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First Ever Scramjet Reaches Mach 10

stjobe writes with the news that a group of US and Australian scientists successfully tested a supersonic scramjet engine in the Australian Outback on Friday. The Sydney Morning Herald reports that a rocket carrying the engine reached mach 10, and climbed to an altitude of 330 miles before the apparatus re-entered the Earth's atmosphere. "Australia's Defense Science and Technology Organization (DSTO) said it was believed to be the first time a scramjet had been ignited within the Earth's atmosphere ... Scramjets are supersonic combustion engines that use oxygen from the atmosphere for fuel, making them lighter and faster than fuel carrying rockets. Scientists hope that one day a scramjet aircraft fired into space could cut traveling time from Sydney to London to as little as two hours."

235 comments

  1. X-43A? by Chairboy · · Score: 5, Informative

    What about the X-43A? It also ignited successfully and flew under power.

    http://en.wikipedia.org/wiki/Boeing_X-43

    This is cool, yes, but the emphasis on "first" seems a bit off.

    1. Re:X-43A? by evil_neanderthal · · Score: 5, Funny

      mach 10? not fast enough! i want one for my microwave! faster pizza bagles! faster ezmac! faster! can i mount one to my pelvis! can't wait to see what the missus thinks. miss. mistress! huh? i need a gun that shoots scramjets with knives on the end! can we start calling it warp 10 instead of mach 10? they should have taped a dvd to it to set a data transfer record! we need a new unit for that! dvd-mph! gigafoot-hertz! i want the 13 gfhz model for my toaster! butter the whole toaster so it doesn't get incinerated from air friction! does it come with internet? i want one with internet! it needs bluetooth! eeeeeeee

    2. Re:X-43A? by drgruney · · Score: 1

      That was actually a typo. This uses the "cramjet" engine... not the "scramjet."

    3. Re:X-43A? by tbischel · · Score: 4, Insightful

      ...it was believed to be the first time a scramjet had been ignited within the Earth's atmosphere
      Ah I see... as opposed to the many airbreathing scramjets ignited outside earths atmosphere.

    4. Re:X-43A? by arcenal · · Score: 1

      While this engine isn't first, the x-43 wasn't first either. HyShot was the first also made by these guys. Perhaps this engine was using a different fuel than the earlier engines but the reporter just went for an easy "WORLD FIRST SCRAMJET" headline?

    5. Re:X-43A? by Gorshkov · · Score: 3, Insightful

      From my quick reading of the wiki on the X-43A you linked to, I get the impression that it only it it's scramjet at about 100,000 feet .... but TFA states that this was the first to ignite and operate it's scramjet *within the atmosphere*. I'd guess that's the difference.

    6. Re:X-43A? by Keys1337 · · Score: 1

      Maybe as opposed to in a lab? I don't really know, just guessing.

    7. Re:X-43A? by Moskit · · Score: 1
      Australians were the first to launch scramjet, although a few years ago.
      Quote from the wikipedia:

      The X-43A's successful second flight made it the fastest free flying air-breathing aircraft in the world, though it was preceded by an Australian HyShot as the first operating scramjet engine flight. (emphasis mine)
    8. Re:X-43A? by pipingguy · · Score: 1

      Eff that, I'm more worried about what kind of impact this new technology might possibly have on global climate change.

    9. Re:X-43A? by Shag · · Score: 1

      Yeah, I've been in a lot of labs with no atmosphere. ;)

      --
      Village idiot in some extremely smart villages.
    10. Re:X-43A? by toiletsalmon · · Score: 1

      That was funny as hell. Thank you...or lay off of the coffee :)

    11. Re:X-43A? by Xichekolas · · Score: 1

      This is one of those rare cases where I wish we could mod higher than +5... thanks for that, a +6 Funny in my book.

      --

      Self-referential Sigs are cool on /. these days...

      54

    12. Re:X-43A? by Arramol · · Score: 1

      Somebody scramjet this guy some ritalin!

    13. Re:X-43A? by PachmanP · · Score: 1

      i need a gun that shoots scramjets with knives on the end!
      Well not exactly a gun that shoots scramjets with knives it's a scramjet powered gun... http://en.wikipedia.org/wiki/Ram_accelerator
      --
      You're thinking small. Why miniaturize the laser, when we could instead enlarge the sharks? -John Searle
    14. Re:X-43A? by Hucko · · Score: 1

      You forgot to add it was done at a fraction of the cost of USA version.

      --
      Semi-automatic amateur armchair Australian philosopher; conjecture ready at any moment...
    15. Re:X-43A? by Anonymous Coward · · Score: 0

      Maybe they are in use already on some other planets by Klingons, Vulcans or other technically advanced aliens.

    16. Re:X-43A? by Shinmizu · · Score: 1

      Ah, you did the grad student experience, too?

    17. Re:X-43A? by Shag · · Score: 1

      Grad students at least have some eventual escape to work toward. I'm research support staff in a graduate school.

      --
      Village idiot in some extremely smart villages.
  2. "First ever scramjet" ...? by pushing-robot · · Score: 2, Informative

    From TFA: "Australia's Defence Science and Technology Organisation (DSTO) said it was believed to be the first time a scramjet had been ignited within the Earth's atmosphere."

    http://en.wikipedia.org/wiki/Hyper-X

    Is there something I'm just not getting here?

    --
    How can I believe you when you tell me what I don't want to hear?
    1. Re:"First ever scramjet" ...? by QuantumG · · Score: 0

      Other than the fact that scramjets have been under research for longer than fusion now and will continue to be forever because they're really interesting research topics and make for great research papers, but are mostly an enigma that we're unlikely to solve anytime soon.

      --
      How we know is more important than what we know.
  3. OK but... by phantomcircuit · · Score: 1

    While that is VERY cool, this particular design is mroe of a technical demonstration than an engine that could propel an aircraft.

    So while this is a big step forward, it isn't as big as it seems.

  4. Altitude of 330 miles??? by niktemadur · · Score: 1

    Holy cow, this thing can achieve Earth orbit! So why focus just on the Sydney-London thing (or to use that ol' "New Orient Express" analogy, New York-Honk Kong) instead of cheap space travel?

    --
    Lil' Thindime, lilting a lacrimose lament, krashes the kwaint konfines of Kokonino Kounty
    1. Re:Altitude of 330 miles??? by Rei · · Score: 4, Informative

      Holy cow, no it can't! Not only isn't it going nearly fast enough, but the vast majority of that delta-V came from a conventional rocket. The scramjet experiment only operated for 14 seconds.

      This is an experiment. Scramjets are still in the "data-gathering" phase, not the "let's make a realistic engine" phase, nor the "let's make a scramjet-powered craft" phase.

      --
      Everybody point at the libertarian and laugh.
    2. Re:Altitude of 330 miles??? by Lisandro · · Score: 2, Informative

      Holy cow, no it can't! Not only isn't it going nearly fast enough, but the vast majority of that delta-V came from a conventional rocket.

      Not only that, scramjets need an additional propulsion system in order to reach working speeds. Usually, yes, conventional rockets are used. This is one of the major drawbacks in these type of designs.

    3. Re:Altitude of 330 miles??? by Anonymous Coward · · Score: 0
    4. Re:Altitude of 330 miles??? by cheater512 · · Score: 1

      When you say 'most' your saying that the conventional rocket got it to 51% or higher of its speed?
      A Mach 5 conventional rocket? Cool!

    5. Re:Altitude of 330 miles??? by MikShapi · · Score: 2, Interesting

      You seem to be sharing the common misconception that LEO altitudes and above cannot be reached at low speeds.

      Dude, you can reach an altitude of 330 miles just fine with a perfectly low speed. There's nothing unphysical about it that requires the invocation of holy cows. It is also true that with the lack of a *horizontal* velocity of about mach 30 (at ~100km, you'd need less if you get as far as 330 miles high), you fall back down (well, not back to the same place, you may have traveled halfway around the world by then, but still, back *down*) like a rock. This is what spaceship-1 did, this is what this experiment did. This is what ICBM's do. This is even what proposed "2-hour-sydney-to-london" flights will do. Speed is only needed to get into low orbit.
      They go high, fast enough to stay in space for the duration of cruising their trajectory, without air resistance and at pretty dang fast speed, then they just drop back into the atmpsphere.

      Nothing to get overly excited about. The concept was already proven to work, and we haven't reached a point where the technology is generating value yet, so it's all still technological limbo. Not that it wouldn't be nice if it actually got done after 20 years of R&D. Shorter times for less fuel would pro'lly mean many more flights in lifetime of aircraft, less fuel burned, less time-in-air per trip, more in-range accessible destination for carriers and while I haven't the slightest clue as to what operational costs on scramjet-based planes would look like, it would seem to have the potential to cheapen things from where they are today.

      --
      -
    6. Re:Altitude of 330 miles??? by AaronLawrence · · Score: 1

      Isn't escape velocity something like Mach 30? Which means they are about 1/3 of the required speed. Not what I'd call close...

      --
      For every expert, there is an equal and opposite expert. - Arthur C. Clarke
    7. Re:Altitude of 330 miles??? by dbIII · · Score: 2, Insightful

      Not that it wouldn't be nice if it actually got done after 20 years of R&D.

      Oddly enough I was looking at a scramjet model at around this time in 1987. Subsequent revisions used less fuel and had other advantages - but while it's relatively cheap to do computer modelling and to build a shock tunnel to test these things at mach 8 on the ground it costs a lot to launch a rocket to get the higher speeds. It's not that surprising that it has taken over 20 years on a shoesting budget in a relatively small engineering department in Australia to get this far and get moved to a better funded organisation.

    8. Re:Altitude of 330 miles??? by gkhan1 · · Score: 1

      According to wikipedia, Mach 1 is 340.3 m/s and escape velocity from earth is 11.2 km/s. That would make escape velocity about Mach 32.

      However, remember that you don't need escape velocity to exit the atmosphere, you just need continual force upwards that is greater than gravity. Space shuttles don't come anywhere near 11.2 km/s.

    9. Re:Altitude of 330 miles??? by stjobe · · Score: 1

      Space shuttles don't come anywhere near 11.2 km/s.
      Unless 71.4% is anywhere near. 8000 m/s is in the neighborhood, no? However, at booster separation it's only travelling at 1400 m/s, so you're still on the mark as far as leaving the atmosphere is concerned.
      --
      "Total destruction the only solution" - Bob Marley
    10. Re:Altitude of 330 miles??? by tigersha · · Score: 1

      Uhm, you need to reach escape velocity if you want to escape the earth. That aircraft is going to come down again, one hopes.

      Escape veolcity is the speed you need to jut fly away without necessarily accelerating.

      --
      The dangers of excessive individualism are nothing compared to the oppressiveness of excessive collectivism
    11. Re:Altitude of 330 miles??? by gkhan1 · · Score: 1

      Yes, that is what I meant, I should have been clearer :) Space shuttles don't leave the atmosphere because they attain exit velocity, they leave the atmosphere because there is continuous thrust.

  5. NASA by jrwr00 · · Score: 1

    I can see it now, Using the power of duct tape, they will strap the scramjet to the shuttle.

    I'm guessing they will need LOTS of tape :)

    1. Re:NASA by michele15 · · Score: 1

      You think will be?

  6. Bzzzt. Wrong! by tritone · · Score: 5, Informative

    "scramjets are supersonic combustion engines that use oxygen from the atmosphere for fuel"

    Scamjets use oxygen from the atmosphere as an oxydizer unlike traditional rocket engines which need to carry their oxydizer. Scramjets still need to carry fuel.

    No. I am not a rocket scintist.

    1. Re:Bzzzt. Wrong! by AaronLawrence · · Score: 0

      Yes, makes a "small" difference doesn't it. The difference between saying "I made a better engine" and perpetual motion.
      But who cares about these tiny details.

      --
      For every expert, there is an equal and opposite expert. - Arthur C. Clarke
    2. Re:Bzzzt. Wrong! by superphreak · · Score: 1

      No. I am not a rocket scintist.
      Really? What exactly is a "rocket scintist"? Lol.

      --
      Evolution is a state-sponsored, state-protected religion.
    3. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 1, Insightful

      Bzzzt. Wrong! Using oxygen as a fuel would just mean the engine has a very large fuel supply in which it is immersed. Really handy, but nothing perpetual about it.

    4. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 1, Informative

      True, but conventional rocket engines are hydrogen + oxygen = water. But oxygen is a lot heavier than hydrogen, what with all of those extra protons, so it makes up most of the fuel. A scramjet, by weight, only needs a fraction of the fuel of a conventional rocket.

    5. Re:Bzzzt. Wrong! by khallow · · Score: 1

      Oxygen is not a fuel. It is an oxidizer. The word you're looking for is "propellant" not "fuel".

    6. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 1, Funny

      Bzzzt. GAY!

    7. Re:Bzzzt. Wrong! by Teun · · Score: 1

      You are very right.
      And just as curious is the statement that it was the first time a scramjet had been ignited within the Earth's atmosphere, because by design a scramjet doesn't carry it's own Oxygen the atmosphere is the only place it can ignite.
      All together a rather sad summary of a nice engineering feat.

      --
      "The likes of Facebook and WhatsApp are free to those whose privacy is of zero value."
    8. Re:Bzzzt. Wrong! by AaronLawrence · · Score: 1

      Except of course it's impossible to use oxygen by itself as a fuel.

      --
      For every expert, there is an equal and opposite expert. - Arthur C. Clarke
    9. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 0

      No. I am not a rocket scintist.
      Really?
      What exactly is a "rocket scintist"? Lol. Really? Did you actually laugh out loud?
    10. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 0

      That's a terribly earth-centric view. What's so special about oxygen?

    11. Re:Bzzzt. Wrong! by heinousjay · · Score: 1

      It smells nice.

      --
      Slashdot - where whining about luck is the new way to make the world you want.
    12. Re:Bzzzt. Wrong! by khallow · · Score: 1

      It grabs electrons. I should have mentioned that. Fluorine is also an oxidizer.

    13. Re:Bzzzt. Wrong! by Breakfast+Pants · · Score: 1

      Are you serious? We've been flying these around Venus for years.

      --

      --

      WHO ATE MY BREAKFAST PANTS?
    14. Re:Bzzzt. Wrong! by sasdrtx · · Score: 1

      I'm rather surprised it took so long for somebody to point out this flagrant display of ignorance. It indicates to me that the article isn't worth reading, because if they can't get the fundamentals right, they very likely aren't going to get anything else right.

      --
      Most people don't even think inside the box.
    15. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 0

      Your mom has been flying around venus for years.

    16. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 0

      Really? Did you actually laugh out loud?
      You have to remember that many people around here don't actually have lives, so to them something as simple as a misspeling or ty[po would be cause for great hilarity.
    17. Re:Bzzzt. Wrong! by Anonymous Coward · · Score: 0

      carry it's own

      "its".

    18. Re:Bzzzt. Wrong! by Teun · · Score: 1

      Sorry!
      Won't happen again Ma'm.

      --
      "The likes of Facebook and WhatsApp are free to those whose privacy is of zero value."
  7. Not for me by stinerman · · Score: 1

    I don't know about traveling that fast. If you do it enough the time dilation might make it that my friends and family would die a few seconds sooner (relative to me of course).

    </sarcasm>

    1. Re:Not for me by Dersaidin · · Score: 1

      Or would you live a few seconds longer?...

    2. Re:Not for me by MemoryAid · · Score: 1
      There are some quantum effects that cancel out the time dilation thing. While you are travelling at hypersonic velocities, your death is much more likely; in fact, you are both alive and dead at the same time, in proportion to the appropriate actuarial table. When you slow back down, that dual state resolves itself into one or the other. Statistically speaking, it evens out pretty well with the extra seconds you may gain at the end.

      That's just the theory, though. In practice, you are much more likely to die in a fireball.

      --
      Language students: Don't try to learn English here. This ain't it.
  8. Why was the altitude changed? by thesolo · · Score: 5, Insightful

    This event took place in Australia, and was reported by an Australian paper; therefore, it was correctly reported in the metric altitude of 530 kilometres.

    So why was the summary changed by slashdot editors to the imperial unit?

    Firstly, not everyone who reads this site is American, and secondly, this is an audience of nerds. I think we can handle kilometres! Even the USA's NASA is all metric now.

    The scientists who developed this scramjet used metric, the country it was tested in used metric, the newspaper that reported it used metric, so how about we keep it that way?

    1. Re:Why was the altitude changed? by Anonymous Coward · · Score: 2, Insightful

      Don't forget, this was the country that elected George Bush. They're only comfortable with simple things, thinking confuses them.

    2. Re:Why was the altitude changed? by drgonzo59 · · Score: 4, Funny

      And besides we all know that God uses the imperial system and only communists use metric...Hail Bush!

    3. Re:Why was the altitude changed? by earlymon · · Score: 0

      uh, maybe because a good many of us learned that 62 miles meant space, that Yuri Gagarin orbited above 180 miles, that Friendship 7 made a 120 miles, and that until we're talking parsecs, it's all just noise?

      --
      Pathological kinda promises Path + Logical - but instead, you get stuck with pathetic.
    4. Re:Why was the altitude changed? by timmarhy · · Score: 0, Troll

      do you have a fucking point? learn metric you backwards country

      --
      If you mod me down, I will become more powerful than you can imagine....
    5. Re:Why was the altitude changed? by rafaMEX · · Score: 1

      thesolo , now you have replays saying the metric is more complicated lol, why 1 meter == 1,000 kilometer or 1,000 mm == 1 meter how is that more complicated ? lolz :P

    6. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      What's even worse is that Americans don't even use Imperial units.
      They use their own half baked system consisting of some of the same names, and completely different measurements that they have the audacity to call English. As if it were the Queen's fault or something.

    7. Re:Why was the altitude changed? by foniksonik · · Score: 1

      why should we, when Google does conversions... is it really important what measurement system is used as long as it is consistent?

      --
      A fool throws a stone into a well and a thousand sages can not remove it.
    8. Re:Why was the altitude changed? by Gryle · · Score: 1

      Most Americans refer to it as measurement system as "Customary" or "Traditional" rather than "English".

      --
      Only two things are infinite, the universe and human stupidity, and I'm not entirely sure about the universe - Einstein
    9. Re:Why was the altitude changed? by Gryle · · Score: 0, Offtopic

      do you have a fucking point? learn metric you backwards country
      We'll learn the metric system when you learn the proper rules of capitalization and punctuation. Do we have a deal? :)

      --
      Only two things are infinite, the universe and human stupidity, and I'm not entirely sure about the universe - Einstein
    10. Re:Why was the altitude changed? by earlymon · · Score: 1

      do you have a fucking point?

      no, other than that maybe quibbling over units of measure accomplishes nothing, and that the real measure of the accomplishment is not diminished by a conversion factor. i didn't fully realize that there could be a real reaon for the complaint over the change from km to mi other than the guy having a bad day. what one system accompishes over another is meaningless for some of us that have worked space-based systems - conversion tends to be a rather automatic process when you think globally.

      learn metric you backwards country

      and perhaps i'll learn to be less subtle as well - thanks!

      btw- thanks for the promotion to country; fortunately, it won't require me to buy larger asbestos underoos

      ps - you misspelled Système International d'Unités (SI) base units as metric - are we all happy now?

      --
      Pathological kinda promises Path + Logical - but instead, you get stuck with pathetic.
    11. Re:Why was the altitude changed? by cheater512 · · Score: 1

      Its a American website.

      From my experiences they are very bad at converting anything.
      Timezones, Metric -> Imperial, etc...

    12. Re:Why was the altitude changed? by cheater512 · · Score: 1

      Yeah sure. Now I insist everyone counts in hexadecimal since computers do it and its consistent. :)

    13. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      Actually, NASA isn't all metric yet. Perhaps officially, they claim to be using metric, but internally, a lot of engineers are still using whatever they want. As a result, NASA uses a mix of imperial and SI units (and the nautical mile also, which isn't an official SI unit.)

    14. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      From my experiences they are very bad at converting anything.

      If you're so superior at converting, convert the miles to kilometers in your head and you have nothing to complain about.

      Personally, I convert just fine, and thus usually don't give it a passing thought when something is miles or kilometers.

      While I prefer the kilometer for its conversion ability, it is naive to pretend that the mile is an eccentric unit. This is the internet, and we are speaking in English. A quick check of googlefight shows that "miles" is written 10 times more often than "kilometers". So use your intellect and convert.
    15. Re:Why was the altitude changed? by Anonymous Coward · · Score: 5, Insightful

      England invented proper rules of capitalization and punctuation, and they officially use the metric system now. Is there any country other than the US which doesn't? (According to Wikipedia two other countries actually do; Liberia and Myanmar. Great company.)
      Not to mention that the US has been butchering proper English spelling and grammar ever since Webster. Just switch to Metric measurements and the Celsius temperature scale already. The rest of the world is getting tired of having to convert measurements for the sole purposes of dealing with the US. [/troll]

    16. Re:Why was the altitude changed? by Chibi+Merrow · · Score: 2, Funny

      So why was the summary changed by slashdot editors to the imperial unit?


      Mostly just to piss people like you off.
      --
      Maxim: People cannot follow directions.
      Increases in truth directly with the length of time spent explaining them
    17. Re:Why was the altitude changed? by Heir+Of+The+Mess · · Score: 4, Informative

      You missed another Americanisation. It's Defence Science and Technology Organisation. Check their website http://www.dsto.defence.gov.au/. Not everyone uses Americanised spelling.

      --
      Australian running a company that does C# / C++ / Java / SQL / Python / Mathematica
    18. Re:Why was the altitude changed? by Fred+Ferrigno · · Score: 1

      Really? Seems to me that most people don't have a name for it at all. It's not something commonly referenced, so I can't imagine any term that I'm confident would be interpreted correctly consistently. Normally you'd just say the specific unit you were talking about. "Is that in meters or feet and inches?" Also you might identify something in terms of not being metric.

    19. Re:Why was the altitude changed? by Rufty · · Score: 1

      Strawman. Miles fails the googlefight against "km"

      --
      Red to red, black to black. Switch it on, but stand well back.
    20. Re:Why was the altitude changed? by Down8 · · Score: 1

      Bad translation - "standard or metric?" is the question often asked....

      -bZj

      --
      .sig
    21. Re:Why was the altitude changed? by jac89 · · Score: 1

      Oh England claims to use the metric system. However if you drive down any road in England, what unit of distance are the road signs in? Miles.. What units of speed are the speed limits in? Miles per hour... Loads of the English still use the 'stone' (14 pounds) to measure their weight. People won't change the units that they are used to, unless they are forced to. In France they made Imperial units illegal, it worked, the French now use Metric units. However isn't that a bit overkill? As long as people are familiar with both systems they can choose which they prefer. I agree there is a need for consistency in the scientific community. This already exists, they use the Metric system. For the simple layman, why force a change? Imperial units work, Metric units work. You can argue one may be easier than the other, but is it easier to learn a new system than stick with what you know? There are tons of easily available methods of conversions. I say let it be.

    22. Re:Why was the altitude changed? by haraldm · · Score: 1
      Maybe this is the New World Order.

      The SRP (*) trying to dominate everything, and the thoughtlessness of some of their inhabitants, makes me sicker every day. No this is not a troll post or a flamebait, I'm just worried.

      (*) Single Remaining Superpower

      --
      open (SIG, "</dev/zero"); $sig = <SIG>; close SIG;
    23. Re:Why was the altitude changed? by mpe · · Score: 1

      What's even worse is that Americans don't even use Imperial units.
      They use their own half baked system consisting of some of the same names, and completely different measurements that they have the audacity to call English. As if it were the Queen's fault or something.

      They are the units used in the 18th century which predate the Imperial standards. The most notable difference is with volume measurement. An interesting piece of trivia is that both inches were redefined to be exactly 25.4 mm in the 1940's so when it comes to measuring length metric is already widely used.

    24. Re:Why was the altitude changed? by mpe · · Score: 1

      Not to mention that the US has been butchering proper English spelling and grammar ever since Webster.

      Thank's Noah... You also find this happening with proper nouns which is a definite faux pas.

      Just switch to Metric measurements and the Celsius temperature scale already.

      But would the units actually get spelt correctly?

      The rest of the world is getting tired of having to convert measurements for the sole purposes of dealing with the US.

      Probably mostly the Mexicans and Canadians. On the other hand does the rest of the world actually want to deal with the US :)

    25. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      In 3 years in the stress analysis world of Space Shuttle SRBs, I don't recall ever seen a non-standard unit. Loads in lbs, stress/moduli in psi (or, often, loads and stress/moduli in the hybridized kips and ksi).

      How many of those who make noise about SI vs standard bother to differentiate between SI and binary prefixes (kibi = 1024, kilo = 1000)? That's what I thought. Now everybody calm down, and rejoin me in drooling over the scramjet.

    26. Re:Why was the altitude changed? by lhbtubajon · · Score: 1

      Even bigger strawman.

      "km" fails the googlefight against "mi".

      You can't go comparing an abbreviation to a non-abbreviation and then try to pretend they're the same.

      And, by the way, "mph" destroys "kph" by over 14x.

    27. Re:Why was the altitude changed? by foniksonik · · Score: 1

      Th point is that everyone can use whatever system of measurement they want... as long as a consistent conversion exists.

      How about 330 miles in parsecs?

      or in hands

      --
      A fool throws a stone into a well and a thousand sages can not remove it.
    28. Re:Why was the altitude changed? by bogjobber · · Score: 1

      Well the US "officially" uses the metric system also, and has for about 140 years. Congress made it the "preferred" method in 1975. The only problem is that no one payed attention to Congress and standard is still used for everything outside science/education and industry. It's actually quite similar to what has happened in the UK, just to a different degree.

      As for "proper" English spelling and grammar, get over it. We're not English, and haven't been for 230 years. Languages evolve. Pull the stick out of your ass and move on.

    29. Re:Why was the altitude changed? by A+Holstenson · · Score: 1

      Ah yes, but by converting from 530 km to 330 miles and back again you've just lost some accuracy. 330 miles rounds to 531 km. And 530 km should have rounded to 329 miles.

      The fact is that they should have given the altitude in feet, as almost every altitude in aviation is given in that unit. The Russians use the metric system for their altitudes, but they are pretty much alone.

      An altitude of 530 km converts into 1 738 845.14 feet. I would probably round it to 1 700 000 feet, because the measurement is not accurate to begin with and there is no indication if it is a geometric or a pressure altitude.

      In this case the accuracy and unit doesn't really matter, but that is not always the case.

    30. Re:Why was the altitude changed? by phantomfive · · Score: 1

      Different countries use the metric system to different degrees. El Salvador uses kilometers for measuring distance on the road, but pounds for weighing things. When I was in Scotland last month people were talking about their weight in stones. In the US, for some purposes the metric system is used, for example, calculating the trajectory of probe going to Mars. Personally I think Farenheight is much easier to use for measuring weather, but clearly celcius is better if you happen to be interested in the boiling point of water. Kelvin sucks for weather, but is obviously useful for some things; but that's just my opinion after using both C and F for a number of years.

      --
      Qxe4
    31. Re:Why was the altitude changed? by bar-agent · · Score: 0, Troll

      Just switch to Metric measurements and the Celsius temperature scale already.

      Your Moms switched to Celsius. So now instead of a 90F hot MILF, she's a 90C torrid slut and gives you 13 venereal diseases if you just look at her sideways. She also switched from pounds to kilograms, so we're talking Jabba the Hutt here.

      Nothin' personal man, I'm just sayin' the metric system ain't for me. But hey, if that's your thing, go ahead and hit it...

      --
      i'd hit it so hard, if you pulled me out you'd be the king of britain [bash.org]
    32. Re:Why was the altitude changed? by codemachine · · Score: 1

      How is Farenheight better for weather? I don't see any advantage there at all.

      In many climates, it is the freezing point of water that is important. Having that be the 0 degree is fairly handy for weather. Above and below 0 is then equivalent to above or below freezing, and we get a temperature range of around -40 to +40 (neither extreme is fun). Above or below 32 seems a bit arbitrary.

    33. Re:Why was the altitude changed? by phantomfive · · Score: 1

      It is easier to get a feel for temperatures with farenheight. For example, 72F and 74F are roughly the same, and so it is easy to know that I feel comfortable in the 70s, kind of warm in the 80s, and dying when it's above 100F. Celcius on the other hand, go from 20C to 25C and that's a huge difference. above 28 and you are already burning up, and below 17 and it's a bit chilly. It's just easier to fit weather temperatures into your mind, and get a feel for what a different temperature is. Also, a single degree farenheight is about the smallest change in ambient temperature that the human body can detect, thus reducing the need for fractional measurements. That is my experience after using both of them, although looking at wikipedia (entry under farenheight), there are other people who feel the same.

      --
      Qxe4
    34. Re:Why was the altitude changed? by shaitand · · Score: 1

      'Firstly, not everyone who reads this site is American'

      And we welcome our guests. Just the same, this is an american site for americans. If I start reading a german blog I'm not going to complain if they have the nerve write the articles in german despite having some americans in the audience.

    35. Re:Why was the altitude changed? by shaitand · · Score: 1

      Variations in C seem to be too large to me. Using F standard gets a weather variation of anywhere from -40 to 104, using your -40 to 40, I'd put a real world range of -20 to 120, that gives standard 144 degrees of precision without resorting to fractions and metric only 80. Since real people don't say its 70.345 degrees out that gives standard greater precision in practice.

      When you adjust a thermostat, one degree F is a fairly large temperature adjustment. Adjusting my AC from 77 to 78 degrees reduced my electric bill by about $5/month and made a comfort difference that required a couple weeks of adjustment. How would you adjust 25C to 25.5555556C on your thermostat? Do metric thermostats show partial fractions of variation?

    36. Re:Why was the altitude changed? by Tickletaint · · Score: 1

      That's because nobody writes "kph"; the more common abbreviation is "km/h." Of course, "mph" still wins, probably due to rural Americans' obsession with motoring. (I personally have nothing against imperial units, mind you.)

      --
      Make Slashdot readable! See journal.
    37. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      You mean Americanized spelling!

    38. Re:Why was the altitude changed? by evilviper · · Score: 1

      How is Farenheight better for weather? I don't see any advantage there at all.

      You only need to use 2 digits the vast majority of the time, and usually don't need to go into negatives. In addition the precision is just right, precise enough for what people want to know, without requiring a decimal place, which, when you start using, you have the burden of accuracy down to 1/10th of a degree...

      The same can be said for at least a few other imperial measurements... Inches, feet, gallons, etc., they just happen to match real-world scenarios very often. With large measurements like km/kelvin/tonne/etc., I suppose it really doesn't matter, as long as you have a point of reference.
      --
      Slashdot gets worse every day... Pipedot: News for nerds, without the corporate slant
    39. Re:Why was the altitude changed? by argStyopa · · Score: 1

      "This event took place in Australia, and was reported by an Australian paper; therefore, it was correctly reported in the metric altitude of 530 kilometres.
      So why was the summary changed by slashdot editors to the imperial unit?
      Firstly, not everyone who reads this site is American, and secondly, this is an audience of nerds. I think we can handle kilometres! Even the USA's NASA is all metric now.
      The scientists who developed this scramjet used metric, the country it was tested in used metric, the newspaper that reported it used metric, so how about we keep it that way?"

      Oh noes! We've confused the foreigners agin!

      Why do you care?

      Slashdot is, last time I checked, based in the US. So if they want to change their summaries to imperial units, and that really, really bothers you - don't read it? No, not everyone who reads the site is American. But IIRC most of the guys that write it, ARE. If you can't figure out from that why it was converted, well, starting your own site would be an option.

      --
      -Styopa
    40. Re:Why was the altitude changed? by lhbtubajon · · Score: 1

      Didn't know that. Thanks.

      As for rural Americans, I don't think they have much choice. Perhaps you mean "suburban?" Even then, unless you're within the sprawl of a major city, you don't have much choice in the U.S. "Obsession" has little to do with it when the main issue is "necessity."

    41. Re:Why was the altitude changed? by bar-agent · · Score: 1

      (Score:1, Troll)

      Is it at least a funny troll? Because that's what I was going for. :)

      --
      i'd hit it so hard, if you pulled me out you'd be the king of britain [bash.org]
    42. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      I'm in BC near the southern border, and these are my observations: In science contexts people use full metric. On the road people use meters and litres. For the height of an individual, people absolutely use feet. For the weight of an individual, people almost always use pounds. People use kilometers for lengthy walkable distances, but feet for shorter ones. When it's to do with dimensions it's usually inches and feet (and you don't really have a choice because things are done with common fractions of an inch). Cooking usually involves cups, but food involves grams and drink involves millilitres (except for non-canned beer). I still don't know what an ounce is, but I should. Temperature outside is in Celsius, but it's probably Fahrenheit inside an oven.

      I'd rather use full metric to make conversions easier, but I have to interface with other people so it isn't really a choice. Also, everyone, including me, have a sense of feet and pounds for measuring people.

      To say Canada is metric without qualifying it is highly misleading. I imagine things are the same throughout all large cities in Canada, although I haven't verified it.

    43. Re:Why was the altitude changed? by emilper · · Score: 1

      if we make learning English in school mandatory, would you convert to the metric system ? It's kind of difficult to know when to use "the" and when not to use is, and having to know when to multiply by 12, or by 14, or by 6 etc. to get to the next division is ... well, dealing with the measuring system used in US and UK is like playing Dragon Poker.

    44. Re:Why was the altitude changed? by Rufty · · Score: 1

      Hmm, lemme see. First page of google hits on "mi" Michigan and MI5. Nothing about distance.
      Better disguise, but still a strawman.

      --
      Red to red, black to black. Switch it on, but stand well back.
    45. Re:Why was the altitude changed? by lhbtubajon · · Score: 1

      First page google search on "km":

      knowledge management
      kings mission
      kernel management

      Oh, and ONE instance of "kilometre" (the Wikipedia entry).

    46. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      Huh? If you had a old digital thermostat, you'd choose 25C or 26C... if you have a modern one you usually have half or quarter degree increments, and if you have a analog thermostat control, you don't have that problem. We usually heat our house to about 16C during winter (on days below 10C), and cool it to about 28C in summer (on days above 34C). I don't consider a single Celsius degree difference to be significant, and are surprise that you'd consider a smaller F step to be a fairly large amount.

      Right now it is 11C in my house, 7C outside. It is nearly 1pm. If it drops below 10C inside, I might turn the heater on, or I might put some gloves on.

    47. Re:Why was the altitude changed? by shaitand · · Score: 1

      'Right now it is 11C in my house, 7C outside. It is nearly 1pm. If it drops below 10C inside, I might turn the heater on, or I might put some gloves on.'

      My god. I would never consider letting my home get so warm or cold that I had to wear outside clothing like gloves or a jacket.

    48. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      It's easier for you because you are used to the old imperial units.

      I hear "72 degrees" and think "What the hell. You'd be burning up".

      Also, how is it an advantage that "72F and 74F are roughly the same". 22C and 23C are roughly the same too.

      Celsius is pretty damn easy. 21C to 24C are comfortable "room temperature". 30 is a hot day, 15 is a cold day. 0 is freezing, 100 is boiling.

    49. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      I certainly can't tell the difference between 22C and 23C on my air conditioning.

      25C would be a bit too warm, though. 22C to 24C are the usual settings that people use.

    50. Re:Why was the altitude changed? by Anonymous Coward · · Score: 0

      For most people, putting on the heater or air conditioner is a big deal. We have debates at our house all the time about whether it's "heater weather" yet. Just turning on climate control for the hell of it is environmentally irresponsible.

      Of course, if you are in some sort of apartment with a central boiler, you might have a radiator on all the time. But most people aren't.

      And we don't even think about turning on the air conditioning here until it gets to around 35 degrees celsius.

    51. Re:Why was the altitude changed? by shaitand · · Score: 1

      'Just turning on climate control for the hell of it is environmentally irresponsible.'

      hmm, well I honestly couldn't give a fig about the environment. But I do care about my electric bill, maintaining a reasonable constant temperature uses less energy than letting the temp get to an extreme and then trying to reign it in.

      'Of course, if you are in some sort of apartment with a central boiler, you might have a radiator on all the time. But most people aren't.'

      News to me. Once when I was a kid I lived in an apartment with separate units in the bedrooms. That was in government provided housing. Cost a fortune to run them as I recall. Outside of that, I haven't seen anything but central air and heat in apartments and houses. Maybe its a geographical thing? You are using C so I take it you aren't in the states...

  9. Suborbital trajectories? by caseih · · Score: 5, Interesting

    This is very interesting to read as I just finished reading Ben Rich's book "Skunk Works" where he talks about the SR71. When president Reagan announced the administration's intention to build a hypersonic airplane, he just shook his head. It's simply not practical, with or without the scramjet engine. The SR71 flew at 85,000 feet at about Mach 3.2, and reaches skin temperatures of 2000-3000 degrees (F I presume) just from moving through the atmosphere. Accelerating to Mach 10 would burn up or otherwise compromise any current building material, except for the carbon-carbon and ceramic materials used on the space shuttle's heat shield, but aren't practical for airplanes. So what good is this scramjet, at least as far as a hypersonic airplane goes? Seems to me all this talk of Sydney to London in 12 hours is a bit fanciful. So the question is, how exactly will this engine be used to accomplish this? The only way to reach hypersonic speeds without burning up is to make the trajectory sub-orbital so that the aircraft is in the thinnest atmosphere possible when it's firing it's engines to go Mach 10. But of course there's not a lot of oxygen at that altitude. And to really achieve sub-orbital trajectory you need a rocket engine, not any kind of air-breathing engine. So my questions are: Is Ben Rich right that hypersonic travel is essentially impossible? Will the scramjet help with a suborbital trajectory? I understand that igniting the scramjet is a breakthrough. Jet turbines at supersonic velocity have always been problematic.

    Off-topic, Ben Rich says in his book that the codename Aurora that everyone likes to think refers to some hypersonic aircraft, was actually the codename placed on the B-2 project as Lockheed and Northrop were competing for the contract. It's funny to think that to this day, folks still hang onto this and imagine some mythical hypersonic airplane. Which never existed. Or does it?

    1. Re:Suborbital trajectories? by caseih · · Score: 1

      Ahem. Sydney to London in 2 hours.

    2. Re:Suborbital trajectories? by richdun · · Score: 2, Informative

      Technically speaking, yes, hypersonic travel will always be impossible, barring some super-material able to take the heat. The trick is that once you get out of the atmosphere, a term like "hypersonic" is nonsensical. The speed of sound in a vacuum approaches a theoretical infinity, so to reach it, let alone top it by a factor of 7 or more, would be nonsense (unless, of course, your name is Brannon Braga! *rimshot*)

      Often, though, for simplicity sake, we use terms like "mach 10" to mean mach 10 at sea level or some other decently benchmarked altitude.

    3. Re:Suborbital trajectories? by Rei · · Score: 5, Insightful

      All of his points are basically correct in the present day. However, the most critical one -- the expense of heat-resistant materials -- may only be temporary. It's hard to say. Carbon fiber was once the "we'd love to use it, but it'd be too expensive except for pricey custom luxury jobs" material for airplanes. Now look at the Dreamliner -- a mass-produced majority-carbon-fiber giant by Boeing, which despite delays, companies have been snapping up.

      I wouldn't rule out the concept of hypersonic travel just because heat resistant materials are expensive today. If the rest of the tech is there and is affordable, and there is sufficient demand... who knows? The airline industry is bloody huge and there is lots of money to be made by faster travel, so it could draw a lot of R&D money if the other tech looks good.

      --
      Everybody point at the libertarian and laugh.
    4. Re:Suborbital trajectories? by richdun · · Score: 2, Interesting

      Er, it's the night for corrections - the speed of sound in a vacuum approaches a theoretical asymptote, not infinity. The speed of sound generally gets lower as the material loses density, higher as the material gains density (think about a wave traveling through a solid block, as opposed to one traveling through water, then one traveling through the air)

    5. Re:Suborbital trajectories? by Anonymous Coward · · Score: 0

      You could make it out of Unobtanium.

    6. Re:Suborbital trajectories? by khallow · · Score: 1

      I think you ignore several things. First, I think regenerative cooling (using the fuel to absorb the excess heat) has progressed since the days of the SR71. So my take is leading edge surfaces will take a higher thermal load. Second, why not fly higher? I understand that thermal heating is still a problem at higher elevations merely because there's less atmosphere to transfer the heat to, but the less atmosphere there is, the less heat that your fuel needs to absorb. Finally, I figure the Shuttle is a demonstration that ceramics and similar materials can be used on an airplane. After all, that is what the Space Shuttle is (well, a crude glider) when it is reentering Earth's atmosphere.

    7. Re:Suborbital trajectories? by Anonymous Coward · · Score: 0

      Ceramic tiles?

      Uh, Columbia much?

      Why not just make plane out of O-rings FFS.

    8. Re:Suborbital trajectories? by Anonymous Coward · · Score: 0

      NASA investigates scramjets for the same reasons they do all their other basic research: the hope that future projects will be based on knowledge learned, whether those projects are foreseeable or not.

    9. Re:Suborbital trajectories? by dbIII · · Score: 1

      It is useful because multi-stage rockets that don't need as much propellant to lift the same amount of stuff to the same height and the same speed can carry more stuff. Forget the Buck Rodgers spaceplane the journalist threw in to flesh out the article, it's no more relevant than the little submarines in people's blood that get brought up in nanotech articles.

    10. Re:Suborbital trajectories? by Anonymous Coward · · Score: 1, Interesting

      There's also the problem that a hypersonic aircraft would sustain heating for a lot longer than the shuttle does. Passive heat shield material probably isn't going to cut it. (Incidentally, there's been some interesting work done on titanium alloy heat shields...)

      Almost any serious hypersonic proposal includes active cooling, using cryogenic fuel to cool the leading edge (which is the only part that's problematic; passive materials can handle the rest). It'd certainly make me nervous to ride in a vehicle that requires an active cooling system to work perfectly to avoid burning up, but it could solve the problem.

    11. Re:Suborbital trajectories? by mduell · · Score: 2, Informative

      Now look at the Dreamliner -- a mass-produced majority-carbon-fiber giant by Boeing, which despite delays, companies have been snapping up.

      I think you're confusing the Dreamliner with the WhaleJet.... Dreamliner hasn't had any delays.

    12. Re:Suborbital trajectories? by mpe · · Score: 1

      The only way to reach hypersonic speeds without burning up is to make the trajectory sub-orbital so that the aircraft is in the thinnest atmosphere possible when it's firing it's engines to go Mach 10.

      It still needs to get to that altitude first, flying at a speed which will generate a suitable amount of aerodynamic lift.

    13. Re:Suborbital trajectories? by mpe · · Score: 1

      Almost any serious hypersonic proposal includes active cooling, using cryogenic fuel to cool the leading edge (which is the only part that's problematic; passive materials can handle the rest). It'd certainly make me nervous to ride in a vehicle that requires an active cooling system to work perfectly to avoid burning up, but it could solve the problem.

      You also need reusable tanks to store the fuel and cryonic fuel handling at all the airports you want to use. AFAIK no such tanks currently exist.

    14. Re:Suborbital trajectories? by mpe · · Score: 1

      Technically speaking, yes, hypersonic travel will always be impossible, barring some super-material able to take the heat. The trick is that once you get out of the atmosphere, a term like "hypersonic" is nonsensical.

      Once you get out of the atmosphere you need a rocket engine to provide any thrust you might need to alter your course. If you want to make quick climb through the atmosphere you need a thrust to weight ratio considerably greater than unity as well as a way to package passengers and cargo which allows for 2-3G in the direction of the tail.

      Possibly a more useful application of scramjets would be to propel a plane at a more modest mach 2-3. A problem with both the Concorde and TU-144 is that the air flowing into the engines cannot be supersonic, regardless of the airspeed.

    15. Re:Suborbital trajectories? by khallow · · Score: 1

      Columbia flew successfully 27 times before the accident. And that there's been four other Shuttles all which have successfully flown (even Challenger flew 9 times successfully before its fatal accident).

    16. Re:Suborbital trajectories? by mpe · · Score: 1

      Finally, I figure the Shuttle is a demonstration that ceramics and similar materials can be used on an airplane.

      You'd undoubtely want a mechanism to detect a bird strike (or similar) to the leading edge of the wing.

    17. Re:Suborbital trajectories? by Firethorn · · Score: 1

      27 & 9 missions? So what? That's still way, way, way too low for any manned commercial flight system, one involving civilian passangers* to boot?

      A quick check shows ~115 missions to date with the shuttle. Two of which were failures with 100% fatality rate. That tends to suggest to me that there's a 1-2% chance of dying on any given shuttle launch.

      With that failure rate, your standard commercial aircraft would be lucky to last a month. Any 'extreme sport' with that fatality rate would be banned; any dealers sued into oblivian.

      *I know many NASA astronaughts are civilians, but they should at least know the risks, facing heavy competition to ride a rocket into space.

      --
      I don't read AC A human right
    18. Re:Suborbital trajectories? by Anonymous Coward · · Score: 0

      I don't think bird strikes are a big worry at 85,000 ft.

      Granted, you'd want to know about them at lower altitudes, but at that point you'd be going at the kinds of speeds we've been doing for a while now. I suspect this is a known/solved problem.

    19. Re:Suborbital trajectories? by mindstrm · · Score: 1

      The speed of sound in a gas varies with temperature... not density.

    20. Re:Suborbital trajectories? by Sinical · · Score: 1

      Off-topic, Ben Rich says in his book that the codename Aurora that everyone likes to think refers to some hypersonic aircraft, was actually the codename placed on the B-2 project as Lockheed and Northrop were competing for the contract. It's funny to think that to this day, folks still hang onto this and imagine some mythical hypersonic airplane. Which never existed. Or does it?

      I work with a bunch of former B-2 folks, and they've *never* mentioned this. I'm guessing it would have come up.
    21. Re:Suborbital trajectories? by khallow · · Score: 1

      27 & 9 missions? So what? That's still way, way, way too low for any manned commercial flight system, one involving civilian passangers* to boot?

      Nah, 0 times per vehicle is too few. A manned system is viable on 1 launch per vehicle (ie, an expendable launch system), just as long as there're plenty of vehicles.
    22. Re:Suborbital trajectories? by Firethorn · · Score: 1

      Of course, the trick here is that the shuttle isn't billed as 'disposable' or 'one use', and right now it's sitting at a 2% cooked kibbly rate, of which 50% has you spread across three states on return...

      I'm a fan of returning to disposable reentry pods, such as what we used successfully before the shuttle, and the Russians still use.

      Of course, my idea is that cargo is lifted by cargo rockets, people are lifted in a dedicated people system*, work is done in a space station, and you bring back as little as possible in favor of eventually implimenting recycling technologies at the space station.

      *IE no SUV like shuttle

      --
      I don't read AC A human right
    23. Re:Suborbital trajectories? by smellsofbikes · · Score: 1

      Probably nobody will ever read this, but I had a nice long chat one time with an engineer who worked for NASA and was a fairly high-ranking officer in the USAF as well. He was working on the National Aerospace Plane and he felt that the leading-edge materials were not overwhelmingly difficult to solve. They were doing a lot of work with carbon-carbon matrix stuff that forced carbon out -- bled it -- to form continuously ablating surfaces, and had some neat systems for forcing hydrogen slush, a mixture of solid and liquid hydrogen, through the surfaces to simultaneously cool them and vaporize the slush for use in the fuel system. They were more concerned about stability and the ability to get the thing to produce thrust at zero velocity so it could take off, than they were with the craft burning up.

      By the way, not that any of us know what we're talking about, but a lot of the people talking about the Aurora are claiming it has some sort of pulse-jet or non-steady-state engine, based on visual sightings and pictures of the contrails. I've seen something, well before I read about this, that fit the descriptions I've since read of an aircraft with a non-steady-state jet engine, although I have no idea what it was. If the Aurora was the B-2, then there's likely something else out there that military plane spotters are calling the Aurora now.

      --
      Nostalgia's not what it used to be.
    24. Re:Suborbital trajectories? by khallow · · Score: 1

      I'm a fan of returning to disposable reentry pods, such as what we used successfully before the shuttle, and the Russians still use.

      Capsules are an excellent and economical way to return to Earth. My take is that winged designs still can be viable. Frankly, the Shuttle was rendered expensive more by its low launch frequency rather than the unwieldiness of the technology. My take is that its launch costs would have more than halved per launch if it could have achieved the 40 launches per year rate that they originally wanted for the vehicle. Even if that meant (and it probably did) building more launch vehicles.
    25. Re:Suborbital trajectories? by Firethorn · · Score: 1

      My take is that its launch costs would have more than halved per launch if it could have achieved the 40 launches per year rate that they originally wanted for the vehicle.

      The problem with the space shuttle is that they attempted to reach a bit too far; they wanted the shuttle to be everything. A dedicated people mover would have been able to match the shuttle's capacity and still cost an order of magnitude less, a dedicated set of cargo lifters would have the same effect. The end result is that the shuttle is like an SUV: Capable of many things, but ultimately more expensive and less safe than the alternatives.

      The people mover could be a winged design, but they should go back and do it using updated materials. We've come quite a way material-science wise than when the shuttle was produced.

      --
      I don't read AC A human right
  10. ICBM by Anonymous Coward · · Score: 0

    ScrambleJet = ICBM
    Nothing like a dinkum Aussie WoMD.
    Aussies are evil !!!

  11. Oxygen by mixtape5 · · Score: 1

    "uses oxygen" oxygen in space O.o?

    --
    WoW: Scheod 70 orc warlock on Shadowmoon
  12. four words by Jbcarpen · · Score: 0
    Sonic Boom From Hell.

    Thank you.

    --
    GENERATION 667: The first time you see this, copy it into your sig on any forum and add 1 to the generation
  13. Obligitory Spinal Tap joke: by rts008 · · Score: 1

    Sooo...it only goes to 10.

    This one goes to 11!

    Okay, now my funny bone has been buried....

    Kudos to these people. It may have only been for some seconds, but at least they are forging onward, and I salute their work!

    Proving theory is usually no easy task, a working prototype seems to be 3/4 of the battle.

    Seriously, hat's off!!!

    --
    Down With Slashdot BETA!!! I've been around the corner and seen the oliphant; you can only abuse me from your perspecti
  14. 330 miles is well beyond the Kármán line by eyebits · · Score: 4, Informative

    330 miles is approximately 5 times the minimum altitude for entry into "space." The Kármán line is at an altitude of 62 miles (100 km) which is the boundary that defines where space begins. 75 miles is where atmospheric drag starts to have an effect. This means the craft traveled well into the Thermosphere. People who travel above 50 miles are called astronauts by NASA.

  15. Mach unit valid in space? by Gabrill · · Score: 1

    engine reached mach 10, and climbed to an altitude of 330 miles before the apparatus re-entered the Earth's atmosphere.
    Does it bother anyone else that they're using the speed of sound IN THE ATMOSPHERE to measure a speed of a vehicle NOT IN THE ATMOSPHERE? Or is the summary just misleading?
    --
    Always going forward, 'cause we can't find reverse.
    1. Re:Mach unit valid in space? by theeddie55 · · Score: 3, Funny

      for consistency, would you prefer if they used the speed of sound in a vacuum?

    2. Re:Mach unit valid in space? by Semptimilius · · Score: 1

      I don't think it really matters. It's only a reference speed (probably established at a specific set of atmospheric parameters). They could have referenced it against the speed of light, km/h.

    3. Re:Mach unit valid in space? by Anonymous Coward · · Score: 0

      Yes, it's still valid. This is barely beyond the edge of Earth's atmosphere, and as such is still in a non-vacuum. Now, the density is VERY low, but there's still enough gas to determine a Mach number. I'm willing to bet that the Mach number was WAY over 10, and that they're referencing it to sea level, or some other low altitude reference frame.

      And yes, I AM a rocket scientist, I do know what I'm talking about here.

    4. Re:Mach unit valid in space? by Anonymous Coward · · Score: 0

      It's roughly 330-ish m/s, so it's a rather good measure of speed because it's well known and easy to imagine.

    5. Re:Mach unit valid in space? by cheater512 · · Score: 1

      Its the standard unit for speeds in that region.

    6. Re:Mach unit valid in space? by CompMD · · Score: 1

      Mach number is variable. It depends upon temperature and is only valid in a fluid environment, not a vacuum. You can't have "Mach 10" at 330 miles.

      I'm not an aerospace engineer, but I do play one at work.

    7. Re:Mach unit valid in space? by evilsofa · · Score: 1

      Because atmospheric drag is still an issue at 330 miles up. They used Mach number, not the speed of sound. Mach numbers are extremely important when talking about hypersonic speeds in atmosphere.

      Look up the wiki articles on "Mach Number" and "Earth's atmosphere" for more info.

    8. Re:Mach unit valid in space? by Woek · · Score: 1

      I guess it first reached Mach 10 in the atmosphere, and then exited it. A scramjet engine does not work outside of the atmosphere, but it shows that it can give the craft a big impulse. Going Mach 10 in the upper atmosphere doesn't require a lot of thrust; the density is so low that there is relatively little drag. The trick is that an airbreathing engine with a supersonic combustion chamber needs to fully mix AND combust its fuel in one or two milliseconds to use its fuel efficiently.

    9. Re:Mach unit valid in space? by Farmer+Tim · · Score: 1

      Or is the summary just misleading?

      "Ten times the speed of silence" would be silly.

      --
      Blank until /. makes another boneheaded UI decision.
    10. Re:Mach unit valid in space? by nickspoon · · Score: 1

      Hello darkness, my old friend, I've come to talk with you again...

  16. Just ask CIA/Skunk works, area51 by cheekyboy · · Score: 1

    I am sure the skunk works at CIA/Boeing have all the data/results/secrets already.

    Hell, they made the SR71 back in the old days, imagine what they have NOW!!!

    They wont say ever!!! Stupid top secret morons, showing it off will not hamper anything. I bet Boeing just wants to make another $500billion to $1500 billion selling conventional aircraft for
    the next 25 years, then they will bring online the new models later.

    Good article at http://www.americanantigravity.com/documents/NASA- TM-2006-214547.pdf

    "NASA Memorandum on Advanced Propulsion
    by R.L. Sackheim, J.W. Cole, and R.J. Litchford (NASA MSFC)
    Where is U.S. space flight today, and how did we get here? After 40 years, why are we slowly converging on a slightly updated Apollo architecture? Why is there no Moore's law analogy for rocketry?
    Clearly, we have arrived at a watershed moment in space flight history, and it is essential that we reflect on such questions in a forthright way. Decisions are now being made that could set our future course in space for decades to come, and it is appropriate that we examine the logic that brought space transportation full circle almost back to where we started."

    --
    Liberty freedom are no1, not dicks in suits.
    1. Re:Just ask CIA/Skunk works, area51 by deopmix · · Score: 2, Informative

      I really do hate to nitpick, but the skunk-works are Lockheed Martin, not Boeing.

    2. Re:Just ask CIA/Skunk works, area51 by Keys1337 · · Score: 2, Insightful

      I'm sure they could develope some insane passenger aircraft, but they need to make money not bleed it. If I came up with a proposal to build basically the concord on steroids I don't think people would buy it. I'd try to sell them more cost effective and reliable planes since that's what they are buying.

    3. Re:Just ask CIA/Skunk works, area51 by dbIII · · Score: 1

      I am sure the skunk works at CIA/Boeing have all the data/results/secrets already.

      That relies on the yet unproven assumption that they would be competant enough to find their arse if allowed the use of both elbows. Conspiracy theories that rely on unseen internal perfection of groups that make obvious public mistakes are fatally flawed.

    4. Re:Just ask CIA/Skunk works, area51 by Anonymous Coward · · Score: 0

      Conspiracy theories that rely on unseen internal perfection of groups that make obvious public mistakes are fatally flawed.

      That's just what they want you to think!

      Posting as anonymous for obvious reaso

    5. Re:Just ask CIA/Skunk works, area51 by dosquatch · · Score: 1

      That relies on the yet unproven assumption that they would be competant enough to find their arse if allowed the use of both elbows.

      There's something to the conspiracy theories here. The engineers and scientists in other countries are just as capable and clever as our own, yet no other country has managed to do stealth? It's those alien spacecraft from Roswell, I'm tellin' ya...

      --
      "Hey, the third matrix movie would have been good except for the plot,story, and acting." --AC
    6. Re:Just ask CIA/Skunk works, area51 by Nyeerrmm · · Score: 1

      I'd imagine that has more to do with military budget more than anything else. Most countries probably know basically how it works (RAM, proper geometry), but they don't have the money available for the military to develop it fully, since the basic concepts are only a small part of the picture, and I'm sure all that RAM, and the design time to match aerodynamic needs with low visibility geometry probably takes a lot of time, money, and experience (we've been doing it for a long time, relatively.)

    7. Re:Just ask CIA/Skunk works, area51 by dosquatch · · Score: 1

      Dammit, stop messing with good conspiracy theories by offering perfectly reasonable explanations! I keep tellin' ya, it's the aliens!

      --
      "Hey, the third matrix movie would have been good except for the plot,story, and acting." --AC
  17. Only old farts, MAINSTREAM idiots use MILES by cheekyboy · · Score: 3, Insightful

    Yeah nerds, learn KM, not Miles.

    No self respecting scientist or nerd would ever use the word MILES in their own documents.

    Slashdot is NOT mainstream, get back to being NERDY!!!

    --
    Liberty freedom are no1, not dicks in suits.
    1. Re:Only old farts, MAINSTREAM idiots use MILES by Guppy06 · · Score: 1

      If you wanna use kilometers, build your own scramjet.

  18. That's all well and good, but... by plaxion · · Score: 1

    does it run Linux?

    /obligatory

    1. Re:That's all well and good, but... by Anonymous Coward · · Score: 0

      Imagine a beowulf cluster of these. . .

  19. HyShot, HyCAUSE and HiFire by Anonymous Coward · · Score: 5, Informative

    It was the same fuel as HyShot, plain old hydrogen (plus oxygen gathered from the atmosphere). This scramjet project was named HyCAUSE and the engine was physically a fair bit larger than the successful HyShot flights by the same team a few years back. The team originated from the University of Queensland moved to the Defence Science and Technology Organisation about a year ago. The next flights are a series of ten over five years under the name "HiFire".

  20. Sure it can reach Mach 10... by americangame · · Score: 1

    but is it a robot in disguise?

  21. SCRAM has been done, The real trick will be ... by WindBourne · · Score: 3, Insightful

    getting these to fly without using a rocket to start it. If we can get it to start from say a mach 2 or better sub sonic mach .9, then this will be feasable for more than just bombs. As it is, the only place that this will be of use is in intercontental bombs (small and cheaper).

    --
    I prefer the "u" in honour as it seems to be missing these days.
    1. Re:SCRAM has been done, The real trick will be ... by Anonymous Coward · · Score: 0

      That and getting useful amounts of thrust.

      As I understand, the Australian project was mostly to demonstrate it was possible to achieve a self-sustaining combustion in a supersonic airstream. The actual thrust produced was something like a couple ounces. The significantly more expensive X-43 project wasn't much more impressive in that respect, but from what little information I was able to find, it sounds like it produced about enough to account for the aerodynamic drag.

      If anyone can conclusively confirm or deny this, I would love to see a source, but it seems all of the interesting facts about this project are classified.

    2. Re:SCRAM has been done, The real trick will be ... by smellsofbikes · · Score: 1

      I had an interesting discussion once with a guy who was a designer for the national aerospace plane project, high-ranking USAF as well as NASA. We spent about an hour talking about all sorts of different aspects: fuel, high-temp skins, control systems. The only thing he wouldn't talk about was how it took off: how it produced thrust with zero V.
      I spent some time thinking about it and reading about it. These are some things I know: the system had a single duct going through the whole plane, and it had multiple injection points for fuel. They'd inject at one area in one realm of flight, and another at another, to maximize thrust and also because at full (proposed) speed it actually took the entire length of the craft just to get the hydrogen to diffuse enough with the oxygen to combust smoothly. So, at lower speeds it injected midbody and at high speeds, very near the nose itself.
      Couple that with the old jet trick of starting one jet's engine by parking another jet right in front of it and blasting the front jet's exhaust down the dead jet's intake to get the compressors spinning up high enough, which was used with success to get engines started...
      I bet what they were planning on doing was injecting fuel at the nose at high pressure, pointing backwards, and igniting it, and using the resultant backwards airflow to get the second ignition point at midbody running, so essentially it's operating as a ramjet using its own exhaust to provide the ram air pressure.

      --
      Nostalgia's not what it used to be.
    3. Re:SCRAM has been done, The real trick will be ... by WindBourne · · Score: 1

      That is interesting. Another idea that I was thinking of was that the military is researching using a circular maglev track to launch items into space. Assume that they used that to get the spaceplane up to say mach 3 or 4 (which is VERY doable in a relatively short time), and then launch it. Of course, the track is suppose to be a 20-50 mile diameter track that builds up the speed and then on the last circle, throws a switch sending it up a launcher. That would be very useful for something like this.

      --
      I prefer the "u" in honour as it seems to be missing these days.
  22. Re:Relativity in a Dark Place by craznar · · Score: 4, Funny

    As the theory of relativity breaks down when someone switches the lights off - as C becomes ZERO.

    Oh no ...Einstein didn't think of that.

    --
    EMail: 0110001101100010010000000110001101110010 0110000101111010011011100110000101110010 0010111001100011011011110110
  23. Military, not Civilian applications by moikka · · Score: 4, Insightful

    This is prime example of technology that has almost purely military applications.
    However since that does not excite public positively, they are instead fooling the public talking about civilian use.
    What might be possible some day is to deliver a bomb from Sydney to London in very short time. Not human passangers.
    The inherent heat problems are about 100 times easier to solve, if you imagine
    the payload is 50kg of plutonium instead of 5000 kg of humans.

    1. Re:Military, not Civilian applications by moikka · · Score: 3, Interesting

      Also think about their primary selling-point,
      capable of using oxygen from air and not having to carry it,
      is only an advantage over rocket-engines.
      Jet engines already use oxygen from the air.


      In civilian travel there is great need for fuel-efficiency.
      If their biggest problem is excess heat,
      it automatically means they are wasting huge amounts of fuel to create that heat.
      Only military can afford this wasted fuel.


      Also there is a huge problem in take-off and landing from ground.
      Ramjet is not going to work in those cases.
      So for civilian aircraft use they are going to need conventional jet engines for that purpose.
      Guess how aerodynamically efficient these extra jet engines are going to be at 10 Mach?
      Also another problem that does not exist in military use.


      So 100% certainty the only application this is going to have is delivering bombs.

  24. 2 hours by Anonymous Coward · · Score: 5, Funny

    Including airport queues that's only about 5 or 6 hours.

    1. Re:2 hours by WaZiX · · Score: 1

      2 days counting the strikes...

      In Socialist Belgium, Security Strikes!

  25. 100,000 feet is well within the atmosphere by Anonymous Coward · · Score: 4, Informative

    According to wikipedia, (I know), the atmosphere is usually considered to end at 328,000ft. (Karman line)

    The Stratosphere goes to 160,000ft. You have to go above 50 miles (264,000ft) to be considered an astronaut, and atmospheric effects are noticeable at 400,000ft during reentry.

    1. Re:100,000 feet is well within the atmosphere by Gorshkov · · Score: 1

      gotcha .... I stand corrected. I gotta learn to NOT post at 4am ..... it's causing a lot of pissyness in the global warming article just down the hall :-)

    2. Re:100,000 feet is well within the atmosphere by Nexx · · Score: 1

      So that article's "abuse" and this one's "funny walks"?

  26. Re:330 miles is well beyond the Kármán l by GISGEOLOGYGEEK · · Score: 1

    Significant atmostpheric drag occurs AT much hiGHer elevaTIonS. To say that it starts to have an effect at 75 miles is nuts.

    tHE International space station constantly looSEs eleVATion dUe to atmostpheric drag, it's usual elevation is around 500 miles. When the space shuttle visits, it usually burns its rockets to push the ISS back to an elevation close to that.

    Just last year the ISS was in a very low orbit becuase solar storms had caused the upper atmosphere to bulge, placing more drag on the station.

    (my keyboard is failing, sorry about the mixed case words)

    --
    George Bush + Linux = "I will not let information get in the way of the fight against Windows"
  27. Aurora? by Anonymous Coward · · Score: 0

    What about the Aurora?

  28. 330 miles ? by Yvanhoe · · Score: 2, Insightful

    How is an altitude of 330 miles within earth's atmosphere ?

    --
    The Wise adapts himself to the world. The Fool adapts the world to himself. Therefore, all progress depends on the Fool.
    1. Re:330 miles ? by jkerman · · Score: 1

      Its not. it reached that altitude /before/ returning to the atmosphere. its right in the summary!!

    2. Re:330 miles ? by LifesABeach · · Score: 1

      Possibly by using a can or two of Foster's before measuring.

      Cheers Mate.

  29. Supersonic scramjet? by Anonymous Coward · · Score: 0

    That's supersonic supersonic cramjet, twice as supersonic as a usual cramjet. Quite cool.

  30. Scramjets need an atmosphere by Moraelin · · Score: 5, Informative

    Scramjets need an atmosphere anyway, just like ramjets and turbojets. That's the whole idea. The air flows through it, fuel is injected into that air and ignited. Trying to operate a scramjet in a vacuum would make as much sense as trying to operate a turbojet there. Pretty much all 3 are the same jet engine, more or less. A turbojet uses a compressor in the front to push the air into the engine. A ramjet relies on the fact that if you fly fast enough to start with, you get air pushed into the engine anyway. (Plus some clever design of the intake so the flame doesn't go in both directions.) But the air is slowed down to a subsonic speed at the point where the fuel is injected and lit. A scramjet is a ramjet where the air does flow at supersonic speed through the engine, so basically it's choked. You can add the fuel past the choke point and, since waves can't move backwards in a supersonic flow, whatever pressure you generate there by burning fuel can only go towards the back engine. The front of the engine can't "notice" the higher pressure in the back half because a pressure wave would have to travel through that air faster than sound speed, which isn't possible. Another rough description would be that a scramjet is like a turbojet with an afterburner, only without the turbojet. (Sorta like the sound of one hand clapping, I guess;) Instead of having the turbojet push air through a nozzle and add extra fuel to it, the engine _is_ the nozzle and the airplane's existing speed is what pushes air to it. So you just add the fuel and light it. It's an afterburner without a turbojet. But in the end all 3 work by the same basic principle: air comes through the front, fuel is added, hot air comes out the back. No air, no flame, the engine stops. The plans to use a scramjet to get to a highe enough orbit or even leave the planet, involve getting enough speed while still having enough air for the scramjet, or as boosters in addition to the normal rocket engines, or both.

    --
    A polar bear is a cartesian bear after a coordinate transform.
    1. Re:Scramjets need an atmosphere by Gorshkov · · Score: 2, Informative

      now, THAT was an explanation. Right now I regret that I'd already posted to this discussion - I can't use my mod points on you. Thanks.

    2. Re:Scramjets need an atmosphere by Anonymous Coward · · Score: 0


      Who's jetting what now?

    3. Re:Scramjets need an atmosphere by dyslexicbunny · · Score: 5, Informative

      A ramjet relies on the fact that if you fly fast enough to start with, you get air pushed into the engine anyway. (Plus some clever design of the intake so the flame doesn't go in both directions.) Not necessarily. The ramjet inlet's design is such that the air is compressed through ram compression, essentially the air is compressed as it is slowed down. There really isn't any clever design on the inlet. The pressure in the inlet area is greater than the that of the combustor and so long as that is true, no flame will come out. You're essentially correct but I just wanted to nitpick.

      Explaining the turbojet is easier after explaining the ramjet. Ramjet performance suffers below Mach 1 because you can't get enough compression for efficient combustion. The turbojet adds a compressor to add work to the flow so you can get the desired pressure ratio coming into the burner. Then you have to go through the turbine such that you can power the compressor.

      Engines with compressors are far more interesting as they can be pushed to the point (whether by power setting or flight condition) such that the compressor can stall and flame will shoot out the front of the engine. It's something pretty important in compressor design since they operate with an adverse pressure gradient (pressure out > pressure in). This is why you see compressors with 10+ stages powered by only 1-2 turbine stages. It's really quite interesting.

      You basic principle explanation isn't great for non-engineers. Try using "Suck, squeeze, bang, blow." I explained that to some friends of mine and they were way more interested. They not only laughed but they then wanted to hear more detail. But solid explanations on your part, I just wanted to nitpick a couple things since I'm a propulsion guy.
    4. Re:Scramjets need an atmosphere by vikstar · · Score: 1

      You seem to know what you're talking about, so I'd like to ask you a question. I read (turbject thrust reversers) that one of the ways to achieve thrust reversal on turbojet engines is "target type of thrust reverser" which from what I gather reverses the fan blades so that they blow forward rather than backward. However, won't this reduce pressure in the engine making it go out, and therefore make the plane loose power (electricity)?

      --
      The question of whether a computer can think is no more interesting than the question of whether a submarine can swim.
    5. Re:Scramjets need an atmosphere by lommer · · Score: 1

      I gather reverses the fan blades so that they blow forward rather than backward

      Nope. For thrust reversers, the jet engine stays exactly the same, you just drop a bucket behind it. This redirects the exhaust air forwards, thereby braking the aircraft.

    6. Re:Scramjets need an atmosphere by dyslexicbunny · · Score: 2, Interesting

      lommer gave a pretty solid explanation of what is going on with thrust reversers.

      Reversal depends on the engine type (turbojet, turbofan, etc..) and the manufacturer. I've seen some information that one manufacturer blocks the bypass nozzle and redirects the flow out to reverse thrust. Pretty much, the fan still operates as usual but the bypass air is used and not the core flow (through the burner). It sounds like you have some mild confusion as to engine classes/terminology so I'll provide some details that might help clear things up plus a couple decent links with flowpaths.

      Turbojet describes a simpler turbomachine engine -> inlet, compressor, burner, turbine, nozzle http://www.aerospaceweb.org/question/propulsion/je t/turbojet.jpg
      Turbofan describes a more complex engine -> inlet, fan, splitter, compressor, burner, hp turbine, lp turbine, nozzle... splitter, bypass duct, bypass nozzle http://www.aerospaceweb.org/question/propulsion/je t/turbofan.jpg

      Turbofans are used nowadays on commercial aircraft because they have a significantly better fuel consumption. Engine thrust can be calculated using
      Thrust = mass flow * (jet velocity - intake velocity)

      You have two ways of increasing thrust: you can have a small mass flow and have a large Vjet (turbojet) or you can have a large mass flow and smaller Vjet (turbofan). The only way to produce a large Vjet is to burn more fuel. The term bypass ratio is used to compare the bypass air / core flow. The GE90 sports bypass ratio of 9. Bypass is difficult to deal with since increasing bypass ratio will reduce fuel burn BUT when in cruise, they have a ridiculous profile drag.

      Ultimately, engine design is a complicated trade with multiple attributes at different mission segments matching vehicle thrust requirements, vehicle dimension needs, field conditions, maintainability, and noise and emissions regulations just make up a handful of the design concerns. So next time you fly, try getting a seat behind the engine and try to check things out. The design process is really quite amazing.

      I'm going to stop here since I've written a lot. I'm just excited about having insightful things to say for once.

    7. Re:Scramjets need an atmosphere by Moraelin · · Score: 1

      Well, the fact that it's slowed down and compressed sounds clever enough to me :P

      --
      A polar bear is a cartesian bear after a coordinate transform.
  31. Gah. Once more, with formatting by Moraelin · · Score: 5, Informative

    Scramjets need an atmosphere anyway, just like ramjets and turbojets. That's the whole idea. The air flows through it, fuel is injected into that air and ignited. Trying to operate a scramjet in a vacuum would make as much sense as trying to operate a turbojet there.

    Pretty much all 3 are the same jet engine, more or less. A turbojet uses a compressor in the front to push the air into the engine. A ramjet relies on the fact that if you fly fast enough to start with, you get air pushed into the engine anyway. (Plus some clever design of the intake so the flame doesn't go in both directions.) But the air is slowed down to a subsonic speed at the point where the fuel is injected and lit. A scramjet is a ramjet where the air does flow at supersonic speed through the engine, so basically it's choked. You can add the fuel past the choke point and, since waves can't move backwards in a supersonic flow, whatever pressure you generate there by burning fuel can only go towards the back engine. The front of the engine can't "notice" the higher pressure in the back half because a pressure wave would have to travel through that air faster than sound speed, which isn't possible.

    Another rough description would be that a scramjet is like a turbojet with an afterburner, only without the turbojet. (Sorta like the sound of one hand clapping, I guess;) Instead of having the turbojet push air through a nozzle and add extra fuel to it, the engine _is_ the nozzle and the airplane's existing speed is what pushes air to it. So you just add the fuel and light it. It's an afterburner without a turbojet.

    Downside: a turbojet can start at zero speed, ramjets and scramjets need enough airspeed to start. Hence all these experiments involve booster rockets.

    But in the end all 3 engines work by the same basic principle: air comes through the front, fuel is added, hot air comes out the back. No air, no flame, the engine stops.

    The plans to use a scramjet to get to a highe enough orbit or even leave the planet, involve getting enough speed while still having enough air for the scramjet, or as boosters in addition to the normal rocket engines, or both.

    --
    A polar bear is a cartesian bear after a coordinate transform.
    1. Re:Gah. Once more, with formatting by 6Yankee · · Score: 5, Funny

      Well, that's one way to get +10 Informative ;)

    2. Re:Gah. Once more, with formatting by sticky.pirate · · Score: 1

      Slashdot is REALLY going downhill: now even the comments are dupes

    3. Re:Gah. Once more, with formatting by Moraelin · · Score: 1

      Heh. Trust me, I'd rather have just edited the old one, if it were possible.

      --
      A polar bear is a cartesian bear after a coordinate transform.
    4. Re:Gah. Once more, with formatting by salec · · Score: 1

      Another rough description would be that a scramjet is like a turbojet with an afterburner, only without the turbojet. (Sorta like the sound of one hand clapping, I guess;) Instead of having the turbojet push air through a nozzle and add extra fuel to it, the engine _is_ the nozzle and the airplane's existing speed is what pushes air to it. So you just add the fuel and light it. It's an afterburner without a turbojet.
      Does it mean that a multi-mach plane can be made that shuts down the turbo engine and closes front air intake past some speed to run on afterburner only?
    5. Re:Gah. Once more, with formatting by Moraelin · · Score: 1

      Well, air has to come through that nozzle, one way or another. In a turbojet, you have the turbojet's exhaust coming through it. (Which still has lots of oxygen, since if you used enough kerosene in the turbojet to use all oxygen, you'd also melt the turbine at the back.) In a ramjet, it's the simple fact that you move forward very fast and the air is rammed into the engine. But one way or another, for the afterburner to work, you have to already have a jet of air coming out the back end.

      So if the front intake is shut down, you'd have to have some other way of creating a jet of air through the nozzle. (Opening extra vents around, perchance?) It would also have to be the kind of nozzle which works well for both.

      At least theoretically, I'm sure someone could figure out something smart there. I'm just not sure how. I could see the reactor turned into the central intake piece for a ramjet, sorta, but not sure how it would work for a scramjet. Then again, I'm not an aerospace engineer anyway.

      On the other hand, well, we have enough trouble making a scramjet that just works as it is. Having it _also_ work as a nozzle for a turbojet, is trying to solve a second problem at the same time, when we're still just experimenting with the first one. So, well, let's take it one problem at a time :)

      Combinations for ramjets do exist, though, it's just that they're a combination with rocket instead of with turbojet. In some missiles, the ramjet engine first holds the fuel for the rocket engine. When that's exhausted, the ramjet kicks in. Some extra boosters may be used, but even those often are just extra combustors that use the propellant stored inside the ramjet.

      At a (layman's uninformed) guess, probably that would be the easiest solution for a hypersonic aircraft, with the technology we have now. Ramjets are already well understood and work, and are already used in missiles. The combination with rocket engine is also well understood.

      Whether it's actually desirable to make a Mach 5 passenger aircraft, though, that's a whole different question. For starters the noise level would be horrible, and the fuel efficiency wouldn't be too good. While a ramjet is more efficient than a turbojet above Mach 2 to 4, that doesn't really say that much. Both are considerably less efficient than just staying subsonic with a turbofan.

      --
      A polar bear is a cartesian bear after a coordinate transform.
  32. Six seconds of flight by Richard+Kirk · · Score: 2, Interesting

    Scramjets look good on paper. The thin air coming in is compressed by a series of standing shock waves. Unfortunately, the geometry of these shock waves can easily be upset by small distortions in the engine, which in turn can lead to changes in the stresses with in the engine, which - to cut a long story short - can mean the engine spectacularly demolishes itself when faced with real bits of atmosphere with unpredictable air currents. I found the flight time in...

    http://www.abc.net.au/science/slab/hyshot/default. htm

    It may not sound like much, but six seconds is very respectable for a scramjet. Yay!

    There is a lot of touting about how this would get you from London to Sydney in 40 minutes and stuff. I am not sure how true or economical this is, even if scramjets can be made safe. When you are flying fast, you can either take your oxidant with you (as rockets do) or you can scoop it up as you go along. Scooping it up as you go along means taking in air that was initially at rest and getting to move at the speed the engine is currently going. As only 20% of the air is actually the oxygen you want, this is not necessarily an effective thing to do. It becomes most effective when the oxidant (oxygen) is a lot heavier than the reductant (fuel - and hydrogen is particularly light), so scooping it up as you go takes a lot off the take-off weight.

    The other London to Sydney option is to get just beyond the atmosphere using a conventional rocket, then going ballistic and weightless for the main distance, and re-entering and gliding, a lot like the space shuttle. While being weightless is fun, being weightless for 20 minutes makes most people puke, so a large passenger jet might skip the atmosphere and retain a little gravity. A scramjet might be used for this.

    Nevertheless, yay!

    1. Re:Six seconds of flight by Mike+Van+Pelt · · Score: 1

      cooping it up as you go along means taking in air that was initially at rest and getting to move at the speed the engine is currently going.

      One quibble:

      Actually, the whole idea of the scramjet is that you don't boost the air up to the speed the engine is currently going. You burn the fuel in the air as it passes through the engine at supersonic speed. That's the "SC" in Supersonic Combustion Ramjet.

      There are, of course, lots of practical difficulties; you listed some of them.

    2. Re:Six seconds of flight by Anonymous Coward · · Score: 0

      While being weightless is fun, being weightless for 20 minutes makes most people puke, so a large passenger jet might skip the atmosphere and retain a little gravity.

      Ditch all windows and spin the craft like they did in the space station docking sequence in 2001 (1968)

      Won't that solve the problem of nauseous passengers?

    3. Re:Six seconds of flight by Scott+Carnahan · · Score: 1

      One more London to Sydney option is to build a large tube in the ocean, remove all of the air and water from the tube, and run a maglev through the vacuum. This eliminates air resistance and problems with moving parts, at the expense of considerable capital investment and some heat dissipation issues. There don't seem to be any fundamental obstructions to making this trip in under an hour, although the acceleration may be a bit uncomfortable - you need about 1.4g to do 20000km in 40 minutes.

      --
      "Your notation sucks!" -- Serge Lang (1927-2005)
    4. Re:Six seconds of flight by Richard+Kirk · · Score: 1
      The man is, of course, quite right.

      In a SCRAMjet, we are not accelerating and squashing the air like the Olympus engines on Concorde, but trying to get the thrust from the air as it goes through. I had skipped this bit to keep my note short and accessible to people who might be confused by the original article. Rather lazy writing style, and serves me right for being caught out.

      Thanks.

  33. Re:330 miles is well beyond the Kármán l by jamesh · · Score: 4, Funny

    Message intercepted. Cover blown. Please return to base for debriefing.

  34. Faster is better by Anonymous Coward · · Score: 1, Insightful

    ... all the better to bomb you with.

  35. Minor correction by Anonymous Coward · · Score: 0

    Probably best to refer to the original press release:

    http://www.dsto.defence.gov.au/news/5118/

    As it says, the test that took place is the first time flight data was taken from a certain design of scramjet, not scramjets in general. I think the media got a little carried away.

  36. scramming before exit or after re-entry? by dillee1 · · Score: 1

    The article is a typical layman news-speak that has little detail.
    Does the new craft
    1) start the scramjet engine after boosting, attaining enough speed and reach apogee of 530km?
    2) boost with rocket, reaching apogee of 530km, re-entry and starts the scramjet with gravitational acceleration? (ala another HyShot)?
    Either way, both have a lot of previous art and whats so special about it?

    1. Re:scramming before exit or after re-entry? by DragonTHC · · Score: 1

      you have to start the scramjet under acceleration.

      otherwise, you'll never get enough flow through it to start it up.

      --
      They're using their grammar skills there.
  37. Some background by anonieuweling · · Score: 1

    http://www.uq.edu.au/news/index.html?article=11183 So which Skyshot plane did fly here?

  38. It's x10 powerful!!! by Anonymous Coward · · Score: 0

    My experiment consist on

    40% methane as superfuel + 20% kerosene as fuel + 15% titaniate of potasium as superoxidizer + 5% sulphate of cupper as oxidizer.

    1. Re:It's x10 powerful!!! by Victor+Antolini · · Score: 1

      What's the other 20%? Evil?

    2. Re:It's x10 powerful!!! by Anonymous Coward · · Score: 0

      Superevil.

  39. What's that in... by kybred · · Score: 1

    This event took place in Australia, and was reported by an Australian paper; therefore, it was correctly reported in the metric altitude of 530 kilometres.

    530Km? What's that in furlongs?

    1. Re:What's that in... by foniksonik · · Score: 1

      530 kilometers = 2 634.61386 furlongs ...google to the rescue

      --
      A fool throws a stone into a well and a thousand sages can not remove it.
    2. Re:What's that in... by Atzanteol · · Score: 1

      2,634.61386 furlongs.

      --
      "Ignorance more frequently begets confidence than does knowledge"

      - Charles Darwin
  40. Gah. Once more, with formatting by roman_mir · · Score: 4, Funny

    Now, that was an explanation! Right now I regret that I'd already posted to this discussion - I can't use my mod points on you. THANKS.

  41. Misleading summary by Anonymous Coward · · Score: 0

    The scramjet didn't "reach" mach 10 or 530km, the rocket carrying it did:

    "They said it reached an altitude of 530 kilometres (330 miles) before the scramjet was successfully deployed"

    Pretty far cry from what the article summary claimed, or from even being interesting.

  42. Microsoft Bought Them. by twitter · · Score: 0, Offtopic

    This is cool, yes, but the emphasis on "first" seems a bit off.

    The vague, hyped up and imageless press release is typical of the new management's style. The Australian Defence Science and Technology Organisation signed an unconditional surrender to M$ in May. I found those pictures when I visited the official media release and saw Steve Ballmer instead of scram jets in the image gallery. It's almost like they did this on purpose, just to show you that Vista is being accepted by any government agency.

    --

    Friends don't help friends install M$ junk.

  43. Oceania Rules Australia by twitter · · Score: 1

    Is there something I'm just not getting here?

    Get with the program, comrade, the party also invented the helicopter. All progress and innovation come from the company.

    --

    Friends don't help friends install M$ junk.

  44. Rudundant and repetitive by keithjr · · Score: 1

    http://en.wikipedia.org/wiki/Scramjet saying supersonic scramjet is like saying IRS Service

    1. Re:Rudundant and repetitive by mshurpik · · Score: 1

      Here's the relevant paragraph from the Wiki article:

      "Unlike a rocket that quickly passes mostly vertically through the atmosphere or a turbojet or ramjet that flies at much lower speeds, a hypersonic airbreathing vehicle optimally flies a "depressed trajectory", staying within the atmosphere at hypersonic speeds. Because scramjets have only mediocre thrust-to-weight ratios, acceleration would be limited. Therefore time in the atmosphere at hypersonic speed would be considerable, possibly 15-30 minutes. Similar to a reentering space vehicle, heat insulation from atmospheric friction would be a formidable task. The time in the atmosphere would be greater than that for a typical space capsule, but less than that of the space shuttle."

      Now we know why the SR-71 required titanium construction at only mach-3.

  45. Actually, it could be done by Moraelin · · Score: 2, Insightful

    Actually, at least theoretically a scramjet would continue to accelerate as long as you have air and fuel. You have enough air you have of that ascent (after that you have the speed anyway), and fuel you'd carry anyway. A rocket carries its fuel too.

    That's actually one thing that makes scramjets tempting: the fact that it doesn't cap lower than that orbital velocity, and it can work with rather thin atmosphere too. So if you can go upwards at all with it, and modify the trajectory to have enough air for more of the time, you can eventually get it to stay up there.

    Probably the only thing that _might_ change, if your scramjet doesn't get enough acceleration, is that you shoot it closer to the horizontal than upwards. Well, normal rockets don't really go vertically either. As you've said, they have to end up with that mach 30 horizontal speed. The difference would be that the rocket starts closer to vertical, to clear the dense atmosphere as fast as possible, and bends later, while probably a scramjet would start directly oblique, to make the most of that atmosphere.

    Of course, when experimenting to just get the thing sorted out at all, there's somewhat less point in aiming directly for LEO. So probably 14 seconds are enough for experimental purposes.

    Also, well, while scramjets are still experimental, ordinary ramjets aren't. A heck of a lot of missiles already use ramjets. E.g., IIRC the Russians were the first to use them on anti-aircraft missiles, but in the meantime almost everyone else does.

    So technically we'd already have a pretty damn fast engine to put on an aircraft. If anyone wanted to make a Mach 5 passenger aircraft, that's probably already feasible with ramjets. The reasons why we don't are completely different, and IMHO somewhat unlikely to change because of scramjets.

    --
    A polar bear is a cartesian bear after a coordinate transform.
  46. Popular mechanics... by Anonymous Coward · · Score: 0

    But a sneak peek that I had of next months popular mechanics had a scramjet flying car on its cover. They're just around the corner!

  47. Speed of sound *decreases* with increased density. by Guppy · · Score: 1

    The speed of sound generally gets lower as the material loses density, higher as the material gains density (think about a wave traveling through a solid block, as opposed to one traveling through water, then one traveling through the air) I believe that's incorrect, the speed of sound is given by sqrt([Bulk Modulus]/[Density]). As density decreases, the speed of sound increases. The speed of sound in water is faster than air despite its greater density, due to its much higher bulk modulus.
  48. Re:Relativity in a Dark Place by bar-agent · · Score: 1

    As the theory of relativity breaks down when someone switches the lights off - as C becomes ZERO.

    Oh no ...Einstein didn't think of that.


    He did, actually, but he spent too long on that thought experiment and got eaten by a grue.

    --
    i'd hit it so hard, if you pulled me out you'd be the king of britain [bash.org]
  49. Summary is confusing as hell. by shaitand · · Score: 1

    It says that using air from the atmosphere as fuel is basically what makes a scramjet a scramjet, then claims this is the first scramjet ignited within the atmosphere. How the hell did they ignite the other ones without the atmosphere they use as fuel? Further it goes on to say that they sent it into space. Last I checked there isn't much air to use as fuel in space either.

    Anyone care to explain? Preferably in English.

  50. Time travel by flyingfsck · · Score: 1

    That just shows you how fast it was - it traveled back in time and therefore was indeed the first.

    --
    Excuse me, but please get off my Pennisetum Clandestinum, eh!
  51. Ballistic dive? by mshurpik · · Score: 1

    TFA: They said it reached an altitude of 530 kilometres (330 miles) before the scramjet was successfully deployed following re-entry to the Earth's atmosphere.

    So the scramjet was deployed during a ballistic rocket dive? Seems like an easy way to reach mach-10, with or without a scramjet.

    Now they're talking about using it on the way UP, that's quite different from what they did.

  52. Here's your parting gift... by Anonymous Coward · · Score: 0

    Bzzzt. Wrong again! Oxygen could be used as fuel in a fusion process.

  53. Sig FTW by IdahoEv · · Score: 1

    Internet Explorer's CSS rendering: WYSIWTF

    This one had me laughing and crying at once.

    I do only standards-compliant web design. With no hacks even, if I can avoid it at all. I develop my layouts with simultaneous testing in Safari and FF (which agree on rendering 95%+ of the time), then I go back and try to make them work in IE 5.0 through 7.0. Still with no hacks.

    The IE-compatibility phase of my design process consumes about 80% of the total time for a typical site. No amount of experience seems to improve this, either, because I find new bugs every time. I've found at least three IE bugs not documented at positioniseverything.net.

    --
    I stole this sig from someone cleverer than me.
  54. Happy Noodle Boy? by ndogg · · Score: 1

    I didn't know that Happy Noodle Boy was a /. user.

    (JTHM reference)

    --
    // file: mice.h
    #include "frickin_lasers.h"
  55. HiFire scramjet project? by asky · · Score: 1

    Getting to the core of this story is definitely a real challenge, and we may not get it until Aviation Week http://www.aviationweek.com/ reports on it. However, connecting the dots together, this may be the first test flight of the HiFire project, a joint USAF/NASA/Australian effort.

    AvWeek ran an article on March 18 this year entitled "The HiFire Flight Tests Will Help Integrate Aeronautics and Space Technologies". (URL was really long, possibly session dependent.) From that article: The HiFire payloads will dive into the atmosphere at Mach 4-8 to obtain data directly applicable to new hypersonic flight vehicles. The tests are to begin in the outback of southern Australia.

    The AvWeek article further explains that HiFire will "directly support technology needs for the X-15" and that the X-51 is "the jewel in the crown of hypersonics".