1

      If anyone has studied the history of the UKs aviation and space industry will simply say I will believe it when I see it.
      The modified rule has versions for battery tech or mass storage tech. I will believe it when it ships.

      --
      See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
    5. Re:When I see "could" in a headline ... by Tough+Love · · Score: 1

      Actually, blowing up people in an experimental aircraft should be a crime worthy of jail time all up the line, given that we could be blowing up autonomous piloting gear instead.

      --
      When all you have is a hammer, every problem starts to look like a thumb.
    6. Re:When I see "could" in a headline ... by Dereck1701 · · Score: 4, Insightful

      I believe there is a quote from Arthur C Clark regarding this

      "Every revolutionary idea seems to evoke three stages of reaction. They may be summed up by the phrases: 1- It's completely impossible. 2- It's possible, but it's not worth doing. 3- I said it was a good idea all along."

      That's not to say that one should buy into every idea that someone is trying to peddle, but many of the technologies we take for granted today (aircraft, cars, PCs, engineered lumber, etc) were seen as prohibitively expensive, unnecessary and/or dead ends before they became widespread. Air breathing rocket engines of some sort are very likely to be the future of spaceflight, whether or not Skylon will be that future we will have to see.

    7. Re:When I see "could" in a headline ... by KGIII · · Score: 2

      In the scale of things, it wasn't all that odd for the computer that I had in my house, counting all the peripherals, was more costly than my new car in the driveway. I think my first laptop was about $10,000 and had an external tape drive (that had an internal 40 MB HDD IIRC and used proprietary tapes), had a docking station, had an external modem, and I think it had an internal 40 GB drive as well as the ability to use an external monitor.

      The PC on my desk was only slightly less expensive and I think that's because I'd opted to upgrade some of the boards - I'd a whopping 33 MHz as I recall. I'm not able to recall if that was the same laptop that also required an external power supply or not. This would have been sometime around 1990. I'd bought an extra docking station so that I had one at home and one at work. I think it must have been just a bit after 1990, actually? I could be conflating two of them in my head.

      My car was probably about $10,000 or so and likely new at the time. The laptop, with the docking stations and the extras was about that same price. The desktop was less but made the total value certainly higher than my car. At one point, you could even buy insurance for your computer. There were some colorful insurance claims at the time.

      I guess the point is that they probably were prohibitively expensive for some. It used to be that you'd dress in your Sunday finest to go on a plane. It was an event and damned expensive. So, yeah, they were prohibitively expensive - it wasn't just people saying that. It just ended up being less expensive as the number grew. They moved from things for the upper-middle class, to the middle-class, to the working poor, and now even poor people probably have at least one working computer. Well, poor people in my country.

      --
      "So long and thanks for all the fish."
    8. Re:When I see "could" in a headline ... by MobSwatter · · Score: 1

      Actually, blowing up people in an experimental aircraft should be a crime worthy of jail time all up the line, given that we could be blowing up autonomous piloting gear instead.

      No guts, no glory.

      That said...

      I think this craft has taken a wrong turn in power plant design, far too much weight burned in the heat exchangers that can be used for fuel and cargo. There has been nothing I have seen that could rival what modification that the J-58 Ramjet that the SR-71 was supposed to have before the program was cancelled prior to development of it being completed so it got the same thing the A-12 got. Jets have the efficiency in the atmosphere, rockets have it in zero G environment. A direct cross in my opinion between the two isn't where its at, the SR-71 intake changed shape to obtain volumetric stability, and is not the only part of a power plant that can. I admire the Skylon program doing this independently, not an easy task and should have government backing.

    9. Re:When I see "could" in a headline ... by Keith+Henson · · Score: 5, Interesting

      I have followed Skylon for several years now. The engines are very interesting, in fact, the whole design, including the wings is very cool. The wings take the gravity load off, which for something that takes that long to get to orbit is quite an advantage.

      They actually get more energy out of the hydrogen than they would get from just burning it. The reason is that they run the compressor on the temperature difference between ram air and the LH2 flowing to the engines. Burning hydrogen gives about 50 kWh/kg, it takes 20 kWh/kg to make it into a liquid.

      You might note that everyone who has been given the full inside information, including the USAF, agrees that it will work as a SSTO. If anyone wants to build power satellites, Skylon is the only thing that is likely to get the cost to where power satellites could undercut coal.

      --
      End MGM. Get prospective parents of boys to Google: Men do complain
    10. Re:When I see "could" in a headline ... by MobSwatter · · Score: 1

      I have followed Skylon for several years now. The engines are very interesting, in fact, the whole design, including the wings is very cool. The wings take the gravity load off, which for something that takes that long to get to orbit is quite an advantage.

      They actually get more energy out of the hydrogen than they would get from just burning it. The reason is that they run the compressor on the temperature difference between ram air and the LH2 flowing to the engines. Burning hydrogen gives about 50 kWh/kg, it takes 20 kWh/kg to make it into a liquid.

      You might note that everyone who has been given the full inside information, including the USAF, agrees that it will work as a SSTO. If anyone wants to build power satellites, Skylon is the only thing that is likely to get the cost to where power satellites could undercut coal.

      Yes, chilling mass to reduce it to gain additional thrust on burn. Yes I see that, I know it will work but I just don't like the cost in weight for the heat exchangers and just for mach 5 seems a heavy cost. USAF never saw inside OXCART but they did end up with the bird post '64. My grandfather did the funding for it, it was compartmentalized inside CIA SR, and CIA SR was my great uncle Jack's program and he had to cancel it in '64 over what happened to my grandfather as what happened was not clear to him and was considered a security breach. I could slap something together for aircraft style access to space as I inherited enough knowledge to do so but 20:1 the same jerks that screwed it up to begin with would do so again if I did it within their reach in the US.

    11. Re:When I see "could" in a headline ... by fuzzywig · · Score: 1

      The thing is, every idea goes through at least the first phase, and often the second as well. It's pretty hard to tell what's a good idea or not until phase three.

    12. Re:When I see "could" in a headline ... by dmgxmichael · · Score: 1

      It could blow up and kill a lot of people. It could fail to make it to orbit and crash into NYC. It could make early investors billions. It could do a lot of things.

      Could it exist?

    13. Re:When I see "could" in a headline ... by Anonymous Coward · · Score: 0

      Anybody got some ranch dressing for this word salad?

    14. Re:When I see "could" in a headline ... by werepants · · Score: 1

      You might note that everyone who has been given the full inside information, including the USAF, agrees that it will work as a SSTO.

      That's a worthwhile datapoint, but I imagine that there's lots of qualifiers on that. IF they can reach the specified performance from the engines, IF they can get the dry weight as low as their target, IF the thermal protection operates as intended it will work. Saying that you don't see any dealbreakers based on number crunching and design studies is a long way from knowing that none will come up later.

      That said, that big chunk of cash is a pretty resounding endorsement of the idea. Not sure how far that is expected to go, but if they can actually get some hardware built that will make them more successful than any other SSTO program in history.

    15. Re:When I see "could" in a headline ... by HornWumpus · · Score: 1

      Ranch dressing with a just a little lithium...

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    16. Re:When I see "could" in a headline ... by HornWumpus · · Score: 1

      It's like the oft repeated misquote from Ghandi. Anything that gets laughed at will inevitably win...or not.

      --
      John McAfee 'It was like that time I hired that Bangkok prostitute; to do my taxes, while I fucked my accountant'
    17. Re:When I see "could" in a headline ... by MobSwatter · · Score: 1

      Of course, anyone that was related to and with knowledge of the pinnacle of aerospace programs 50 years ago talking about it now days must be crazy. It's okay, go back to sleep and let the batch of closet case Nazi's, superstitious thieving pedophiles lead you all around playing world cop digging a deeper deficit. Your vote means something to them, sleep... Sleep...

    18. Re:When I see "could" in a headline ... by Keith+Henson · · Score: 2

      "and just for mach 5 seems a heavy cost'

      As important, Skylon is at 26 km, which is to say 96% or so of the atmosphere is below it. Also, you *start* with 150 untouched tons of LOX and enough hydrogen to burn all of it in about a 6 to one ratio. The 15 ton payload is only 5% of the 300 ton takeoff mass, but the design goal is to fly it every other day or perhaps every day with a low turn around cost. The heat exchangers are not that big a piece of the mass budget.

      To solve the carbon/energy problem in 7 or 8 years would take a construction rate of 400 five GW power sats a year. This takes around a million Skylon flights. That's a reasonable number considering that we get a million commercial aircraft flights in ten days.

      It's not even close to reasonable if you try to do it with rockets.

      --
      End MGM. Get prospective parents of boys to Google: Men do complain
    19. Re:When I see "could" in a headline ... by MobSwatter · · Score: 1

      You might note that everyone who has been given the full inside information, including the USAF, agrees that it will work as a SSTO.

      That's a worthwhile datapoint, but I imagine that there's lots of qualifiers on that. IF they can reach the specified performance from the engines, IF they can get the dry weight as low as their target, IF the thermal protection operates as intended it will work. Saying that you don't see any dealbreakers based on number crunching and design studies is a long way from knowing that none will come up later.

      That said, that big chunk of cash is a pretty resounding endorsement of the idea. Not sure how far that is expected to go, but if they can actually get some hardware built that will make them more successful than any other SSTO program in history.

      I think the trick in that really isn't possible now days. Powers that be pretty much everywhere no do not really have any interest in building anything fast enough without a destructive primary purpose. While defenses should be part of it, that should not be the only tool in the shed and certainly not the focus of developing the technology. They built something in the US that does Mach 10 which is plenty to breach the atmosphere and transition to rocket propulsion in a zero drag coefficient environment, but they only did it to carry a bomb. Meanwhile NASA is stuck primarily with rockets sending RC toys out there with the shuttle program being cancelled on a classified mission resulting in sending US astronauts to Russia to make it to orbit. If that isn't the short bus then I don't really know of a better example. In light of this and in retrospect, who actually won the space race? One trick pony programs to plant a flag does not equate to us being more 'advanced', just proves the public is willing to accept a hand job.

    20. Re:When I see "could" in a headline ... by Zaiff+Urgulbunger · · Score: 1

      When I see "could" in a headline, I add "but it probably won't/doesn't" to the end.

      Doubly so when it also has "British" in the there! (and I'm a Brit so I'm allow to be disparaging!)

    21. Re:When I see "could" in a headline ... by lucien86 · · Score: 1

      The UK has first world ambitions, third world funding..

      --
      Below the speed of light Special Relativity is one of the most accurate theories in physics - above the speed of light..
    22. Re:When I see "could" in a headline ... by TheTurtlesMoves · · Score: 1

      Wings have terrible LD coefficient at high speed (Subsonic you get 20 or even higher, at March 2 it is about 7 and goes down very fast from there to less than 1 at hypersonic speeds). And getting to orbit is about speed. 7800m/s of speed. Everything scales with v^2. Lift, drag, skin heating, kinetic energy and of course "orbital lift". The fastest aircraft ever was exceptionally expensive, the SR blackbird. It got a mere 1000m/s approximately. Or about 3% of orbital kinetic energy.

      Now even worse is you can't point design things like the SR blackbird, which was designed to sit at a optimal speed and altitude. Getting the intakes to work for that was really really hard. Getting something that need to work over an even larger range of speed in air is even harder. Drag coefficents of intakes can be massive in off design point conditions.

      Space ships are not aircraft. They don't solve the same problem. Beating the space plane dead horse will not get us to space cheaper.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
  2. Stupid article by BradMajors · · Score: 4, Interesting

    Skylon's idea is to use oxygen from the air, rather than taking the oxygen as fuel for the initial part of the ascent. A well known idea that is being worked on elsewhere.

    1. Re:Stupid article by Anonymous Coward · · Score: 0

      Skylon's idea is to use oxygen from the air, rather than taking the oxygen as fuel for the initial part of the ascent. A well known idea that is being worked on elsewhere.

      They have a plan.

    2. Re:Stupid article by cjameshuff · · Score: 0

      And one of limited real world value. LOX is dirt cheap, and launchers have to leave the atmosphere after a short amount of time in order to reach orbital velocity. They add on all sorts of complexity and losses to enable use of atmospheric oxygen. They are accepting increased vehicle and operational costs in order to reduce the tiny fraction of launch costs that come from the propellant. This simply isn't going to result in inexpensive spaceflight.

      Of course, the rest of the vehicle is a fantasy structure of a carbon fiber spaceframe with gigantic liquid hydrogen tanks on the inside and an eggshell-thin ceramic heat shield suspended around it on wires, with insulation and active cooling systems in between. It might be physically possible for a structure that fulfills their requirements to exist, but can it actually be manufactured, let alone maintained and flown? (And of course, if they do manage to work these things out, the same techniques will become available to conventional rockets, along with some things like partially pressure-supported tanks that aren't usable on Skylon due to the bending loads from its horizontal launch...)

      Air breathing engines are better suited for cruise than for acceleration to anything approaching orbital velocity, and with the need for LH2, it's probably not aimed at anything commercial...instead, things like hypersonic drone bombers. Skylon is just PR.

    3. Re:Stupid article by EdgePenguin · · Score: 5, Insightful

      If you think saving money on LOx is in any way the aim of Skylon, you have demonstrated your utter inability to grasp basic rocket science. Its about saving mass; and Skylon does a hell of a lot of that. So much so that (by the estimation of all the third parties who have looked at the design - including the UK government, ESA, DLR and recently the USAF) it can achieve SSTO operation. It takes off and lands like a plane, so no need to integrate it each time. That is an advance on even SpaceX - they have to manufacture a new second stage and attach it to the reusable first stage.

    4. Re:Stupid article by cjameshuff · · Score: 1

      They save mass that conventional rockets expend almost immediately in their flight, pay a big price in aerodynamic drag instead, and additionally pack on lots of extra mass in air breathing equipment and various HOTOL related structure that they then need to take to orbit. They compensate for that and for the efficiency losses of SSTO by claiming a structure and thermal protection system that are basically magic, and gloss over all the additional operational expenses. And no, they don't avoid the need for payload integration.

      SpaceX has the advantage of having a vehicle that actually exists, and they're not content to stop with first stage reuse. The successor to the Falcon 9 will be fully reusable, and far simpler and cheaper to develop, not to mention actually operate.

    5. Re:Stupid article by EdgePenguin · · Score: 3, Insightful

      So let me get this straight; you think you have spotted a major flaw in their design that was not spotted by various governments, space agencies and aerospace companies that have thoroughly analysed this project? Have you done the sums and found that the precoolers have more mass than the oxygen saved? Have you worked out the losses due to drag?

      I was talking about integrating stages, not payload. SpaceX still have to and always will have to do that. The TPS isn't magic either They are already talking to manufacturers about how to build it. Most importantly though is due to the aerodynamics of the vehicle it will have a much milder re-entry than the Space Shuttle, only needing the same kind of thermal protection it has in certain critical areas.

      And no, SpaceX does not have a reusable vehicle that actually exists. They haven't yet recovered a first stage, never mind reflown one.

      Please, could people actually investigate this project, its history and the major players who have invested in it before dismissing it out of hand based on intuition?

    6. Re:Stupid article by Rei · · Score: 2

      Skylon is reusable? So was the shuttle. Skylon saves propellant? Propellant is cheap. Reusable and low propellant consumption are not the key factors - maintenance costs are. And how Skylon will fare in that regard is very much an unknown at this point.

      Part of the problem with building these sorts of reusables is that they're such low volume that you never achieve economies of scales or significant stocks of parts, and have a lot more trouble refining the design with time. SpaceX's approach where the rockets are designed to be reusable but are still an affordable option as a disposal - and starting with the disposable route - works around this problem. They produce them in bulk while progressively refining the reusable aspects.

      That doesn't mean that SABRE/Skylon (which, by the way, is quite an old concept) shouldn't be pursued. It could be a quite useful concept. But it's really not answering the key question. That said, one nice thing about Skylon: being basically a giant hydrogen tank, it has a very low mass/surface area ratio when empty - namely because it has such a big bloated volume due to hydrogen's low density. This gives it a big advantage against craft like the shuttle on reentry - the energy you have to lose is proportional to your mass but the amount of surface you have to lose it from is proportional to your surface area. A reentering Skylon is a whole lot of... well, nothing. Just a big hollow shell for the most part.

      --
      The yellowcake is a lie.
    7. Re:Stupid article by EdgePenguin · · Score: 4, Insightful

      Once more, saving 250t of liquid oxygen is absolutely nothing to do with cost! Its to do with reducing the take off mass - which is what enables the performance required for SSTO.

      Oh, and the Space Shuttle wasn't reusable, it was rebuildable.

    8. Re:Stupid article by thinkwaitfast · · Score: 2
      There is a drawback in using atmospheric oxygen. The vehicle must stay low enough to have something to scoop up. Exactly how low is a messy calculus problem and also requires different structures and heat dissipation techniques.

      The two extremes are 1. shoot straight up out of the atmosphere, then straight tangential to the local surface (horizontal) and 2. Stay at sea level until you achieve orbital velocity, then head straight up. The space shuttle accent is closer to (1), popping out of the atmosphere then diving down toward Earth to pick up the horizontal component. And remember, every second you are not in orbit, you have to expend fuel to keep yourself off the ground. SpaceX did this analysis and concluded that while it was interesting and has merit that their current solution was better. Musk also said they might to back to revisit the problem in the future, but that it is a close trade off.

    9. Re:Stupid article by Tough+Love · · Score: 1

      Skylon's idea is to use oxygen from the air, rather than taking the oxygen as fuel for the initial part of the ascent.

      Skylon's stupidity is to insist on combining a jet and rocket motor, whereas the jet could be attached to a separate vehicle, flown back independently. Just leave the LN gear in the atmosphere, please.

      --
      When all you have is a hammer, every problem starts to look like a thumb.
    10. Re:Stupid article by Tough+Love · · Score: 1

      Whoops, I meant liquid helium gear, even worse. Think of all the party balloons that could be harmed.

      --
      When all you have is a hammer, every problem starts to look like a thumb.
    11. Re:Stupid article by Burdell · · Score: 1

      Welcome to the 1970 or so plan for the Space Shuttle. A flyback booster was in the original concept, but it didn't pan out. Now, materials engineering and manufacturing processes have improved dramatically since then, so maybe something is feasible today, but I have my doubts.

    12. Re:Stupid article by Dereck1701 · · Score: 1

      Oxygen is only a small part of the possible advantage of an air breathing rocket engine. Reaction mass is a much larger advantage. Standard rocket engines have to carry all of their reaction mass. Jets carry only their energy source (fuel) and use the atmosphere and external oxygen as an additional reaction mass. I believe a 747 for example sucks in and expels over 5,000 lbs of air a second. That is why jet engines have such a major advantage over rocket engines in terms of Isp (specific impulse: IE fuel efficiency), while a rocket engine has an Isp of around 300-400 jet engines routinely have Isps of 4k-6k. Its not a perfect situation by any means, jet engines have significantly more drag due to the action of having to consume atmosphere but up to about mach 5 they are 3 times or more efficient than rocket engines.

    13. Re:Stupid article by Panoptes · · Score: 3, Funny

      "They have a plan"

      Even better - they have a cunning plan.

    14. Re:Stupid article by Anonymous Coward · · Score: 0

      That is an advance on even SpaceX - they have to manufacture a new second stage and attach it to the reusable first stage.

      SpaceX has to recover a first stage in order for that scenario to work. Something they have yet to do. *Cough* *Cough*

    15. Re:Stupid article by Keith+Henson · · Score: 1

      Edge, you have done your homework.

      I think it would be fun to talk. I am not hard to find. Or you can sign on to the google group power satellite economics where I hang out.

      --
      End MGM. Get prospective parents of boys to Google: Men do complain
    16. Re:Stupid article by dbIII · · Score: 1

      LOX is dirt cheap

      Carrying it around isn't.
      That's why motor vehicles run on fuel that burns in air instead of a self-contained explosive despite such a thing being available in the late 19th century.

      There is plenty on the net about using air when it is available and other things when it is not. Single stage to orbit sounds "simple" but requires moving a lot of leftover mass so why not use the best tool for the job in different conditions instead of a compromise? I don't know about this thing but the scramjet is very promising under some conditions.

    17. Re:Stupid article by Keith+Henson · · Score: 1

      " Exactly how low is a messy calculus problem"

      I have spent a lot of time with the spreadsheets that define a Skylon atmospheric ascent. It's not complicated at all. What they do is fly up the constant pressure line. By the time they switch to rocket mode, they are above atmosphere thick enough to cause Qmax problems. Forces on the vehicle are really mild.

      --
      End MGM. Get prospective parents of boys to Google: Men do complain
    18. Re:Stupid article by khallow · · Score: 1

      Oh, and the Space Shuttle wasn't reusable, it was rebuildable.

      By that sense, so is any airplane. They still need to be inspected after a flight, and parts repaired and replaced on a continuing basis. I would say instead that it is a vastly lower quality of reusability with much higher cost and turn around time between flights than a normal airplane.

      As to Skylon, I hear that even with air breathing engines, it requires a very efficient mass fraction better than any current rocket stage (with the stage filled with low density LH2).

    19. Re:Stupid article by slew · · Score: 1

      Please, could people actually investigate this project, its history and the major players who have invested in it before dismissing it out of hand based on intuition?

      Funded by the UK govt is all you need to know about them... ;^(

      Of course the "visionary" behind this is Alan Bond whose major claim to fame is Project Daedalus. I think that was some sort of contest winner (on par with Mars One)...

      His previous actual efforts was HOTOL and that was canned by the UK govt before it got off the drawing board... Skylon is basically HOTOL-3 (HOTOL-2 was proposed, but it didn't even get past the proposal stage)...

      Okay, my 2cent internet investigation is complete. Your turn...

    20. Re:Stupid article by Anonymous Coward · · Score: 0

      More precisely, it's to do with decreasing the size of the expensive first-stage engines, which depend on the take-off mass. And decreasing them enough that they can be carried for the entire flight, and re-used.

    21. Re:Stupid article by Anonymous Coward · · Score: 0

      Why don't they simply build some sort of supersized SR-71/Mig31 in order to carry a solid fuel rocket to 25kms height. And in order to speed the thing to Mach 3. Then let the solid fuel rocket go and accelerate it to satellite speed and get into orbit.

      Land the Super-Mig31-SR71 and reuse for next launch...

    22. Re:Stupid article by Anonymous Coward · · Score: 0

      Why did they not go the parachute/airbag route ?

    23. Re:Stupid article by Anonymous Coward · · Score: 0

      Use on of these babies to breathe as much air to lift a satellite into space:

      https://de.wikipedia.org/wiki/Tupolew_Tu-144
      https://de.wikipedia.org/wiki/Lockheed_SR-71
      https://de.wikipedia.org/wiki/Mikojan-Gurewitsch_MiG-31
      https://de.wikipedia.org/wiki/Concorde
      https://de.wikipedia.org/wiki/Tupolew_Tu-160

      For the final acceleration phase, use a Trident-style solid booster to lift the sat into space. Of course these aircraft would need to be scaled up to accommodate large satellites. Especially the Tu160 with almost 100t payload looks very attractive...

    24. Re:Stupid article by Maritz · · Score: 1

      So let me get this straight; you think you have spotted a major flaw in their design that was not spotted by various governments, space agencies and aerospace companies that have thoroughly analysed this project?

      Of course he does, this is Slashdot. Most of the blowhard armchair experts on here would look at that article and genuinely think they have some insight to offer that would steer the people working on this project better or get them to chuck it in. Simple arrogance of ignorance at work.

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    25. Re:Stupid article by tsotha · · Score: 1

      Horizontal takeoff makes this quite a bit cheaper, though, from an engineering perspective. The TWR you need at takeoff is much lower - a 747 has something like a 0.27 TWR, which wouldn't even budge a rocket. Lower TWR means smaller engines, less weight, less drag. It also means less stress on the spacecraft, too, which should keep the wear and tear a bit lower. The plan is to go up to 28 km at mach 5.5 before cutting over to LOX. Assuming they can actually get the performance they expect out of the engines, and keep the dry mass to what they expect, this is a doable flight profile.

    26. Re:Stupid article by Maritz · · Score: 1

      Stay at sea level until you achieve orbital velocity, then head straight up.

      Hitting about 8km/s at sea level sounds hazardous to health.

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    27. Re:Stupid article by Maritz · · Score: 1

      Yeah, they're stupid and you're smart, I get it. If only they'd approached you beforehand you could've saved them millions.

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    28. Re:Stupid article by tsotha · · Score: 1

      It's only stupid if they can't pull it off. Having a single engine that can do both is an enormous advantage. Hell, even designing a carrier aircraft to launch non-trivial payloads is an enormous headache. As far as I'm aware, there's one production system that uses an air launch, and its payload to LEO is about half a ton. That's 1/30th the payload REL is planning for Skylon.

    29. Re:Stupid article by Anonymous Coward · · Score: 0

      Obsession with GLOW is a aircraft thing. It has no place in Rocket Science. In fact just going for a larger GLOW and a lower Dry weight is cheaper since the dry weight is what you pay for. *not* GLOW. LOX is litterley cents per liter. I got a quote for 10 metric tons of LOX + truck rental for 2 days at $1000NZD. Most of that was the truck rental.

      Boats don't look like cars or trains. Planes don't look like trains or cars. Why the fuck do we insist that space ships should look like planes or work like places. It is trying to solve a completely different problem. And the one space craft that did operate like a plane was a total disaster both from a safety standpoint and economically.

    30. Re:Stupid article by Anonymous Coward · · Score: 0

      Mach 3, or about 1000m/s is less than 2% of required orbital kinetic energy. Oh and now you have to spend a lot of time in the atmosphere at mach 3 or higher.. yea that will be cheap. NOT.

    31. Re:Stupid article by Anonymous Coward · · Score: 0

      Scale up a U-2 in order to lift a two-stage rocket into this height. So at least the big first stage would be reusable.

    32. Re:Stupid article by Anonymous Coward · · Score: 0

      Because the stresses from that (considering a "land"-landing) crush the stage, which is for all there is mostly a long, very thin-walled can of Aluminum...
      and if you consider a water landing, now it crushes the stage AND gets everything salt-watery-wet, destroying it...

      (TL;DR of all the stuff said about that topic)

    33. Re:Stupid article by SpinyManiac · · Score: 1

      Not an SR-71, a Tu-160. Specifically the TU-160SK / Burlak combo, which was actually studied by the Germans.
      First stage ignition at mach 1.7 and 13500 metres altitude to get a 1100kg payload into a 100km orbit.

      The plane was considered to be the zeroth stage.

      --
      It's never too late to have a happy childhood.
    34. Re:Stupid article by Alioth · · Score: 1

      They aren't trying to save money on not needing as much LOX, the aim of taking a whole lot less LOX is that this can translate into increased payload and decreased vehicle weight.

    35. Re:Stupid article by Alioth · · Score: 2

      No, not at all. The Space Shuttle had to be substantially overhauled after *every single flight*. Airplanes don't. EasyJet for instance turns around a flight in under 30 minutes, which simply wouldn't be possible if it required more than a visual walk around by the crew between flights. I own an aircraft, and typically we only have to take things apart twice a year (and this is for an antique aircraft, too).

      The Space Shuttle was not like this at all. It needed a full engine overhaul after every flight. The turbines on modern widebody twin engine aircraft will go thousands of cycles and tens of thousands of hours before requiring an overhaul - not a single cycle and single flight like the Shuttle.

    36. Re: Stupid article by O('_')O_Bush · · Score: 2

      Drag is a function of velocity. Rockets have to go fast in the atmosphere to build V to keep from wasting fuel fighting gravity. Skylon doesn't have to fight gravity the same way (it uses the atmosphere to fight gravity for it) and therefore doesn't have high drag by needing to punch straight through the atmosphere as fast as possible and where drag is the highest .

      Your thinking is akin to two grave diggers. One uses a shovel to cut the earth and remove dirt (Skylon) making it an easy job to reach 6', while you are trying to suggest that is worse or equivalent to someone trying to dig a grave out of holes from someone pushing a 6' pole into the ground repeatedly.

      --
      while(1) attack(People.Sandy);
    37. Re:Stupid article by Tyrannicsupremacy · · Score: 1

      I play Kerbal Space program so I can visualize exactly what that orbit profile looks like. But it'd be more apt to say the space shuttle is diving down to the backside of earth.

      --
      http://i.cubeupload.com/T6cyLu.png
    38. Re:Stupid article by dotancohen · · Score: 1

      Oh, and the Space Shuttle wasn't reusable, it was rebuildable.

      This is the best way of describing STS that I've ever seen. Not STS as it was designed, but rather STS as it was in practice.

      And that was part of the problem: the orbiters were not designed to be disassembled as had to be done.

      --
      It is dangerous to be right when the government is wrong.
    39. Re:Stupid article by Rei · · Score: 1

      Tankage mass is not generally that expensive, so reducing your tankage by reducing your propellant is not the huge money-saver you're envisioning. It's your engines and particularly all of the components that drive them that make rockets expensive. And Skylon involves totally new, rather complex engines that run in two different operating modes.

      And really, you think Skylon engines wouldn't have to be taken apart, examined, and refurbished just like the shuttle engines? Like jet engines?

      --
      The yellowcake is a lie.
    40. Re:Stupid article by Rei · · Score: 1

      Airplanes used to be terribly unreliable as well. The first cross-country "flight" in the US involved several dozen crashes. Mass production combined with the extensive design experimentation and process refinement that it enabled allowed airplanes to become the reliable, relatively quick turnaround vehicles that they are today (note: while a typical turnaround may be 30 minutes, they still have to be taken out of service regularly for more expenensive go-overs). How do you plan to get this sort of mass production-enabled experimentaiton and process refinement with Skylon? The Shuttle could likewise have been refined to reduce maintenance.... but the vehicle wasn't in the sort of production/design environment that jets are in that enables such refinement.

      --
      The yellowcake is a lie.
    41. Re:Stupid article by khallow · · Score: 1

      The Space Shuttle had to be substantially overhauled after *every single flight*. Airplanes don't.

      You are only arguing a matter of degree.

      typically we only have to take things apart twice a year

      Indeed.

      The Space Shuttle was not like this at all. It needed a full engine overhaul after every flight. The turbines on modern widebody twin engine aircraft will go thousands of cycles and tens of thousands of hours before requiring an overhaul - not a single cycle and single flight like the Shuttle.

      A flight of the Shuttle is typically 250-400 hours which is a much more significant cycle. That's about two orders of magnitude shorter in duration.

    42. Re:Stupid article by aaarrrgggh · · Score: 1

      I doubt Musk's analysis is based simply on the physics of the problem; a large part of the equation is development cost/time, and risk.

      Horizontal take-off is a great strategy... if it can be made to work. I think the Virgin Galactic approach is more interesting though.

    43. Re:Stupid article by khallow · · Score: 1

      How do you plan to get this sort of mass production-enabled experimentaiton and process refinement with Skylon?

      High launch frequency.

      The Shuttle could likewise have been refined to reduce maintenance.... but the vehicle wasn't in the sort of production/design environment that jets are in that enables such refinement.

      That's due to poor strategic direction and design decisions. For example, they could have gone with a two person RLV on the Saturn IB. Then they could have afforded the high launch frequency that one needs to enable and justify those things.

    44. Re:Stupid article by Anonymous Coward · · Score: 0

      'Never argue with stupid people, they will drag you down to their level and then beat you with experience.' — Mark Twain

    45. Re:Stupid article by TheRaven64 · · Score: 1

      To be fair to the space shuttle, it went a really high number of miles between services!

      --
      I am TheRaven on Soylent News
    46. Re:Stupid article by Chris+Mattern · · Score: 2

      Skylon saves propellant? Propellant is cheap.

      On the contrary, propellant is damn expensive. Its mass winds up being most of the mass of the rocket, which you then have to lift.

    47. Re:Stupid article by Chris+Mattern · · Score: 1

      Tankage mass is not generally that expensive

      The engines you'll have to build to lift that mass are another matter.

    48. Re:Stupid article by Anonymous Coward · · Score: 0

      I don't think Pegasus is going to be the only air launched orbital payload rocket for long, Scaled Composites is building a massive aircraft right now for Stratolaunch systems/Vulcan Aerospace. Should be possible of putting somewhere north of 10,000 lbs into orbit.

    49. Re:Stupid article by jabuzz · · Score: 1

      The air liquification stage has been tested in full prototype and passed all test by independent external observers. I believe this included the European Space Agency and the USAF.

      That is using liquid hydrogen to liquefy air in a fraction of a second to be feed into the rocket engine in sufficient quantities for it to be useful. The £120 million that has been announced is to build a full functional prototype Sabre engine. That is a pretty modest sum of money for "rocket" engine that would make all other space launch systems obsolete overnight. Even SpaceX's reusable rockets which they have still to land one would be dead in the water.

    50. Re:Stupid article by Anonymous Coward · · Score: 0

      you have demonstrated your utter inability to grasp basic rocket science.

      Hey, cut the guy some slack, maybe he's just a brain surgeon!

    51. Re:Stupid article by Rei · · Score: 1

      High launch frequency != mass production and continued refining between releases. It doesn't matter how often you launch if you only have a couple vehicles. Airplaines would simply be nothing like the refined vehicles that they are today if there were only five of them out there - no matter how often they flew.

      --
      The yellowcake is a lie.
    52. Re:Stupid article by Anonymous Coward · · Score: 0

      It's not a jet and a rocket, it's a rocket. The turbines provide no thrust, they just provide the highly compressed air for combustion. In terms of propulsion, there is no "switching modes". As the craft goes higher, it takes more energy to compress enough air to feed the combustion, and LOX is added to supplement. At some point, the compression process is a net loss (it takes more energy to compress the air than what is saved by not carrying the extra LOX). At this point, the intake closes, the air compressor shuts down, and the craft continues to orbit on internal oxidizer. During the whole cycle, the actual propulsion is pure rocket.

    53. Re:Stupid article by Rei · · Score: 2

      Skylon's payload is comparable to that of the Falcon 9 V.1.1, but its engines are nonetheless still 70% the thrust of Falcon 9 V1.1 first stage. And a LOT more complex.

      There's a number of other problematic things about Skylon. One is the very HTOL design itself. Rockets (including skylon) are cylinders under some degree of pressure - that's the natural shape for them due to wind resistance. This is a very strong design against loads along its length, not so much for loads applied by stubby wings in the middle. VTOL keeps the loads vertical the whole time, which is a big structural mass savings (it also allows for the use of landing struts rather than landing gear, which are lighter and simpler, and much smaller highly reinforced concrete pads - Skylon requires a whole highly-reinforced runway). VTHL is the next best - you still have to be able to bear lateral loads, but on landing your craft is a tiny fraction of its launch mass, so the lateral loads are a tiny fraction of what they would be with horizontal takeoff. But Skylon is HTOL - it must bear its whole loaded mass at takeoff. It has a takeoff weight like a jumbo jet, yet they want it to have an empty weight a tiny fraction of an unfurnished jumbo jet - yet have far more complicated, powerful engines, to be spaceworthy, to be hauling cryogenic propellants, etc. It's a tall order. Jumbo jets have such high empty weights in large party to withstand their takeoff loads.

      Takeoff is even worse that cruise at full mass, as there's higher pressure, and you have so much force concentrated on the tiny points of your landing gear. It's so much of an issue that some HTOL designs have even tried to work around it by having the craft empty on takeoff and be fueled midair (see "Black Horse" as an example). Some extant systems do this indirectly, for example Pegasus, by employing an airplane to get them off the ground. The airplane doesn't give the rocket much altitude or delta-V, so it's not immediately obvious what advantages it gives that justify the added expense and complexity, but it's a whole host of small side benefits: great flexibility of launch locations, ease of transportation of the rocket, allowing the first rocket stage to be optimized for thinner air, and yes, avoiding the mass penalty of having to withstand the forces of takeoff. The plane has to do that, not the rocket. Other variants that have been investigated have been tow-launch with midair refueling and launch out the back of a cargo plane.

      --
      The yellowcake is a lie.
    54. Re:Stupid article by Anonymous Coward · · Score: 0

      LOX is ATF controlled in the USA. Not that it's that hard to make in small quantities.

      A fellow could have a LOT of fun with 10 metric tons of LOX and a big old bonfire.

      Why do you think nobody has yet brought a truckload of LOX to Burningman? Don't answer 'sanity'.

      Did you see the charcoal grill and thermos full of LOX video on youtube?

    55. Re:Stupid article by erice · · Score: 1

      To be fair to the space shuttle, it went a really high number of miles between services!

      Yes, but for the vast majority of those miles, the main engines are off. The engines only fire during launch. The airframe is stressed during launch and decent. All those miles racked up in the middle orbiting the Earth? They don't count much. A little bit of thrusting from the OMS. Maybe a scratch of micrometeors against the shell. Might as well be sitting in a hanger.

    56. Re:Stupid article by Keith+Henson · · Score: 2

      Thanks for the compliment, AC. Perhaps I can do the same for you some day.

      But let's analyze the case (if any) for power satellites. Electricity is a commodity; like all commodities you have to be competitive on price if you want a significant market share. That means you want to undercut electricity from coal at around 4 cents per kWh. If you set 75% of coal (3 cents per kWh) as the target, then you can back calculate how much you can spend for a levelized cost of electricity of three cents. For generally accepted life and discount rates that's about $2400/kW.

      The mass for ground based solar power is around 500 kg/kW. This article, http://spacejournal.ohio.edu/i..., make a case for 6.5 kg/kW. Not having to support the collectors against gravity and wind, plus the near 24 hr sunlight cuts the mass to about 1%. Parts and the rectenna are currently estimated at around $1100/kW, leaving $1300/kW for transport cost. If we can't get the mass lower than 6.5 kg/kW, then the cost of lifting the power sats to GEO can't exceed $200/kg. At high flight rates, Reaction Engines thinks the cost will get to $120/kg. Electric propulsion from GEO to LEO powered by 25 GHz microwave beams in the hundreds of MW, looks like it will cost under $80/kg.

      This article goes into the transport cost analysis. http://ieeexplore.ieee.org/xpl...

      It was peer reviewed.

      If you don't have easy library access, there is a preprint here:

      https://drive.google.com/file/...

      AC, if you would like to be anything but a blowhard, go through the documents and see if you can find fault with them.

      --
      End MGM. Get prospective parents of boys to Google: Men do complain
    57. Re:Stupid article by Keith+Henson · · Score: 1

      If someone is using them to build power satellites, the fleet size is in the thousands. And they only fly perhaps a 1000 times before they have to be replaced.

      --
      End MGM. Get prospective parents of boys to Google: Men do complain
    58. Re:Stupid article by slew · · Score: 1

      The air liquification stage has been tested in full prototype and passed all test by independent external observers. I believe this included the European Space Agency and the USAF.

      Perhaps I am mistaken, but my understanding is that the pre-cooler air is *not quite* liquefied in SABRE. I have not been able to confirm an observer test (not even a press release from REL's website), but merely, the ESA and AFRL (us airforce research labs) confirming the feasibility of the SABRE engine cycle concept as in no theoretical problems exist for engine. The observer test referenced in the wikipedia and other places doesn't seem to be a valid link (not even a press release from the reaction engine's website), but other sources seem to suggest the ESA observed a test back in 2012 in an experimental rig (not a full prototype).

      That is using liquid hydrogen to liquefy air in a fraction of a second to be feed into the rocket engine in sufficient quantities for it to be useful.

      AFAIK, the liquid hydrogen is simply used as a heat sink in the pre-cooler (helium-cycle) heat exchanger. The final compression to liquid is done with a relatively standard turbo compressor.

      The £120 million that has been announced is to build a full functional prototype Sabre engine. That is a pretty modest sum of money for "rocket" engine that would make all other space launch systems obsolete overnight. Even SpaceX's reusable rockets which they have still to land one would be dead in the water.

      I think the $120M (not £120M, actually a £60M research grant from UK govt) is for a sub-scale prototype. It will of course take much more money to make a full scale model (Reaction estimates £250M) and probably much more for bigger one that would be required for heavy-lift capability (like SpaceX).

    59. Re:Stupid article by Rei · · Score: 1

      You're envisioning the world launching many tens of millions of tonnes of payload into orbit any time soon? Yeah, good luck with that dream.

      --
      The yellowcake is a lie.
    60. Re:Stupid article by EdgePenguin · · Score: 1

      "Tankage mass is not generally that expensive"? FFS. Learn the rocket equation before commenting on launch systems, please.

    61. Re:Stupid article by lucien86 · · Score: 1

      If Skylon was a US project it would (probably) be flying by now.. Sadly...
        Actually Lockheed have a pretty close (~70%) to finished 2nd gen Space Shuttle ready to go - if only someone was willing to fund it..
      Well if Skylon was a Space X project it would (probably) be flying by now...

      --
      Below the speed of light Special Relativity is one of the most accurate theories in physics - above the speed of light..
    62. Re:Stupid article by Anonymous Coward · · Score: 0

      The Space X second stage is an altitude optimized single motor version of the F9 motor in the first stage which will also be reusable in time once the more commercially valuable first stage recovery systems are developed.What Skylon is developing is feasible but commercially not in contention with Space X... It will require many billions more investment in Skylon to get to where space X is NOW. Don't compare existing hardware with proposed, what Skylon offers to its strengths is adaptability and reaction times. Space X is designed for commercial applications as they exist TODAY, Skylon is for the future as we hope it to be, not as it exists now... I like the Skylon idea, but must also acknowledge its a long way from being better then Space X. Put it this way, if Space X fails, Skylon becomes less attractive as an investment to the general market since its seen as a risky and undeveloped technology. Once they build, test and operate full scale propulsion systems we'll be able to evaluate its viability relative to Space X.

    63. Re:Stupid article by TheTurtlesMoves · · Score: 1

      It has passed a test on the ground. At 0 speed. This is a far cry from getting it to work from march 2-6+ with respectable air intake drag. In fact i doubt 100M will be enough to even build just that part and not close to fly it. See both the concord and the SR Blackbird. And they had if far easier than Skylon. And were as expensive as shit to develop.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
    64. Re: Stupid article by TheTurtlesMoves · · Score: 1

      Getting efficient lift at below march 1 is easy. From march 2 to higher than 6 not so much. And even at mach 6 your still only 6% of the way there. And to "save" that you have exchanged cheap fuel tanks and fuel for a very expensive and very difficult to develop supersonic craft. Air intakes along for those speeds are extremely difficult to design without very high drag.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
    65. Re:Stupid article by TheTurtlesMoves · · Score: 1

      I would expect there to be rules to follow for such a truck. What they i couldn't say. But i doubt burning man would be compliant. Also LOX without something to burn is not as much fun as you my think.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
    66. Re:Stupid article by TheTurtlesMoves · · Score: 1

      No it really isn't that expensive. It is about 1% or less of launch costs. Fuel tanks are cheap and the weight is not that expensive to deal with. This is not an aircraft. Cost don't scale like aircraft, unless you insist on using aircraft for space ships. Cost don't scale with GLOW, they scale with Dry weight.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
    67. Re:Stupid article by TheTurtlesMoves · · Score: 1

      TWR of air breathers is on the order of 10 compared to rocket engines in the 50-200 range. So sure you have less max thrust requirements, but your engines+intakes are heaver than the equivalent rocket anyway. Not to mention the very very difficult problem of getting a supersonic craft with a miraculous flight envelope to work without totally shit performance. It cost a fortune for a optimized point design for both the concord and the blackbird. And they are really slow compared to what this needs.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
    68. Re:Stupid article by Rei · · Score: 1

      The rocket equation is not cost. Cost is cost. Proposing an expensive system to reduce fuel and tankage mass is not a money-saving concept. They get some reduction in the required launch thrust, not not incredibly, and at the cost of far more complex engines.

      --
      The yellowcake is a lie.
  3. Only $240M? by gman003 · · Score: 1

    Only $240M in funding? Last I checked, REL had specced the program as costing $12,000M.

    This isn't even the first time they've gotten funding. They've gotten about $450M in several previous rounds. Did they pass some milestone to earn more funding or did they just get paid for the sake of not canceling the project? As far as I can tell the only component that's been tested is the intake air precooler.

    1. Re:Only $240M? by EdgePenguin · · Score: 1

      They have specced billions to get to a flying spacecraft that is ready to be sold to vendors. The money they have got gets them to their next step; a ground test of a full engine. At that point they will be able to unlock more funding as the risk will have gone down. This method has got them this far; they secured funding from BAE and the UK government by demonstrating that the key enabling technology - the precooler - works.

  4. So where's their spaceplane? by tlambert · · Score: 1

    SpaceX started in 2002; Reaction Engines Ltd started in 1989; SpaceX reached the ISS in 1012. Looks like Reaction Engines Ltd is 21 years behind, unless you count only their Skylon project, in which case it's almost 2 years behind.

    Sorry. I'm massively unimpressed. Build something, already.

    1. Re:So where's their spaceplane? by viperidaenz · · Score: 2

      LOX fueled rocket engines have been flying since 1926.

      You're comparing "Tweak existing technology" with "Invent new technology"

    2. Re:So where's their spaceplane? by Anonymous Coward · · Score: 0

      Sorry. I'm massively unimpressed. Build something, already.

      Agreed, Skylon has been mentioned seven times on Slashdot since 2009 and still don't really have anything to show for it.

    3. Re:So where's their spaceplane? by ClickOnThis · · Score: 2

      SpaceX reached the ISS in 1012.

      Whoa, has Elon built a time machine?

      --
      If it weren't for deadlines, nothing would be late.
    4. Re:So where's their spaceplane? by Anonymous Coward · · Score: 3, Funny

      SpaceX started in 2002; Reaction Engines Ltd started in 1989; SpaceX reached the ISS in 1012. Looks like Reaction Engines Ltd is 21 years behind

      You're forgetting that in 2024 Reaction Engines will steal SpaceX's time machine and use it to reach the ISS in 997 AD, beating SpaceX by 15 years. That will have, of course, triggered the time race between the two companies, which will have resulted in both going further and further back in time until they accidentally cause a mass extinction on Earth 66 million years ago.

    5. Re:So where's their spaceplane? by EdgePenguin · · Score: 5, Insightful

      SpaceX started with a lot of money behind it, the support of NASA, and they are doing something very conventional (multi-stage LOx-Kerosene rockets) albeit better than the competition. Reaction engines are aiming at what they claim (with good reason) to be the biggest advance in propulsion since the jet engine. Snarky crap on slashdot is quick enough to write; R&D takes a long time.

    6. Re:So where's their spaceplane? by EdgePenguin · · Score: 5, Insightful

      They have built something. A precooler that can cool incoming air from 1000C to -150C as it comes into an engine intake at Mach 5, and is light and small enough to fit into an aircraft engine. This is the main part of the vehicle that is a big unknown, and they have shown it works in view of experts from government and industry.

    7. Re:So where's their spaceplane? by meerling · · Score: 1

      If it's just the lawyers, marketing weasels, and lazy reporters that go extinct, I don't think anyone will worry. ;)

    8. Re:So where's their spaceplane? by phayes · · Score: 1

      So where is the flight hardware?

      The flying prototype?

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    9. Re:So where's their spaceplane? by quintessencesluglord · · Score: 4, Interesting

      If I remember correctly, Reaction Engines got severely dicked by the UK government (pulling funding declaring the engines covered by the Official Secrets Act), effectively ending private development.

      The design was promising but had teething issues, and has been carried on as a garage project all these years.

      That they've managed to get this far given the hurdles they've had to overcome is nothing short of astounding.

    10. Re:So where's their spaceplane? by solartear · · Score: 1

      Sorry. I'm massively unimpressed. Build something, already.

      Agreed, Skylon has been mentioned seven times on Slashdot since 2009 and still don't really have anything to show for it.

      They built and tested the precooler 3 years ago. It worked. It was technology the USA gave up on several decades ago as impractical if not impossible. Just like oxygen-rich pre-burners, until the Russians showed them the USSR was using them for decades.

      They have also been doing rocket engine tests and releasing some of the findings. Big improvements with a better nozzle type they tested.

    11. Re:So where's their spaceplane? by dbIII · · Score: 1

      SpaceX reached the ISS in 1012

      Yes but they had to loop around the sun to do it :)
      More seriously SpaceX is doing mostly what Grumman etc were doing earlier instead of something very different and they have more people as well as better funding than Reaction Engines.

    12. Re:So where's their spaceplane? by Barsteward · · Score: 1

      you can watch this if you like to see a test engine running and an explanation of the task https://www.youtube.com/watch?...

      --
      "The hands that help are better far than lips that pray." - Robert Ingersoll (1833-1899)
    13. Re:So where's their spaceplane? by Maritz · · Score: 1

      Pretty different things, shouldn't really have to explain how different and to what extent. It should be really fucking obvious.

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    14. Re:So where's their spaceplane? by tsotha · · Score: 2

      If I remember correctly, Reaction Engines got severely dicked by the UK government (pulling funding declaring the engines covered by the Official Secrets Act), effectively ending private development.

      That's a BAE/Rolls Royce project called HOTOL, which was co-created by the same designer. After HOTOL was canceled he started REL.

    15. Re:So where's their spaceplane? by Maritz · · Score: 2

      So where is the flight hardware?

      The flying prototype?

      Parent is replying to a post that said they haven't made anything. "so where is the flight hardware" is a nonsensical response to that post.

      They haven't finished it yet, so it's a waste of time - is that your argument?

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    16. Re:So where's their spaceplane? by phayes · · Score: 1

      tlambert ridiculed the fact that RE is still in the lab/prototype phase after 25 years (note that he never claimed that RE has not built anything, just that their progress in 25 years is massively unimpressive).

      EdgePenguin claimed that having tested a precooler in a lab is some kind of achievement.

      I ask where the flight hardware &/or where the flying prototype is.

      You falsely claim that "Parent is replying to a post that said they haven't made anything" & then misrepresent "no flight hardware" (in 25 years...) as being nonsensical when it is precisely the point: When a lab prototype is their only progress in 25 years there is reason to be massively unimpressed.

      Tests in a lab for bleeding edge technology like this are not proof that it can work reliably outside the lab. That some in government & industry consider the technology to be interesting does not automatically imply that they believe that the technology is feasible for their claimed access to orbital space. Interest for other uses. such as Hypersonic/Suborbital missiles is more likely.

      When RE has flight hardware that has been tested to prove that it can confer cheap & reliable SSTO to orbital space, then I'll be impressed. Their track record so far leads me to believe that this is unlikely to happen in my lifetime. That is my point.

      --
      Democracy is a sheep and two wolves deciding what to have for lunch. Freedom is a well armed sheep contesting the issue
    17. Re:So where's their spaceplane? by AmiMoJo · · Score: 1

      Sadly, I don't think £120m is going to get them very far. They will need at least a billion to get this thing into orbit. 120M is just keeping some of the government's friends employed for another few years.

      --
      const int one = 65536; (Silvermoon, Texture.cs)
      SJW, n: "Someone I don't like, and by the way I'm a fuckwit" - AC
    18. Re:So where's their spaceplane? by Anonymous Coward · · Score: 0

      I think I saw a documentary where the designers were somewhat thankful for at least one part the whole debacle, having to go back to the drawing board on the engine/aircraft designs to avoid the "state secrets" garbage resulted in a better craft. The air cooler on HOTOL had a few issues and the aerodynamics of the aircraft were causing major problems.

    19. Re:So where's their spaceplane? by TheTurtlesMoves · · Score: 1

      Nothing has been demonstrated at march 5. It was all at sea level zero velocity.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
  5. Not so fast by tsotha · · Score: 3, Interesting

    But even if you manage to land the booster stage, it’s going to need a very expensive inspection before it can be flown again. Rockets tread a fine line between flying and exploding. It’s hard enough to get them to work just once, let alone tens or maybe hundreds of times.

    Ultimately jet engines are just complex rocket engines that use outside air for the oxidizer. The reason commercial jet engines are more reliable, generally, is they aren't pushed to the very edge of what's possible, performance-wise, and they're produced in large quantities. But neither will be true for the Skylon SABRE engines. I don't see any reason to think they'll be any cheaper to maintain than the Space Shuttle Main Engines.

    1. Re:Not so fast by EdgePenguin · · Score: 1

      Because Reaction Engines are not NASA and its not the 1970s anymore? You seem to be assuming that SSMEs are the cheapest LH2 engines that could ever be made (wrong - see RS-68, RD-0120 etc.) and that NASAs procedures for turning them around are optimal.

    2. Re:Not so fast by tsotha · · Score: 1

      Reaction Engines are not NASA, true. And as such they don't have any experience taking engines (of any sort) to space and back. And yes, other hydrogen engines have been cheaper. But they weren't designed to be reused, either.

      It's not difficult to imagine an organization that can do things more cheaply than NASA. But just wishing away costs like that isn't going to work. Even assuming they get the damn thing to work at all, I will be shocked if their net $/kg figure is lower than SpaceX's.

    3. Re:Not so fast by EdgePenguin · · Score: 3, Insightful

      They have worked out their cost/kg and found it to be lower - and had their sums checked by third parties. I have the feeling this project is largely not being taken seriously because Americans don't pay attention to anything outside their borders (and generally refuse to believe any worthwhile advance comes from outside the US)

    4. Re:Not so fast by _merlin · · Score: 1

      Ultimately jet engines are just complex rocket engines that use outside air for the oxidizer.

      No, more importantly than that they use outside air for the reaction mass, and this is what makes them so much more efficient than a rocket.

    5. Re:Not so fast by tsotha · · Score: 1

      Your feelings aside, I think the reason most people don't take this project seriously is so far all they've actually produced is a pre-cooler.

    6. Re:Not so fast by kellymcdonald78 · · Score: 1

      The X-33 was also supposed to dramatically reduce the cost of access to space. People had checked "the sums" Of course the problems started to arise when they actually started building the thing. Suddenly it wasn't as easy to build composite conformal LH2 tanks as they thought and the program went from "the SSTO future of cheap space travel", to a rusting curiosity. For Skylon to work, it requires everything to go just right, if 1 or 2 technologies don't pan out, or turn out to weigh more than originally expected, you suddenly have a vehicle that can't carry a useful payload. Every single SSTO project has turned out this way, brilliant on paper, but much harder once metal is bent. Maybe Skylon will be different, but they have a long, long, long road before the first one flies. I can understand the national pride angle (hey I'm Canadian, so I don't even have a bird in the fight), but I'm confident that Skylon will never fly. SpaceX by luck or good planning has stumbled onto a virtuous cycle that puts them on the most viable path to reliability and to reducing the cost of access to space. How: 1. They built a heavily over-engineered largely conventional rocket that has a viable path towards reusability. They can build a little, test a little, get missions under their belt and learn how the Falcon 9 flies and where they can optimize performance (Falcon 9 "full thrust" launches later this year). However even if all these reusability experiments fail for some reason, they still have a profitable launch vehicle. If Skylon fails, they've got nothing, except maybe a very very expensive ballistic transport. 2. All of the R&D flights are on someone elses dime. By building the Falcon 9 larger than what is needed for most LEO payloads, it can fly those payloads at a profit, and then, once the second stage is away, do what ever experiments they wish to test out various recovery options. They are running a viable business while building up the experience and expertise they need to reuse a stage. Most launch vehicles are built to the smallest possible size and then scaled with SRBs so any flight test incurs additional costs (even if its just for the SRBs). Skylon requires $12 billion up front to build a vehicle, someone needs to be willing to invest that money on a vehicle that may or may not work. 3. Development costs, to 2014 SpaceX has invested ~$1 billion to develop both Dragon and Falcon 9 (both their money and NASA's). The initial Falcon 9 version took $300 million to develop (less than what was spent to just develop Skylon's heat exchanger). For argument sake, lets say it will cost SpaceX $1 billion in R&D on the Falcon 9 before they can start recovering stages, and over the lifetime of the vehicle they fly 200 times. That's $5 million per flight in R&D costs. Skylon at $12 billion (and those were 2004 numbers), even it if flies 1000 times, is $12 million a flight in amortized R&D costs per flight (almost a quarter of the price of an expendable Falcon 9). Skylon estimates amortized launch costs at $1000/kg, SpaceX is hoping for $1100/kg, so while operational costs of Skylon may theoretically be much cheaper. when you account for the R&D costs, the differences are negligible (and Falcon 9 is far lower risk than Skylon) 4. Scaleability. To scale Falcon 9, you can stretch the tanks, upgrade the engines, or in the case of Falcon Heavy, stack cores . With the exception of Falcon Heavy, all of these have already been demonstrated. To scale Skylon requires the entire vehicle to be redesigned. In 3 years when REL starts looking for investors to fund the rest of the development of Skylon (even if they now have a demonstrable engine), are those dollars going to flow to a high risk, high cost proposal, or to SpaceX who by routinely recovering and reusing stages has just quartered the cost of launch

    7. Re:Not so fast by WolfWithoutAClause · · Score: 1

      Actually, their team are were built from battle hardened rocket engineers, who had put stuff into orbit before.

      I've looked at their design, been to lectures by them and asked questions. If it works, I will be absolutely gobsmacked if it isn't cheaper than SpaceX.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    8. Re:Not so fast by WolfWithoutAClause · · Score: 3, Informative

      Actually, the Skylon group predicted that the X--33 wouldn't work. They said that the X-33 was too tail heavy. And fixing it would mess up the payload fraction. And they were right.

      It's difficult to get your head around just how far ahead these guys have been for about 20 years.

      The ultimate reason is that they built a computer model of launch vehicles, which they fiddled with until they got a plausible vehicle. Then they did a back-back comparison with a pure-rocket vehicle, and found that there was no big advantage. Then they fiddled around more, and out popped Skylon, and then they found it *seriously* beats pure-rocket vehicles; it's not even close.

      Skylon is looking at costs starting around $500/kg and then going lower. SpaceX won't be able to get down to that.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    9. Re:Not so fast by tsotha · · Score: 1

      Sure, at this stage of any project it's easy to be "looking at" very low costs. They haven't done anything yet. The nature of these kinds of projects is there are a whole bunch of costs, technical an regulatory, that aren't apparent until you actually start building something. The X-33 is actually pretty instructive - like REL, Lockheed Martin tried to pack a whole bunch of new technologies into a single program, and the failure of any of them would doom the program. And no, the X-33 didn't fail because it was tail heavy. It failed because the unobtainim we needed for the stupid multi-lobed LH2 tank simply wasn't available.

      The risks for large cost overruns grow as you add brand new technology. For Skylon It's not just the SABRE pre-cooler. A craft with a fully carbon fiber frame, ceramic skin, and active cooling gets a big Marge Simpson "Hrrmmmm, okaaaaaaay". Sure, it's probably doable. But that's not at all an easy thing to design, and cost estimates are likely to be optimistic.

      This thing is going to be a whole lot more expensive than the sums they've penciled out. The only question is how much more. Don't get me wrong - I'd love to see them succeed. I'd love to see an honest-to-God SSTO that dramatically cuts costs to orbit. I'd even settle for a failure that lit the way to a follow-on success since I'm, you know, more of an enthusiast than an investor. It's just way too early to get excited, though. When they have a full-power SABRE engine reliably propelling a test bed from the runway to Mach 5.5 at 26 km, one that comes in at the weight they need, one that doesn't break the bank, then it's time to get excited.

    10. Re:Not so fast by Anonymous Coward · · Score: 0

      Skylon is looking at costs starting around $500/kg and then going lower. SpaceX won't be able to get down to that.

      Yes, but by the time Skylon (stupid name, btw) is ready for commercial or government payloads, Elon Musk will have retired on SpaceX money and be riding in his Hyperloop from L.A. to San Francisco.

    11. Re:Not so fast by dave420 · · Score: 1

      They have done something, though. You stating they haven't doesn't change that.

    12. Re:Not so fast by Barsteward · · Score: 1

      have you checked what that pre-cooler has to do ??? its the new technology part of the project.

      --
      "The hands that help are better far than lips that pray." - Robert Ingersoll (1833-1899)
    13. Re:Not so fast by tsotha · · Score: 1

      Sure. They're on the one yard line. Only 99 to go!

    14. Re:Not so fast by tsotha · · Score: 1

      As the AC pointed out above, they're planning to get a mass factor out of the structure that nobody's been able to get in the past.

    15. Re:Not so fast by Anonymous Coward · · Score: 0

      Neither America nor Britain have access to Wehrmacht personell lately. So yeah, no way to realize it.

    16. Re:Not so fast by Maritz · · Score: 1

      This thing is going to be a whole lot more expensive than the sums they've penciled out. The only question is how much more.

      Wow, predicting that a large and complex project will cost more than initially anticipated? You're all about the bold predictions. Now I know you're talking real sense. Go ahead, say they haven't built anything yet again.

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    17. Re:Not so fast by Anonymous Coward · · Score: 0

      Most people do not even try to start, thinking that will never works, so...

    18. Re:Not so fast by Anonymous Coward · · Score: 0

      Nothing changed that *SMACK* is the sound of dave420 going down being wrong eating his words bitch slapped by apk http://slashdot.org/comments.p...

    19. Re:Not so fast by kellymcdonald78 · · Score: 1

      SpaceX has computer model of Falcon 9. It originally showed that they'd be able to recover the second stage. Then reality settled in, once they had real performance numbers and actual flight data, they revised their models and like that it wasn't viable to recover it anymore. SSTO models are insanely sensitive to changes in assumptions. All it takes is 1 or 2 technologies to not pan out exactly as expected and you've got zero payload. X-33 isn't the only one to suffer from this, same thing happened to the X-30, X-34, Kistler and Rotary Rocket, of course then again REL is "just so far head of anyone else". A computer model is exactly that, a model, entirely based on assumptions of material properties and masses. These assumptions don't always line up with reality. The $500/kg number doesn't include amortized R&D costs, which when its going to cost $12B or more (again these are 2004 numbers, with inflation it's now $15B), these are the costs that kill your economics. Skylon themselves have quoted $1000/kg when these are included (as I said, even over 1000 flights, amortized R&D just by itself is almost a quarter of the cost of an expendable Falcon 9). When you factor that in, Skylon isn't much better than Falcon 9

    20. Re:Not so fast by WolfWithoutAClause · · Score: 1

      > Sure, at this stage of any project it's easy to be "looking at" very low costs. They haven't done anything yet. The nature of these kinds of projects is there are a whole bunch of costs, technical an regulatory, that aren't apparent until you actually start building something.

      I don't agree. For example, the Space Shuttle estimates were about on the money. As in they said, the cost estimate is $X, but we'll need $1.2 X, to allow for obvious contingencies. President Nixon went: we don't budget contingencies, we'll give you X and then fund the overrun later. NASA: OK boss.

      So actually, it cost what they said, but it looked to the rest of the world like an overrun.

      And the Space Shuttle main engine was about as complicated as SABRE looks like it will be, maybe more so, it was an unreasonably complicated design.

      And Reaction Engines actually have a careful design, with computer modelling of everything. That bodes well for a relatively straightforward detailed design and build. The X-33 had none of that, and when they got around to it, they found the horizontal stabilisation was total shit.

      And the engine is particularly clever in that it works almost the same at all speeds; the precooler means that it doesn't care whether it's at ground level or Mach 5, the air behind the cooler is at the same temperature. That means, like a rocket engine, they can do almost complete testing when stationary. And the precooler also, they've already tested the precooler; it works fine. And the precooler was the most challenging bit of the whole system; it's something like half a gigawatt per tonne of cooling.

      The take-home message is not that it's not a clever design, it's that most of the clever bits are easy to ground test. About the only bit they can't totally test on the ground is the aerodynamics of the aeroshell- but that was basically the same problem that the Space Shuttle faced and dealt with.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    21. Re:Not so fast by tsotha · · Score: 1

      Oh, aren't you a genius for pointing out I've pointed out the obvious? Your parents must be very proud!

    22. Re:Not so fast by WolfWithoutAClause · · Score: 1

      Actually, I once did a computer model of SpaceX-style reusability, and that's actually what my model showed me, that it would be extremely hard for SpaceX to get it to work.

      But my modelling shows that Skylon ought to make orbit, and return and land safety with comparative ease, Their design is very insensitive to weight growth; and they actually have spare mass built into their design in case things are harder than they look.

      But yeah, I do agree with you pretty much on the economics, that's the worst part of their design. But compared to the economics of the Space Shuttle... ;)

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    23. Re:Not so fast by Anonymous Coward · · Score: 0

      Dude, you're in the "I coulda been a contender" realm.

      You're talking trash about SpaceX when they have a flight record. Their tech works and they built it. When it breaks they own up, talk straight and fix it.

      What does Skylon have? A computer simulation? Third party evaluations of their paper plans? A cool looking proposal? Ask yourself why Skylon has been stuck in low gear for 20 years. You claim it's money and money alone, their tech is superior. Even if we take you at your word, a superior proposal gets left in the dust by real implementation every time.

      I know of literally dozens of cool proposals in the aerospace industry that went nowhere. Maybe hundreds! I wish Skylon well but right now they have a paper spaceplane.

    24. Re:Not so fast by TheTurtlesMoves · · Score: 1

      They haven't worked out costs. They have guessed costs. And on the very very optimistic side i may add.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
    25. Re:Not so fast by WolfWithoutAClause · · Score: 1

      > Their tech works and they built it.

      LOL, I don't think so.

      This is the tech that keeps lithobraking and exploding when it's supposed to be landing on a barge. They've been trying to pin a landing since the first flight of Falcon 1. They're currently on Falcon 9.

      Maybe they'll succeed one day, but the very high performance rockets they build are obviously *very* fragile.

      And that's the problem with their approach, pure rocket reusables have to be super lightly built, and then it's very difficult to make it back down to the ground.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
  6. Ob. XKCD by zorro-z · · Score: 2
    --
    -Z
  7. why the complex dual-mode engine? by Anonymous Coward · · Score: 0

    Why not just fit it with a turbo-jet *and* a rocket engine--each optimized for their own roles and just switch from one to the other rather than combining them?

    1. Re:why the complex dual-mode engine? by Anonymous Coward · · Score: 1

      Weight.

    2. Re:why the complex dual-mode engine? by Anonymous Coward · · Score: 0

      You would have to have more structure to accommodate both rocket and jet engines, that adds quite a bit of weight. You'd also have more drag on the craft because of the big cones sticking out of the back of your "jet" and the big air collectors sticking out of your "rocket". "Stage and a half" concepts are preferable, have a rocket strapped to the bottom/top of a jet, release it when the jet has reached its maximum speed/altitude and off you go. Some stage and a half concepts even integrate ram jets to get a little more speed/altitude from the carrier craft.

  8. Skylon Pros and Cons by Irate+Engineer · · Score: 2

    Pros:

    A single engine that can transition from air breathing jet to scramjet to rocket, all the way from runway to orbit and back!

    Cons:

    A single ungodly complex engine that might transition from air breathing jet to scramjet to rocket, all the way from runway to orbit. Or not.

    Cool idea on paper, but I see way too many moving parts over a huge performance envelope for me to believe this will ever be a robust engine. It just seems too complex to be a "fuel-up-and-go" engine. Looks more like a engine that would need to be torn down and inspected after every flight, assuming it works once. But best of luck to them all the same.

    --

    Left MS Windows for Linux Mint and never looked back!

    Vote for Bernie in 2016!

    1. Re:Skylon Pros and Cons by EdgePenguin · · Score: 4, Insightful

      Wrong on multiple points

      It never becomes a scramjet. Not being a scramjet is in fact the entire point behind the last few decades of research. You can either try to burn fuel in a supersonic flow through your engine (scramjet) or you can slow the flow to subsonic and compress it so the fuel can burn properly (ramjets etc.) - problem is, this compression superheats the air. SABRE dumps the excess heat into the cryogenic hydrogen the vehicle carries so that you can operate an engine at high Mach number without its insides melting.

      As for too many moving parts; they precooler itself does not appear to have any moving parts. It needs a liquid helium cooling loop to connect it to the hydrogen supply, but that isn't overly complex. Everything behind that is well established jet/rocket engine technology. Even if you assume that each precooler + bypass is itself as complicated as enough engine, the spacecraft only has as many "moving parts" as an ordinary rocket with 4 engines. SpaceX happily flies a rocket with 9 engines and will likely be able to reuse its first stage in a cost effective way.

    2. Re:Skylon Pros and Cons by tomhath · · Score: 1

      SpaceX happily flies a rocket with 9 engines and will likely be able to reuse its first stage in a cost effective way.

      I'll believe that when I see it. IMHO air breathing planes will never replace solid fuel boosters to get through the atmosphere.

    3. Re:Skylon Pros and Cons by EdgePenguin · · Score: 2

      Your opinion is based in ignorance then. Costs cannot come down without re-usability and solid rockets are not reusable. The Shuttle SRBs had reusable casing - which had to be separated into segments, refilled with solid fuel, and then put back to together. Ever see an Airbus A320 get chopped into segments between flights?

    4. Re:Skylon Pros and Cons by Irate+Engineer · · Score: 1

      The spacecraft only has as many "moving parts" as an ordinary rocket with 4 engines. SpaceX happily flies a rocket with 9 engines and will likely be able to reuse its first stage in a cost effective way.

      And you do realize that even these "ordinary rockets" still do explode, even though the basic technology has been around since the 1960s? See Orbital, see the SpaceX Falcon 9 CRS-1 mission. And even some of the simple "technologies" (tank support struts) fail in these operational extremes.

      Every component, moving or not, has a non-zero chance of failure. More parts, higher failure probability. Put those parts into an extreme operating environment, probability of something unanticipated biting you in the ass goes up as well.

      If they can launch and return the Skylon with the same maintenance as an airliner, I'll be happy and very impressed. However I really think it is too complicated to work repeatedly.

      --

      Left MS Windows for Linux Mint and never looked back!

      Vote for Bernie in 2016!

    5. Re:Skylon Pros and Cons by EdgePenguin · · Score: 4, Informative

      The existence of failure modes is not a sufficient reason to predict high failure rates.

    6. Re:Skylon Pros and Cons by BradMajors · · Score: 1

      An easy way to reduce the cost of getting cargo into space is to not send humans in the same spaceship. Making a spaceship safe enough for humans is expensive.

    7. Re:Skylon Pros and Cons by Rei · · Score: 3, Interesting

      I've sometimes pondered the concept of a self-consuming rocket engine - basically infinite-staging.

      Picture a spike (although the ideal shape would be different from an aerospike) comprised of small channels between aluminum - for example, assembled via fine aluminum wires or finely corrugated aluminum sheets, all the way through, thus leaving empty space between them. The wires or sheets would be joined together by having any surface oxide removed (or inhibited altogether by alloying agents), and heated enough in a non-oxidizing environment to braze them together. The channels would be filled with an oxidizer-rich polymer/ammonium perchlorate mixture (very mainstream as far as propellants go).

      The engine would need to be lit off across its entire surface, so all channels ignite (or be designed such that neighboring channels ignite neighbors who fail to ignite).

      The propellant mixture would burn down into the channels (as even fine aluminum wire/sheeting takes time to burn through) - lacking any area within the channels to expand into, it remains compressed and accelerates linearly as it moves through the channel (design parameters set such that the compression ratio achieved is the desired compression ratio for the engine). The angle of the channels would direct the stream largely along the spike, so that the gases expand along an ideal expansion profile for generating forward thrust. Since the entire spike would be comprised of channels, again, the ideal shape would be different form an aerospike; the exhaust gases don't simply come from the top.

      As the oxidizer-rich propellant burns down, it progressively erodes the aluminum making up its channels (again, alloying agents in the aluminum may be used to help or hinder this process). Since the exterior ends of the channels would be exposed to the oxidizer-rich exhaust for the longest, they'd progressively burn down from their ends. Since the exhaust burns further as it flows (and the oxidizer would be more liberated), again the erosive potential of the stream would be highest near the end of the channels. So like a wick keeping pace with a candle as it burns down, the channels would be expected to erode away at approximately the same rate that the propellant burns down.

      Aluminum metal is itself is a very energetic-burning compound - aluminum dust is often included in solid rocket mixes, so the erosion of the aluminum channels is a significant thrust contributor. Lithium-aluminum would be even better - lithium-aluminum is stronger than aluminum, and lithium is even more energetic than aluminum. It would also help neutralize the hydrochloric acid that occurs in most ammonium perchlorate-based solid propellants (although there are other techniques as well, such as burning magnesium and/or sodium nitrate with it).

      In a naive implementation, the spike would change from the ideal shape to a progressively suboptimal shape as it burned down. But the rate of propellant burn and aluminum erosion could be controlled by tweaking the parameters of the system such that the areas of the spike you want to last longer can burn down slower than the areas you want to burn down faster. Hence the ideal spike shape can be retained as the engine burns down, all the way to right before it burns out.

      Basically, your rocket would be... no rocket at all; just propellant. The entire thing is consumed. It'd be useless for orbital maneuvering**, but to get to orbit, the rocket equation likes nothing better than non-stop continuous staging with no tankage or engine mass at all (a caveat in this regard: your gimbaling system and interstage would still have to be sized for when it's at full size and max thrust). No complex systems at all. No exotic manufacturing techniques needed. No exotic, expensive materials. Just aluminum and a not-particularly-unusual solid rocket propellant. Getting the details of the mix right to ensure 1) even ignition, 2) even burndown, and 3) aluminum erosion at the proper rate would take research and experimentation, but I would e

      --
      The yellowcake is a lie.
    8. Re:Skylon Pros and Cons by Anonymous Coward · · Score: 0

      Wow. I'll tell the Wright Brothers they were wrong, then. Or did they actually use an air-breathing gasoline engine to spin a propeller to push their kite through the atmosphere at Kitty Hawk??

    9. Re:Skylon Pros and Cons by Anonymous Coward · · Score: 0

      If I'm reading you correctly, that would make the the thrust's surface area larger and having adjacent cells (even if they failed in part) would mean a sort of redundancy in outcomes. It might end up that your idea is safer. You didn't mention that - so it may be something you've overlooked or something that I am not understanding. I figure, a single cell (in your design) failing to ignite immediately or in perfect synchronization would have less impact than a general failure to fire issue with current rocket technologies. I'd also assume that it would be likely to ignite even if it's just a bit later.

      Hmm... You should probably put that on 'paper' and submit it to someone who's a more formal student. I don't know as I've seen that suggested before but I am not a rocket surgeon.

      KGIII (It's saying that the resource is no longer available when I try to post logged in. I think my VPN is screwing up.)

    10. Re:Skylon Pros and Cons by Anonymous Coward · · Score: 0

      So it borrows efficiency in the future for a working jet engine now. The SSME uses the cryogenic hydrogen to cool the rocket nozzle so it can obtain a higher ignition temperature and thereby higher fuel efficiency. If you heat that hydrogen up before switching to rocket propulsion you won't have this option and your rocket engine will be less efficient.

      Spaceplanes look cool, but until this thing is manufactured and tested any cost-to-orbit numbers quoted are speculation. Maintenance costs are unknown. The article is basically an ad dumbing down and misrepresenting why it is expensive to go to space, not to mention misrepresenting how much cargo mass is lost per passenger.

    11. Re:Skylon Pros and Cons by dbIII · · Score: 1

      A single ungodly complex engine

      That's rockets for you. Anything other than solid fuel stuff gets bits added onto bits to even out what the first bit does.

      Looks more like a engine that would need to be torn down and inspected after every flight

      Yes.

    12. Re:Skylon Pros and Cons by Electricity+Likes+Me · · Score: 1

      This is a hybrid rocket engine.

    13. Re:Skylon Pros and Cons by tsotha · · Score: 1

      Heh. A caseless rocket engine.

    14. Re:Skylon Pros and Cons by Anonymous Coward · · Score: 0

      You have forgotten two basic details. The combustion must be contained by some type of container (usually the body of the rocket engine in a normal design) and the pressure that the combustion will cause. Your idea would generate a Christmas tree that probably explode on the ground or burn like a huge fire, without moving.

    15. Re:Skylon Pros and Cons by Rei · · Score: 1

      As mentioned, it's contained within the aluminum channels. A sizeable chunk of the mass of the "engine"/propellant would be aluminum metal (whether wires, corrugated sheets, etc, brazed together), meaning rather tremendous total structural strength. Each individual channel has little strength, but on the other side of each channel is another channel - the outward-pushing pressure from combustion in one channel is countered by the opposite pressure from the adjacent channels.

      --
      The yellowcake is a lie.
    16. Re:Skylon Pros and Cons by Anonymous Coward · · Score: 1

      This idea is patented, see

      http://www.google.co.uk/patents/US4170875

    17. Re:Skylon Pros and Cons by Rei · · Score: 1

      Similar, but not the same. Their design calls for no reinforcement at all - pressure is to come only from the bow shock. That significantly reduces the potential for pressure (as well as making the rocket more fragile), and thus the efficiency - particularly at low velocities and low external pressures (hence their focus on hypersonic missiles). In particular, due to the need for a bow shock to compress the exhaust gases, at zero velocity there is zero compression - they have to launch it from a cannon to get it going. My proposal would certainly benefit from a bow shock but does not fundamentally require one, as the eroding aluminum structure provides compression as well. Ironically, they also, include the aluminum in the propellant mix, but include it as a powder, where it's not doing any good toward increasing the pressure. Sure, the powder burns much faster, but the whole purpose of the aluminum in my variant is to not burn too quickly, so that it's around long enough to do some good.

      Still, neat to see that they were exploring some of the same concepts.

      --
      The yellowcake is a lie.
    18. Re:Skylon Pros and Cons by Anonymous Coward · · Score: 0

      It's not clear to me from your description whether the oxidiser is to be solid or liquid. If it's solid, what you've described is a solid rocket motor; if it's liquid, you've described a hybrid rocket motor.

      You've described the propellant block as being shaped similarly to an aerospike, presumably for the same reason. But it's critical to the operation of an aerospike that the exhaust gases are released at the base (top) of the spike, and expand as they travel along its length. Since the exhaust gases in your design are released from the entire surface of the spike, you don't get that benefit; you're essentially just running a rocket without a nozzle.

      To minimise air resistance, a rocket motor and tankage should be long and slender. But if you make your spike long and slender, your performance is even worse: along most of the length of the spike, your exhaust gases are being emitted laterally, and the thrust is (symmetrically) sideways.

      Finally, I'm not sure that sintering a large mass of aluminium wires in a non-oxidising environment is such a cheap thing to do. It would certainly be more expensive than casting propellant blocks for existing solid rockets; it might be cheaper than assembling complex liquid-fueled engines. But the performance would be much closer to the former: solid rocket engines already have a small non-fuel mass fraction, and even eliminating this entirely wouldn't allow you to rival the performance of liquid H2/O2 with solid aluminium/perchlorate. So, at best, this would be a compromise in both price and performance between solid and liquid rockets.

    19. Re:Skylon Pros and Cons by Rei · · Score: 1

      It's not clear to me from your description whether the oxidiser is to be solid or liquid

      How can that not be clear? It says many times that the oxidizer is ammonium perchlorate. That's a solid. Polymer/perchlorate mixes are pretty standard solid rocket fuels.

      If it's solid, what you've described is a solid rocket motor; if it's liquid, you've described a hybrid rocket motor.

      Conventional solid and liquid rockets do not consume their "casing" and "engine" as they fly

      You've described the propellant block as being shaped similarly to an aerospike, presumably for the same reason. But it's critical to the operation of an aerospike that the exhaust gases are released at the base (top) of the spike, and expand as they travel along its length

      I wrote twice, "although the ideal shape would be different from an aerospike" The presence of exhaust gases being released both at the top and further down changes the ideal shape from a spike to a more conical form. Note of course that even in most conventional aerospike designs, a fraction of the exhaust (usually from that which is used to drive the turbopumps) is exhausted through the bottom of the spike.

      Since the exhaust gases in your design are released from the entire surface of the spike, you don't get that benefit; you're essentially just running a rocket without a nozzle.

      I think you're confused about how aerospikes (and rocket engines in general) work. The aerospike isn't what causes the gases to compress - just the opposite, it's an expansion nozzle, akin to the bell-shaped traditional expansion nozzle. There are one or more combustion chambers above the spike which are responsible for creating the compressed gas stream, which emerges at high velocity through the throat. In a conventional bell nozzle, this gas streams out straight downward and is constrained in outward expansion by the bell on all sides, up until (ideally) it reaches ambient pressure. In an aerospike, it emerges angled inward, with the ultimate expansion force being directed downward due to the action of the low pressure wake in the center, which effectively acts as an extension of the spike out to infinite length. At high pressure, the expansion remains angled inwards for a long period due to the exterior air pressure, and tracks its path away from the rocket. At low pressures the exhaust stream angles more outward and forms a broader expanding column, but still linearly directed away from the rocket. The exact process is complex and involves the reflection of compression waves, but that's getting a bit off topic here.

      Like in a traditional aerospike, in what I was talking about, the spike isn't what causes the gases to compress. The gases are compressed because the burning propellant is in channels inside an aluminum structure. It has nowhere to go but out one end, but the tight channel limits the rate at which it can escape. Each little channel - space between wires or aluminum corrugations - is like a micronozzle. The spike itself is, as in an aerospike, the core of an expansion nozzle. Its purpose is not compression - it's expansion.

      your exhaust gases are being emitted laterally

      Again, quoting the above: " The angle of the channels would direct the stream largely along the spike"

      Laterally? Why on Earth would one angle the channels laterally? What's the logic in directing your stream outward?

      Lastly, see the comments above: there's actually an Air Force patent for something similar (although it relies on bow shock for compression rather than microchannels, and is thus limited to high speed atmospheric usage and lower compression ratios). If the Air Force saw fit to patent a related concept (to avoid having to pay royalties to others if they should build it, according to the patent), then it's certainly not absurd.

      --
      The yellowcake is a lie.
  9. 50% more than LEO, TO BE EXACT by raymorris · · Score: 5, Insightful

    To get to low earth orbit, a vehicle needs to be travelling at 17,400 MPH (7.7 km/s). If it travels just bit faster, 25,000 MPH, you can head off wherever you want to go in space. Orbit is 2/3rds of the way to anywhere.

    1. Re:50% more than LEO, TO BE EXACT by Anonymous Coward · · Score: 1

      You mean go nowhere, right? It's mostly an empty, deadly, radiation-blasted hell. You know that, right? Repeating the feverish sci-fi "proverbs" of a professional daydreamer doesn't change that, right?

      www.distancetomars.com

      You may very well toss small robotic camera boxes to your precious "anywhere", but considering the universe is 14 billion light years across, and it took 40 years for a camera box to barely reach the edge of just our solar system, what, precisely, do you expect this "anywhere" to be?? Who is this "we" who wants to go in space? "Anywhere" in space, no less!

      Put down the Star Trek, pick up the physics and reality 101. For your own good.

    2. Re:50% more than LEO, TO BE EXACT by k6mfw · · Score: 1

      Put down the Star Trek, pick up the physics and reality 101. For your own good.

      Larry Krause implied this but not in those words. In a presentation he mentioned amount of energy it takes to accelerate a federation starship is way more than the mass of the ship (E=mc^2). I tried some basic calculations using KE=1/2mv^2, my values seemed quite low. However the concept seems valid (examine amount of energy it takes to put a measley 3000 lb (mass) into LEO.

      --
      mfwright@batnet.com
    3. Re:50% more than LEO, TO BE EXACT by Princeofcups · · Score: 1

      To get to low earth orbit, a vehicle needs to be travelling at 17,400 MPH (7.7 km/s). If it travels just bit faster, 25,000 MPH, you can head off wherever you want to go in space. Orbit is 2/3rds of the way to anywhere.

      Nice numbers, except that's not the way it works. Higher orbits are SLOWER than low ones. And then there's oblique verses circular, which comes from the way you are pointed when you are accelerating. Seriously, Orbital math is hard.

      --
      The only thing worse than a Democrat is a Republican.
    4. Re:50% more than LEO, TO BE EXACT by Anonymous Coward · · Score: 0

      Nice job on the condescending tone. Sadly, you and your huge brain schooling us in orbital math is completely besides the point. 25k MPH is the escape velocity from earth.

      You might want to tell that big brain of yours to shut up once in a while and resist the urge to spew facts that are irrelevant. Seriously, navigating life without sounding like a dick is hard.

    5. Re:50% more than LEO, TO BE EXACT by PPH · · Score: 1

      Higher orbits are SLOWER than low ones.

      Once you are up there. But you have to trade kinetic energy (velocity) for potential (altitude).

      --
      Have gnu, will travel.
    6. Re:50% more than LEO, TO BE EXACT by Anonymous Coward · · Score: 0

      Play some Kerbal Space program or Orbiter, once you're out of the atmosphere and don't have to worry about drag you can achieve quite a few transfer orbits with a surprisingly small amount of fuel, especially if you use highly elliptical orbits. Not saying either of those programs have fully real world orbital mechanics, but they do give you a pretty good idea of the basics.

  10. Save the humans by MrKaos · · Score: 1

    It should read "leaving this planet is the only way of saving ourselves". I'm pretty sure the Earth will be here long after any sign of us has vanished.

    --
    My ism, it's full of beliefs.
  11. "Build something" is not "Build everything" by Anonymous Coward · · Score: 1

    Building the hardest individual part and asking for more funding to make the full device, having shown that it works is a perfectly respectable strategy, unless you have a budget larger than most governments or can pull the whole thing of at once using magic, is that what you are asking for?

    1. Re:"Build something" is not "Build everything" by Ol+Olsoc · · Score: 2

      Building the hardest individual part and asking for more funding to make the full device, having shown that it works is a perfectly respectable strategy, unless you have a budget larger than most governments or can pull the whole thing of at once using magic, is that what you are asking for?

      I thinnk the animation is the finished product. It indeed works pretty well.

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    2. Re:"Build something" is not "Build everything" by Maritz · · Score: 1

      You're hilarious. I bet you're chuckling away at just how gosh-darn funny that post was. Well done you.

      --
      I do not want your cheap brainburning drugs. They are useless for work. And I am a working man today.
    3. Re:"Build something" is not "Build everything" by Ol+Olsoc · · Score: 1

      You're hilarious. I bet you're chuckling away at just how gosh-darn funny that post was. Well done you.

      Consider that it might not have been a joke, or meant to be funny.

      --
      The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    4. Re:"Build something" is not "Build everything" by Anonymous Coward · · Score: 0

      Anyone got some Penaten for his butthurt?

  12. Which is the hardest and only novel part... by Anonymous Coward · · Score: 0

    When "all" you have done is the most risky and difficult part then why should you not at least be taken a little seriously..

    1. Re: Which is the hardest and only novel part... by Anonymous Coward · · Score: 0

      There is also the part where the structure is stronger and lighter than snything in existence.

  13. Skylon = SkyNet + Cylon? by tdelaney · · Score: 1

    Seems like a company we can trust with people's lives.

    1. Re:Skylon = SkyNet + Cylon? by freeze128 · · Score: 1

      "Skylons" were the name given to twinkling lights in the sky by Holly Marshall in the original "Land of the Lost" series. They were so named because they looked like pylons in the sky.

    2. Re:Skylon = SkyNet + Cylon? by Anonymous Coward · · Score: 0

      "Skylons" were the name given to twinkling lights in the sky by Holly Marshall in the original "Land of the Lost" series. They were so named because they looked like pylons in the sky.

      According to the interwebs, it wasn't because they looked like pylons in the sky, it was that they protected the pylons and they flew in the sky...

    3. Re:Skylon = SkyNet + Cylon? by tdelaney · · Score: 1

      Thanks - didn't turn up in my web searches (except for disambiguation #5 on Wikipedia) and considering I was born in the same year as Land of the Lost started it's not surprising I wasn't aware of the link.

    4. Re:Skylon = SkyNet + Cylon? by Eunuchswear · · Score: 2

      Nope, it's a reference to the 1951 Festival of Britain.

      --
      Watch this Heartland Institute video
  14. Is Paul Moller on the board? by Anonymous Coward · · Score: 0

    Paul Moller has been announcing that his "Skycar" would give us all a George Jetson flying car future in the near future for something like 50 years. Every few years he gets a bunch of publications to write breathless articles about his flying car tech, which in-turn probably leads a new wave of gullible investors to pour money into one of his businesses. Could the Skycar fly? Possibly, but that does not appear to be the business model. I started my professional life working for a guy like this - an engineer with a small company and an idea. He paid his small staff to keep developing his idea year after year but when you worked for him for a while you realized he had no plan to actually take his project through the regulatory process and into production; it was actually a hobby for him, that was just there to make enough money to stay in business and interesting enough to keep him busy and fiddling until he could retire. My old boss could attract young workers to join (and work cheap) for a while and then get new ones as each figured out the hobby angle.

    The people behind the Skylon have been hyping it for something like a decade, and stories about how it can/could/will revolutionize space travel keep getting written and passed around the net (probably trying to whip-up more investors and even more-probably trying to hit the modern investor jackpot: government subsidy). If you dig through the Slashdot archives, you'll find a bunch of Skylon stories. Do they have something new? Not really. People have talked about flying to space trying to avoid hauling the mass of an oxidizer by using the air for a very long time (it was in some of the proposals for the Reagan-era "National Aerospace Plane" project which failed to get congressional support). In this case, Skylon has a particular air-chilling idea as part of their engine design and BAE is making a relatively small investment in the company. Since Skylon is playing with a particular somewhat interesting engine technolog, it's a low-risk investment for BAE that will probably not help the Skylon people get 1cm closer to space but will get BAE test data on, and some rights to, a narrow bit of engine tech which might someday feed into a future airliner engine and which they then will not need to have any BAE people try.

    1. Re:Is Paul Moller on the board? by k6mfw · · Score: 1

      I met Paul Moller at Yolo County airport in late 1980s. There was a small airshow of sorts, he had a Skycar mockup on display. I asked him why this VTOL will be so much cheaper than what typically be from aerospace companies. Moller said these large companies have only one customer, the government, so there is no reason to make any VTOL vehicle lowcost. He is (was or still is?) for the "average." Earlier in 1980s I found a AIAA paper he wrote and had a set of equations dealing with power and diameter of ducted engines (I cannot find it anywhere now). It outlined for a given amount of powered lift the total ducted area needs to be of a certain value. Moller also wrote his equations showed the Canadian Avro-Car in late 1950s was doomed to never get out of ground effect because total ducted area was too small regardless how powerful the engines may have been. I also remembered the slick brocheres, I looked up the company in the phone book and also (what's that publication that was real popular back in the days?) that lists companies, Moller Corp. business that earned money was selling mufflers that were flow efficient. Moller was also a professor at UC Davis.

      --
      mfwright@batnet.com
    2. Re:Is Paul Moller on the board? by Anonymous Coward · · Score: 0

      Moller has been periodically getting investor infusions after sensational magazine pieces in things like PopSci and PopMech since the 70's; He is never going to mass-produce a flying car. He's had the tech in his hands for many years - the stuff he needs but does not make, like the avionics are readily available. He did not need the current crop of quadcopter drones to come along and teach him anything - he's been using multiple ducted fans for lift for something like 40 years (about as long as from the Wright Brothers at Kitty Hawk to Yeager breaking the sound barrier. In fact, Moller's task has been getting easier year-by-year even without him taking any action: composites, and avionics jest keep improving, getting better AND lighter all the time.

      The problem with the flying car is not technical - there have been successful (in the technical sense) flying cars since the 30's. You can find pics and vids online of Gore Vidal as a child flying in one (when his dad was running the civil aeronautics board for FDR). The problem is government regulations. It takes years and millions of dollars to get a small aircraft through the FAA certifications required to make it legal to manufacture and sell. If you spend $10Million getting your flying car certified and you sell a thousand of them, each one carries a $10K surcharge just in regulatory overhead (before you get to the price of liability insurance which is insanely high for plane makers). Then the market is severely restricted because only people with pilot's licenses can buy them and very few people have such licenses - they take a lot of time and money and effort to get and can be taken away from you on a whim by the FAA based on any number of health problems you could get. We allow people with histories of heart trouble, alcoholism, epilepsy, and even severe disabilities to drive cars and tens of thousands die every year as a result, but we as a society are paranoid about small planes (which actually could be safer for people with health issues given the existence of already proven advanced autopilots) and thus ban people who are imperfect human specimens from operating them.

  15. Well by Ol+Olsoc · · Score: 1
    I RTFA, and I won't get that 3 minutes back.

    It's the web equivalent of an infomercial, completele with the "Everything now sucks, SUCKS SUCKS!

    "But we here at Skylon, we have the improvement needed to transform those sucky rocket based systems into a awesome never look back Skylon System!"

    Which by the way, in no way eliminates those rockets they go way out of their way to tell us - suck.

    Come back when your web page wasn't designed and populated by the Marketing department and some ad agency.

    --
    The shepherds did so well protecting the flock that the sheep no longer believed that wolves existed.
    1. Re:Well by Anonymous Coward · · Score: 0

      You do realize that most of the summary links are to websites that contain articles and press releases on them mixed with ads, right? The company is here, http://www.reactionengines.co.uk/

  16. Horrible name, still 15-20 years out by Anonymous Coward · · Score: 0

    1. Skylon? Terrible name, sounds stupid
    2. Great idea and hope they get it off the ground, but it's going to take another 15-20 years before this thing is doing anything but R&D and test flights. Getting the funding is going to take them half that time.

    1. Re:Horrible name, still 15-20 years out by Chrisq · · Score: 2

      1. Skylon? Terrible name, sounds stupid 2. Great idea and hope they get it off the ground, but it's going to take another 15-20 years before this thing is doing anything but R&D and test flights. Getting the funding is going to take them half that time.

      It's even older than that

  17. Video unavailable due to location by nickweller · · Score: 1

    link .. now would be a good time for slashdot to have a discussion on the balkanization of the Internet. Where the media companies are trying to turn Internet media back into television.

    1. Re: Video unavailable due to location by Anonymous Coward · · Score: 0

      They're not *trying* anymore. They're just doing it with the blessing of governments. The internet as you knew it is gone.

  18. I'll believe it when it happens by DrXym · · Score: 1

    I see the potential but this particular project has been popping in newspapers in one form or another for the last 30 years.

    1. Re:I'll believe it when it happens by Anonymous Coward · · Score: 0

      Germany has its own variant, called SÄNGER:

      https://en.wikipedia.org/wiki/Saenger_%28spacecraft%29

      What did the Russians conceive ? I am sure they had something in the race, too..

      https://en.wikipedia.org/wiki/Single-stage-to-orbit

    2. Re:I'll believe it when it happens by tsotha · · Score: 1

      There's something about engineers and rockets. Franklin Chang-Diaz has been plugging away at VASIMR since 1977.

  19. American Calculus ? by Anonymous Coward · · Score: 0

    That is why you could never launch a satellite without von Braun: You would not be able to perform honest calculations.

    According to

    echo "scale=12;sqrt((6.7*(10^-11)*5.97*(10^24))/(6500*1000))"|bc
    7834.833462468451
    $ echo "scale=12;1000/7800"|bc .128205128205

    That is 12% of satellite speed, 6 times more than you claimed.

    Your desire to badmouth stands in the way of achieving Newtonian physics success.

    I wonder why it is different in electronics, though.

    1. Re:American Calculus ? by Anonymous Coward · · Score: 0

      Fuck dude you should perhaps do it properly. Orbital speed is 7834m/s or 30MJ per kg. 1000m/s gives just 0.5 MJ per kg. 2% of 30MJ is 0.6MJ. OP is out a tiny bit. But only a tiny bit. Since kinetic energy is 1/2 *m *v^2. You clearly didn't even read the post. Nice job from that american calculus buddy.

    2. Re:American Calculus ? by TheTurtlesMoves · · Score: 1

      You have confused speed with kinetic energy. All terms for this scale with v^2 not v. Lift, drag, skin heating, and orbital "lift" are all to v^2. So yea it is the Newtonian physics. 1000m/s is a really really long way from 7800.

      --
      The Grey Goo disaster happened 3 billion years ago. This rock is covered in self replicating machines!
  20. YEAH by Anonymous Coward · · Score: 0

    Crypto-communist scaremongering. We never had better life on the globe and we now have the technology to live almost indefinitely in a bunker, should a nuclear war break out. We can clone "good" humans in case of too much atrophy due to application of medicine. We can repair defective DNA. We can grow food in reactors. We have almost infinite sources of energy from Uranium, Thorium and soon H2 fusion.

    We currently enjoy the luxury of badmouthing nuclear energy so that the Oil+Gas Scammers from BP to Gazprom have their nice business protected. But there is no rational reason we cannot again use fission. China does it on a large scale.

    Population growth levels off except in countries ruled by Mohammedism and in Africa. They need to level off too. With war or without.

    I am not a proponent of the bunker scenario, but I hate being sheep-i-fied by communist propaganda. Humanity can continue to exist here indefinitely and will do so. Our massive brain can fix ANY obstacle to our specie's existence.

    We do not need your rotten ideology. Stop the B.S.

    Captach: Incest. That can be fixed using gene editing. And it WILL be used. Too many horrible genetic deseases around. Why do we need to suffer it, if it can be fixed using technology ???

    1. Re:YEAH by MrKaos · · Score: 1
      Oh, how droll, I have. got. my. own. troll.

      Crypto-communist scaremongering. We never had better life on the globe and we now have the technology to live almost indefinitely in a bunker, should a nuclear war break out. We can clone "good" humans in case of too much atrophy due to application of medicine. We can repair defective DNA. We can grow food in reactors. We have almost infinite sources of energy from Uranium, Thorium and soon H2 fusion.

      You idealism is inspiring, if misguided.

      We currently enjoy the luxury of badmouthing nuclear energy so that the Oil+Gas Scammers from BP to Gazprom have their nice business protected.

      Agreed. Nuclear still needs to sort it's issues out.

      But there is no rational reason we cannot again use fission.

      The question is if human systems can acquire the required discipline to run them without blowing them up.

      China does it on a large scale.

      So in one breath you praise and criticize communism, an interesting dichotomy.

      Population growth levels off except in countries ruled by Mohammedism and in Africa. They need to level off too. With war or without.

      Well, you didn't give a fuck when they were committing human right violations before, so why would you now.

      I am not a proponent of the bunker scenario, but I hate being sheep-i-fied by communist propaganda.

      Riiiight, so advocating going to the stars is communist propaganda. You've probably heard this before, your a moron.

      Humanity can continue to exist here indefinitely and will do so. Our massive brain can fix ANY obstacle to our specie's existence.

      We do not need your rotten ideology.

      So solving the problem of getting mass into orbit cheaply shouldn't be too much of an issue then. Oh, but you think only communists can do it.

      [sic]Captach: Incest. That can be fixed using gene editing. And it WILL be used. Too many horrible genetic deseases around. Why do we need to suffer it, if it can be fixed using technology ???

      Well, let's make a start by spelling the things we need to fix properly. Maybe the genetic diseases came from growing food in the reactor.

      Stop the B.S.

      From the authority of BS.

      --
      My ism, it's full of beliefs.
  21. News flash by Big+Hairy+Ian · · Score: 1

    British Rocket plane sparks Flame War on Slash Dot!

    --

    Build a Man a Fire, and He'll Be Warm for a Day. Set a Man on Fire, and He'll Be Warm for the Rest of His Life.

  22. Here's hoping by ThatsNotPudding · · Score: 1

    they go with round windows this time.

  23. 'Skylon'? Isn't that... by Anonymous Coward · · Score: 1

    ...the planet the Blancmanges come from? They mean to win Wimbledon!

  24. Anyone else.. by Anonymous Coward · · Score: 0

    Read this and think: "Cylon?" Oh *$&^#!

  25. My prediction by Anonymous Coward · · Score: 0

    It won't revolutionize anything. It will come to nothing. In a few months time, a few years, at best, it will be thoroughly forgotten, dead and buried, for all practical purposes. I wish this post could be put forth as an example of short-sightedness in a couple of decades - but it won't.

  26. Try it. Go slow and see if you end up in space by raymorris · · Score: 1

    If going slower puts you further away, try walking at 4MPH and see how far into space you get. I said:

    >> If it travels just bit faster, 25,000 MPH, you can head off wherever you want to go in space.

    At escape velocity, you CAN head off into space. If you WANT to orbit at say, a geostationary altitude, you can slow down - at that lower speed you WILL orbit - you cannot leave that orbit without applying more power.

    In other words, if you want to orbit at a distance, you can go slower. If you want to escape earth's gravity, in order to have complete freedom, you have to achieve escape velocity of 25,000 MPH (or continue to burn your engines for at least an hour which isn't possible due to fuel mass).

    Seriously, Orbital math is hard (for you).

  27. Can't ignore sunk cost by Guspaz · · Score: 1

    Skylon will supposedly be cheaper to operate than currently existing expendable multi-stage rockets or future reusable ones. The problem is that Skylon will have a massive sunk cost: estimates from more than a decade ago put the total sunk costs at $12 billion USD, a figure that is sure to be much higher in reality.

    Skylon has a similar payload capacity to a Falcon 9 rocket, which costs $61.2M per launch. Skylon is predicted to have a $14.7M USD launch cost (assuming the prediction is remotely accurate). Skylon would have to launch more than 800 times just to break even compared to Falcon 9. If SpaceX or any other company is successful in bringing the cost of launch down via reusability, then Skylon could take even longer to pay off.

    In short, considering the enormous costs, Skylon is unlikely to ever be cheaper than alternatives.

    1. Re:Can't ignore sunk cost by Howitzer86 · · Score: 1

      Maybe so, but if you complete a wonder before the other guy, you win the game.

    2. Re:Can't ignore sunk cost by Anonymous Coward · · Score: 0

      $12 Billion, assuming their cost overruns weren't too bad, would be chump change for a reusable orbital craft assuming it didn't need major repairs on a regular basis or its engines weren't made of gold & platinum. The Space Launch System, the heavy lift rocket NASA is building is expected to cost at least $40 Billion for R&D and the first 3 launches. With mission development and payloads for Moon, asteroid or Mars shots it could go over $100 Billion. Modern airliners aren't much better, with costs running into the tens of billions of dollars to develop. If travel into orbit ever does really take off the SpaceX method will have some serious limitations whereas a Skylon type system will have major advantages (just fuel it up, run some tests, relaunch). Full reusability one of the last hurdles to space access.

  28. STOP SAM by Anonymous Coward · · Score: 0

    Sam, stop posting links to these fucking web sites that insist on running a bunch of popups and advertisement scripts. Nobody can read the story because of that bullshit.

    If it doesn't stop, some posters will get banned.

  29. No, no, I have a plan! by Anonymous Coward · · Score: 0

    ARTHUR: What happens now?
        BEDEMIR: Well, now, uh, Launcelot, Galahad, and I wait until nightfall,
                and then leap out of the rabbit, taking the French by surprise --
                not only by surprise, but totally unarmed!
        ARTHUR: Who leaps out?
        BEDEMIR: Uh, Launcelot, Galahad, and I. Uh, leap out of the rabbit, uh
                and uh....
        ARTHUR: Oh....
        BEDEMIR: Oh.... Um, l-look, if we built this large wooden badger--
                [twong]
        ALL: Run away! Run away! Run away! Run away!
                [splat]
        GUARDS: Oh, haw haw haw.

  30. Meh by stoatwblr · · Score: 1

    We need Lofstrom loops and skyhooks.

    This is small stuff. OK for getting people to LEO but not much more than that.

  31. Need to stop doing dumb things by ebvwfbw · · Score: 1

    Like launching rockets from about as close to sea level as they can get. We have real estate that is at least a mile higher with no problem. Denver for example.

    Why launch from the surface in the first place. Could use something like a 1950s B52 or an old 1960s era C5 galaxy... even the european copy of the C5 - the A380 to haul a rocket way up there to begin with, they go right up to the tropopause. Then they don't need anywhere near as large of vehicle nor fuel.

    1. Re:Need to stop doing dumb things by Rei · · Score: 1

      An extra kilometer or two is almost irrelevant in terms of the delta-V required to reach orbit. Meanwhile, launching from near the sea means that ascent (the time when a launch failure poses a serious risk of killing people) is done over open water - also where the noise won't bother people. And hauling things up mountains usually isn't cheap regardless.

      Far more important than altitude is latitude. The boost to rockets given by Earth's spin is not insignificant.

      Even planes don't help much. A dozen or so kilometers and a few hundred meters per second is nothing compared to the needed 300-400 kilometers and 7800 meters per second (the latter taking an order of magnitude more energy to achieve than the former). That said, there are some advantages to plane launch not at all related to the altitude. One is that it lets your first stage engine be more optimized to low air pressure. Two, it avoids some energy loss to wind resistance on ascent. Three, it makes it easier to move your rocket around (if it's already designed to be plane-carried), and four it makes it easier to launch over the ocean in an equatorial location (for the reasons described above). These latter two are actually the most significant. A few rockets, most notably the Pegasus, are launched in this fashion.

      There are some scaleup problems, though. First, the rocket has to be carried somewhere on the plane. Underneath a wing imposes some ground clearance requirements, and underneath a plane altogether imposes huge ground clearance requirements (the reason why the suborbital Virgin Galactic carriers are designed in that unusual shape). Underneath a wing on a regular plane also lopsides the load on the plane and increases wing loadings. Mounting on the top of the fuselage makes launch harder. Some work has been done with carrying rockets inside the fuselage and dropping them out the back, but it imposes some significant maximum size issues.

      The second problem, and more fundamental, is that scaling up rockets from Pegasus-size quickly imposes carrier plane size requirements that become ridiculous. The world's largest airplanes already face serious engineering challenges, let alone planes designed to carry many times more. So air launch is pretty much limited to small launches. You could do larger than Pegasus, of course (higher ISP engines, larger custom-designed carriers), but not tremendously larger.

      There have been some interesting hybrid concepts proposed. For example, Black Horse / Black Colt was to work around the problem of HTOL spaceplanes facing huge loadings on takeoff by having them takeoff almost empty, meeting up with a refuelling tanker at high altitude, rapidly getting their propellant offloaded there, and then going off to space. I once did some back-of-the-napkin work on a variant that takes off with no propellant at all onboard, being towed up (with fueling lines attached) by a jumbo jet that fuels it during its ascent, to avoid having to do a midair docking on (very limited) rocket power.

      --
      The yellowcake is a lie.
    2. Re:Need to stop doing dumb things by ebvwfbw · · Score: 1

      The military didn't think so. They're launching in Colorado now. When I asked, I got way more information about just how much smarter it was to launch there than at Canaveral FL. Friend of mine's Dad was one of the founders of Goddard and really was a Rocket Scientist.

    3. Re:Need to stop doing dumb things by Rei · · Score: 1

      I don't know what "launches from Colorado" you're talking about. United Launch Alliance is *headquartered* in Colorado, but they launch from Florida. The US also has nuclear missile silos in Colorado, but they're suborbital vehicles, not orbital, and their primary location constraint is "somewhere that the enemy can't destroy us before we launch", not "the location that's optimal for minimum delta-V launches"

      The vast majority of US launches are done from far-southern, coastal sites, for the aforementioned reasons. It is certainly possible to launch inland, but it requires serious closures downrange and increases liability costs. Likewise, it's possible to launch from more northerly locations, but it costs you serious orbital energy which you have to make up with extra staging. This is the reason why the Soviets, which lacked good southern launch sites, launched so many craft into so-called "Molniya" orbits rather than GEO (it's a pseudo-geosynchronous elliptical orbit that takes less energy to achieve, particularly from northerly latitudes... the downside is that it's not actually geosynchronous).

      And to reiterate: an extra couple kilometers in height is irrelevant compared to the 300-400km for orbit, which is in turn a tiny fraction of the energy needed to reach 7800m/s orbital velocity. Ask your "friend's dad" about that.

      --
      The yellowcake is a lie.
  32. 30 years on by Anonymous Coward · · Score: 0

    In the mid-80s I was involved in the HOTOL project - a "space plane" with dual function engines for atmospheric and orbital capability. It petered out quietly. 30 years on we start again...

    1. Re:30 years on by Rei · · Score: 1

      From Wikipedia:

      Skylon is based on a previous project of Alan Bond, known as HOTOL.[10] The development of HOTOL began in 1982, at a time when space technology was moving towards reusable launch systems such as the Space Shuttle. In conjunction with British Aerospace and Rolls-Royce, a promising design emerged to which the British government contributed £2 million. However, in 1988, the government withdrew further funding, and development was terminated. Following this setback, Bond decided to set up his own company, Reaction Engines Limited, with the hope of continuing development with private funding.

      After securing more funding in the 1990s, the initial design underwent radical revision and, since 2000, Reaction Engines has been working with the University of Bristol to develop an engine design vital to the success of Skylon. The STRICT/STERN designs resulting from this programme were deemed a great success.[11] The next stage of development will be to construct a full-sized working prototype of the SABRE Engine.[12]

      There are several differences compared with HOTOL. Whereas HOTOL would have launched from a rocket sled, to save weight, Skylon uses a conventional retractable undercarriage. Skylon's revised engine design, the SABRE engine, is expected to offer higher performance.[13] HOTOL's rear mounted engine gave the vehicle intrinsically poor in-flight stability. Skylon solves this by placing engines at the end of its wings, but further forward and much closer to the vehicle's centre of mass longitudinally. Early attempts to fix this problem had ended up sacrificing much of HOTOL's payload potential, and contributed to the failure of the project.[14]

      .

      --
      The yellowcake is a lie.
  33. Cheaper regular air travel by MoarSauce123 · · Score: 1

    What the heck do we need cheaper space travel? I want to cheaper transatlantic flights so that I do not have to get a second mortgage on the house just to visit my family in Europe. Fix that, engineers!

  34. The number of self proclaimed experts on here.. by JohnStock · · Score: 1

    ...declaring with their infinite wisdom that this project wont work is embarrassing. Especially when 2 governments and 3 leading space agencies have closely looked at the project with positivity.