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HyShot Scramjet Test Declared a Success

An anonymous reader writes: "ABC news is reporting that analysis of the flight data from the recent HyShot scramjet test (covered by Slashdot previously) suggests that the test was successful and that the engine achieved combustion in flight after reaching Mach 7.6. The University of Queensland is also reporting the news."

253 comments

  1. I will take two! by rosewood · · Score: 1, Funny

    One step closer to being able to fly farther, cheaper, faster?

    That is, other then getting drunk on jet fuel and then lighting my own farts.

    1. Re:I will take two! by Wiener · · Score: 1
      One step closer to being able to fly farther, cheaper, faster?

      I'd like to just be able to fly in comfort.

    2. Re:I will take two! by ThereIsNoSporkNeo · · Score: 1

      "That is, other then getting drunk on jet fuel and then lighting my own farts."

      I'm standing by with a Darwin Award should you fail.

      In you succede, I've also got venture capital.

      Gambling on stupidity-

      --
      With my dying breath, I curse Zoidberg!
    3. Re:I will take two! by Anonymous Coward · · Score: 0

      What.. too cheap to buy your extra seat on SouthWorst?

  2. BBC link on the story... by MrFenty · · Score: 5, Informative
  3. Queensland university article text by Anonymous Coward · · Score: 0, Informative
    HyShot program secures place in flight history

    University of Queensland researchers today (August 16) claimed success for the world`s first flight test of supersonic combustion, the process used in an air-breathing supersonic ramjet engine, known as a scramjet.

    "Our honest understanding from preliminary data is that the experiment worked," said international HyShot(TM) program leader Dr Allan Paull, of UQ's Centre for Hypersonics.

    "We received data for the full length of the 10-minute flight. All indications are that supersonic combustion occurred. We'll now be submitting the results to international peer review."

    On July 30 a safe and successful launch of a Terrier Orion Mk 70 rocket containing a scramjet payload was held at Department of Defence's Woomera Instrumented Range, 500km north of Adelaide, in the South Australian desert.

    The aim of the HyShot(TM) program is to provide the world's first in-flight tests of scramjet technology, validating experiments held in ground test facilities.

    While scramjets raise the possibility of Sydney to London flights in two hours, they are set to revolutionise the launch of small space payloads, such as communications satellites, by substantially lowering costs. They have the added benefit that they do not even have to carry most of their propellant as they use oxygen from the atmosphere.

    University of Queensland Vice-Chancellor Professor John Hay congratulated the international HyShot(TM) team on its success, which he said put Australia at the forefront of this new technology and enhanced the country's international prestige in space research.

    "It's a magnificent example of international collaboration, involving researchers from Australia, the United States, Britain, France, Germany, Korea and Japan," he said.

    Professor Hay is chair of the Group of Eight, Australia's leading research-intensive universities which produce the majority of Australian scientific research.

    "Australia has proved we can develop this technology at a fraction of the cost of overseas programs. We must now build on success and secure the program in Australia so the intellectual property is not lost to the country. The danger is that the program could move offshore.

    "Dr Paull has received approaches from top Australian researchers based in NASA, Boeing and other organizations keen to return to Australia to work on the HyShot program if suitable funding is available."

    Professor Hay said these researchers were trained at UQ's Centre for Hypersonics, which is directed by Professor Richard Morgan. This is the largest group of hypersonics researchers in Australia and the largest University-based hypersonics group in the world, with some of the world's most advanced equipment for simulating velocities of eight times the speed of sound to 50 times the speed of sound, the speeds experienced by reentry vehicles such as space shuttles and after interplanetary missions.

    "HyShot(TM) provides a significant opportunity for Australia to reverse the brain drain," Professor Hay said.

    Dr Paull said he was negotiating with various groups to conduct an extensive, ongoing and advanced $50 million program of six flights over five years, leading to a free flying scramjet engine. The program would provide information to determine a cost effective launcher based in northern Australia to launch small, lightweight satellites.

    "The program has generated lot of international interest," he said. "We currently don't have funding for future flights, but the Japanese, through NAL, have provided funding to build a new payload." Dr Paull will visit international collaborators in the next few weeks for talks on future flight programs.

    The recent HyShot(TM) launch was designed to take the scramjet engine to a speed of Mach 7.6 (or more than seven times the speed of sound) for the experiment, using a Terrier Orion rocket. The rocket and payload reached an altitude of 314km before the rocket was configured to fly in a new trajectory pointing the payload back down to earth. The flight experiment took place within only the last few seconds of the flight, lasting almost 10 minutes.

    After the Terrier booster had finished its work and subsequently fell 5km downrange, the Orion continued on with the scramjet payload and impacted some 370km downrange of the launch site, very close to the nominal impact point predicted by the scientists.

    Radar and four sets of telemetry (radio) tracked the flight. One telemetry station was at Woomera Instrumented Range, while three telemetry officers were stationed at three points of a triangle more than 300km downrange in the middle of the desert. They not only captured the final seconds when the experiment occurred, but one site, to its credit, also captured all but the first 15 seconds of the flight.

    Dr Paull said this was a "tremendous achievement."

    "All those who were involved in producing this most exciting result are to be commended," he said.

    After everyone had gone home, the researchers faced a nail-biting wait for the telemetry officers to come in from the dust with their precious data, before analysis could occur.

    Dr Paull said everything appeared to have worked to plan, with only a minor glitch of a horizon sensor to turn the rocket failing half way through the flight, but a backup system had kicked in, using all their software capabilities.

    Astrotech Space Operations senior engineer Dr Morgan Windsor said the job that so few with so little undertook was incredible and the fact that it worked was almost anti-climactic.

    "Allan said a number of times that just getting the payload launched was a great success and indeed it was. But now that he has achieved combustion in flight this represents a huge accomplishment and a first internationally. I am so pleased that I had the opportunity this late in my career to support UQ, Allan and his team and have not sensed a greater feeling of accomplishment," Dr Windsor said.

    Professor Hay and Dr Paull thanked all consortium partners and sponsors, in particular:

    Astrotech Space Operations/DTI
    QinetiQ
    Defence Science and Technology Organisation (DSTO)
    Defence Corporate Support
    Aircraft Research and Development Unit, Australian Defence (ARDU)
    the Australian Research Council
    NASA Langley Research Center
    NAL (National Aerospace Lab. Japan)
    AFRL (Air Force Research Laboratory, USA)
    DLR (German Aerospace Center)
    Seoul National University
    DISR
    Australian Space Research Institute (ASRI)
    BAE Systems Australia
    Alesi Technologies
    GASL
    Aerospatiale Matra
    NQEA
    UniQuest
    Institution of Engineers Australia (Queensland)
    Jet Air Cargo
    AECA
    Luxfer Australia

    Media contacts:
    UQ Communications - Jan King, telephone 0413 601 248 or 07 3365 1120, Peter McCutcheon, telephone 07 3365 1088 or 0413 380012


    Hyshot(TM) stories are available at www.uq.edu.au/hyshot. Photos, attributed to The University of Queensland (photographer Chris Stacey), can be downloaded from http://www.uq.edu.au/news/hyshot/hyshot-gallery.ph p

  4. Not again. by mrselfdestrukt · · Score: 1, Funny

    For fsck sake. If I have to read about this 1 more time, I'm gonna screamjet.

    --
    "I used to have that really cool,funny sig ,but it got stolen."
  5. Actual Destinations? by d_force · · Score: 0, Interesting
    Disclaimer: I'm no rocket scientist, nor claim to have lots of knowledge about air travel.

    At a practical level, once you're travelling at 7.6 Mach, wouldn't you already be at your destination by then? Granted, it may be nice to circle the globe a couple of times effeciently (i.e. spy planes, etc) -- but for actual travel.. is the plan to try and get this effect to occur at a lower speed for it to be useful?

    --
    SELECT * FROM USERS WHERE A_WINNER = "YUO";
    1. Re:Actual Destinations? by Jucius+Maximus · · Score: 1

      They are using it for reaching the secret extra terrestrial base on the other side of the moon with great speed on short notice.

    2. Re:Actual Destinations? by Xaoswolf · · Score: 2

      I know that if I go on vacation, I would rather not have to strap myself to an MK 70 Rocket before the preflight movie. They have a lot of work before this is practical for almost anything than spyplanes. Also, was this flight manned, they said that the previous attempt was not, and there was no mention of what a flight like this would do to a living organism.

    3. Re:Actual Destinations? by Jhan · · Score: 2, Funny
      Also, was this flight manned [?]

      314 km straight up, followed by a plunge straight into the ground?

      I sure as hell hope it was unmanned!

      --

      I choose to remain celibate, like my father and his father before him.

    4. Re:Actual Destinations? by Oculus+Habent · · Score: 5, Interesting

      Mach 7.6 is right around 2,260 m/s (7,414 ft/s) or about 5,055 mph. It would still take you 5 hours to circumnavigate the globe. Plus you have to consider acceleration time - the rocket doesn't have to worry about killing people.

      Realistically, we probably won't hit Mach 7 in commercial flights for some time, and there will probably be "low-speed" versions for shorter distances. As the article notes (emphasis mine):

      The engine kicked into action on the way back down at 35 kilometres above the earth, with data transmitted by radio until it began to burn up.

      --
      Warning! Error reporting system failu

      --
      That what was all this school was for... to teach us how to solve our own problems. -- janeowit
    5. Re:Actual Destinations? by Xaoswolf · · Score: 3, Interesting

      Me too, but it is an expiremental craft, and there were problems launching the first one.
      hmmm...
      Add a warhead and you have one hell of a fast ICBM...

    6. Re:Actual Destinations? by starman97 · · Score: 4, Insightful

      The 2nd article points out that the engine is for use with space payloads, you dont have to carry your oxidizer while in the atmosphere, reducing vehicle weight and increasing payload.
      Now, getting to Mach 7.6 to light one of these off may take a railgun, something that rules out living payloads, but good for launching cheap infrastructure into LEO.

      --
      Starman97@Gmail.com (bring it on spammers)
    7. Re:Actual Destinations? by John+Allsup · · Score: 3, Informative

      Note that the figures at
      fas.org indicate that the speed of the Minuteman III at burnout is approx. Mach 23.

      What you do have the potential for (given significant further progress) is very fast cruise missiles, not ICBM's.

      --
      John_Chalisque
    8. Re:Actual Destinations? by mprinkey · · Score: 5, Informative

      there will probably be "low-speed" versions for shorter distances

      Probably not. To understand why requires some knowledge of how a scramjet differs from a normal turbofan engine. There are no spinning parts in a scramjet or ramjet engine. The (sc)ram engine requires a strong standing shock to me maintained in the intake. This standing shock replaces the compressor section of a normal turbo fan. There is a minimum speed which will produce a sufficiently strong, stable shock that will allow this to work.

      The SC part is for supersonic combustion which makes that standing shock also replace the combustor portion of the turbo fan. Chemical reactions and transonic fluid dynamics can interact in very complicated ways. This can make this supersonic combustion unstable. The best way to stabilize it is to go faster and increase the strength of the shock.

      So, to sum up, operating scramjets at lower speeds is more difficult, so if anything, we will probably see them operating at the highest possible speeds that the airframe and aerodynamics will allow.

    9. Re:Actual Destinations? by doi · · Score: 3, Informative

      At a constant 1G acceleration, you'd hit Mach 7.6 in about 4 minutes and travel about 260 KM. The Space Shuttle goes supersonic within 75 seconds of liftoff, so it really doesn't take too long. I think by the time the boosters drop off (2-1/2 minutes) it's doing Mach 3 or better.

      The X-15 hit Mach 6.72, and its maximum burn time was under 5 minutes (it was a rocket plane though), so it makes sense for something like a hypersonic engine to be used for real flights, even NY-LA would be practical...under 1 hour door-to-door, no need for a crappy airline meal! The SR-71 has already done NY-LA in about 1 hour at Mach 3.5.

      --
      A man's reach must exceed his grasp, or what's an erection for?
    10. Re:Actual Destinations? by tony_gardner · · Score: 2

      True, except that the heat loads on a vehicle at this speed, at atmospheric pressure, are enormous, as is the drag. That's why they fly at altitude. I guess a simpler way of thinking about it is: if you can only shed your nose cone at 25km altitude (to prevent excessive heat load on the engine), how fast would the rail gun have to launch you at sea level to be going Mach 7 at 25km altitude?

      I haven't done the Maths on it, but I suspect that a rocket launcher would actually be cheaper.

    11. Re:Actual Destinations? by uncoveror · · Score: 2

      Wow! You know about the base. I am glad the real news is finally getting out.

      --
      The Uncoveror: It's the real news.
    12. Re:Actual Destinations? by Waffle+Iron · · Score: 4, Interesting
      What you do have the potential for (given significant further progress) is very fast cruise missiles, not ICBM's.

      Very fast ramjet cruise missiles were under development in the 1950's, but they fell out of favor because ICBMs are even faster and just about impossible to shoot down. However, they did look way cooler than today's boring ICBMs.

    13. Re:Actual Destinations? by afidel · · Score: 2

      There will be no "low-speed" version of this! Scramjets only work at hypersonic speeds, the whole need for the rocket was to get the scramjet up to speed so that it could operate. There are theoretical designs for an engine that would work as a normal jet engine to get the vehicle up to speed and then reconfigure itself to a mode that would allow for scramjet operation, but they are mechanically complex, more failure prone and almost surely more expensive to make, so what will probably happen will be multi-engine systems where you will have say 4 engines, 2 traditional jet engines and 2 scramjets, you take off and land with the traditional engines and cruise with the scramjets.

      --
      There are 4 boxes to use in the defense of liberty: soap, ballot, jury, ammo. Use in that order. Starting now.
    14. Re:Actual Destinations? by Jucius+Maximus · · Score: 1

      I read about 'the base' back in ~1995 or possibly earlier in documents allegedly written by one 'Milton Cooper' , supposedly ex-USAF personnel.

    15. Re:Actual Destinations? by RobertNotBob · · Score: 1
      The terminology HYPERSONIC implies faster than mach 5. If I remember correctly, the simple explaination is that at mach 5 there is a aerodynamic barrier that you can think of being similar to the sound barrier (mach 1).

      Remember that everybody made a big deal about breaking the sound barrier? That's because going mach 1.1 is much more than 20% harder than going mach 0.9. Likewise going mach 5.1 is MUCH harder than going mach 4.9.

      Once you have gotten hypersonic though, you are theoreticly OK until the friction of the air you are traveling through melts your plane. Which of course has to do with the selection of materials, not the ability of the propulsion system.

      --
      ___ I don't respond to Anonymous Cowards, and I Never Mod them UP.
    16. Re:Actual Destinations? by timeOday · · Score: 1

      But wouldn't the scramjet work at lower speeds in denser atmosphere, or not?

    17. Re:Actual Destinations? by tony_gardner · · Score: 2

      Mach 4 at 1 bar doesn't have the same heat load as Mach 7 at 0.02 bar. And you need to be going faster than your cruising speed anyway if you want to launch from a rail gun.

    18. Re:Actual Destinations? by gilroy · · Score: 3, Informative
      Blockquoth the poster:

      At a practical level, once you're travelling at 7.6 Mach, wouldn't you already be at your destination by then?

      Our monkey brains can't really appreciate the size of this Earth. Circumference = 24,000 miles. Mach 7.6 = 5000 mph. So it'd take about 5 hours to circumnavigate the globe -- or about 2.5 hours to reach the opposite point on the other side of the world.


      Depending on lift ability, this could have fascinating implications for rapid-response troops.


      But more importantly, it's potentially an excellent way to lower costs to get things into orbit. And air travel is all well and nice, but the future is in space travel, at least to LEO.

    19. Re:Actual Destinations? by gilroy · · Score: 2
      Blockquoth the poster:

      I know that if I go on vacation, I would rather not have to strap myself to an MK 70 Rocket before the preflight movie.

      Don't take this the wrong way, but nobody gives a damn what your vacation preferences are. It'd be used for extremely urgent deliveries; rapid-deployment troops; or -- and this is the payoff -- launch assit to low earth orbit. Air travel is so, well, 20th century. :)
    20. Re:Actual Destinations? by thogard · · Score: 1

      The problem with scram jets is you have to be moving very fast before they start working at all. That speed just happens to be about mach 7. These types of engines might be able to get up to about mach 15 before you run out of air. To escape velocity is about mach 33. If you could keep the thing in the high atmosphere at the point were you have enough air to keep accelerating but not too much that you burn up. The idea of these is to gain enough speed to put something in orbit whithout hauling around all that O2. When you consider that the upper atmosphere isn't all that well understood as thundersorms can double the air density 200,000 ft above the storms and that would be like hitting a wall at mach 15.

    21. Re:Actual Destinations? by Xaoswolf · · Score: 2
      nobody gives a damn what your vacation preferences are. It'd be used for extremely urgent deliveries;

      fair enough

      scramjet payload and impacted some 370km downrange of the launch site

      please note the word impacted, not the way I'd want them to send the heart I need for my transplant.
      There is a lot of work to be done here before it can be used for anything other than a missile right now, and unfortunately, they don't have the funding for another launch.

    22. Re:Actual Destinations? by IsoRashi · · Score: 1

      Even more practically, according to the article at New Scientist you have to be travelling Mach 5 to even get the engine to ignite. Perhaps this is why they had to launch it on a rocket and then attempt ignition as it re-entered the earth's atmosphere.

      I talked with a buddy of mine who is really into aviation, and to the best of his knowledge, even our (i.e. the US) best and newest fighter jets top out around Mach 4. While this jet engine certainly seems amazing (I mean, c'mon, it's Mach 7.6!), it doesn't seem like there are really any practical uses for it on Earth at this time.

      --
      This is not the greatest sig in the world, no. This is just a tribute.
    23. Re:Actual Destinations? by f97tosc · · Score: 1

      Passenger traffic will probably be the last application.

      But there are tons of military possibilities: Bomber/ spyplane that not only gets to the target extremely fast, but can outrun all antiaircraft weapons (including missiles).

      -Tor

    24. Re:Actual Destinations? by limekiller4 · · Score: 1

      starman97 writes:
      "Now, getting to Mach 7.6 to light one of these off may take a railgun, something that rules out living payloads, but good for launching cheap infrastructure into LEO."

      Apologies in advance for splitting hairs (because that's more or less what I'm doing), but it needn't be cheap nor LEO, but it would help if it was hardened if you're going to railgun it up. =)

      --
      My .02,
      Limekiller
    25. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      "best and newest fighter jets top out around Mach 4"

      This is a very strong argument for the value of scramjets in military applications.

      Furthermore, while jet fighters can breach the sound barrier and fly at a couple of Machs, they do so at an extremely high fuel cost, and thus short range. While this has been improved dramatically in the JSF, it could perhaps (now I am speculating) be improved much further in a scramjet.

      -Tor

    26. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      um....well... this is what is called
      "proof of concept" silly boy. I am sure that when the wright brothers were testing thier first aircraft you would have been there naysaying and talking about how horses were so much better. This is the first step. of course if it were in commercial use you wouldnt have to strap a frikkin rocket on your ass. please think before you post.

    27. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      Doing some dumb math? I come up with a launch speed of about mach 8. that doesn't factor in all that friction while going super-sonic.

    28. Re:Actual Destinations? by realmolo · · Score: 0

      Why use a bomber or a spyplane when you can use a missile and a satellite? Both of which are much faster and much harder to shoot down.

    29. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      IIRC, the SR-71 was going mach 3.5 or approximately that when it passed over LA, no acceleration accounted for, basically. Makes sense too, cause the SR-71 dosen't take off with a full load of fuel, but instead is refueled mid-air before it's mission.

    30. Re:Actual Destinations? by reallocate · · Score: 1
      You won't see it used for puddle-jumping. The speed of sound at sea level is about 760 miles per hour (1225 kph); it's variable per the nature and density of the medium, so in the atmosphere at 20,000 feet it drops to 660 mph (1062 kph).

      So, let's drop it down to an over-ambitious 600 mph, since scramjet-powered craft will be flying considerably higher than 20,000 feet. Multiply by 7.6 and you get 4560 mph, In other words, a tad faster than the fastest speed reached by the X-15 decades ago.

      The point of this thing is to test technology that might allow operational craft to go faster for less money. Very practical if you need to launch small satellites or get people or cargo from, say, Berlin to Tokyo in 3 hours. Or New York to Los Angeles in about 40 minutes.

      --
      -- Slashdot: When Public Access TV Says "No"
    31. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      Ok, I visited the uncoveror site. I give up, is it a parody or not? The story of the "Any" key had me rolling.

    32. Re:Actual Destinations? by k3n-54n · · Score: 1

      Agreed, if you say "first uses". Later, who knows? I fly SF to Japan frequently, and there are sceduled flights NY to Tokyo, which could benefit from this technology, later, when it is more developed. (Comment about banning cars right on. Applies to guns, too.)

    33. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      A bomber can double as a transport for ground troops.

    34. Re:Actual Destinations? by spike+hay · · Score: 2

      There was one supersonic ramjet cruise missile that actually reached hypersonic speeds. I forgot the name. But during one test, the fuel feed got stuck on full throttle, and the cruise missile reached Mach 5.5 with no problem.

      Ramjets have been around for years and can reach Mach 5. Why not use them? All that you would need is a couple of turbojets to reach transonic speeds, then you can fire the ramjet and your are off.

      (BTW, a scramjet would need a turbojet to reach supersonic speeds, a ramjet to reach low hypersonic speeds, and finally a scramjet to accelerate to high hypersonic speeds)

      --
      If you don't understand any of my sayings, come to me in private and I shall take you in my German mouth.
    35. Re:Actual Destinations? by spike+hay · · Score: 2

      2 traditional jet engines and 2 scramjets, you take off and land with the traditional engines and cruise with the scramjets.

      Actually, you would need three sets of engines: Turbojet to reach supersonic speeds, ramjet to Mach 4 so the scramjet can operate.

      The practical limit of turbojet engines is about Mach 2.5, not nearly fast enough for the scramjet. The reason the SR-71 exceeds Mach 3 is that it uses a turbo-ramjet engine. When it gets to a certain speed, all the air and fuel is bypassed and burns independant of the turbines (which completely shut off). This allows the turboramjet to reach higher speeds that a turbojet.

      --
      If you don't understand any of my sayings, come to me in private and I shall take you in my German mouth.
    36. Re:Actual Destinations? by Anonymous Coward · · Score: 0

      Not quite true.

      At Mach 3 cruise the J-58 engines have a bypass (after the fourth compressor stage?) sending most of the air to the rear. The result is about 30% of the thrust comes from the turbojet, and about 70% from the second, ram-jet like system. The turbine section *DOES NOT* shut down.

      Pedants argue that because the bypass comes from after the initial compressor stages the result is not a true ram-jet, but for me it's close enough ;-)

  6. text of the abcnews.au article (slow loading) by Anonymous Coward · · Score: 0

    Scramjet success makes history

    (subtitle:) University of Queensland researchers are celebrating the world's first successful test flight of an air-breathing hypersonic "scramjet" engine.

    Data for last month's flight at Woomera in South Australia indicates the rocket achieved supersonic ignition in the atmosphere, a world first.

    'Hyshot' project leader Allan Paull says the engine reached Mach 7.6, or 7.6 times the speed of sound during the test on July 30.

    It has taken until now for the team to analyse the full flight data.

    A speed of Mach 7.6 would allow airliners to travel from London to Sydney in two hours, compared to more than 20 now.

    "We do believe we achieved supersonic flight for the first time," Mr Paull said.

    The test over the central Australian desert was the first time engineers have made the supersonic scramjet engine work outside an air tunnel.

    The team fired the scramjet engine into the sky on the back of a Terrier Orion Mk70 rocket, which took it into the upper atmosphere.

    The engine kicked into action on the way back down at 35 kilometres above the earth, with data transmitted by radio until it began to burn up.

    A year ago, the US space agency NASA's test of its multi-million dollar unmanned X-43A scramjet prototype failed.

    A previous attempt by the HyShot crew went awry when a rocket used to launch the engine spun out of control.

  7. Mach 7.6 !! by af_robot · · Score: 3, Funny

    Wow!
    This must be twice better than Gillete Mach3 system !!

    1. Re:Mach 7.6 !! by yeoua · · Score: 4, Funny

      Depends on what you think is better. The Gillete Mach3 system will take 3 swipes at your hair. This Scramjet system seems to attempt to take a record 7.6 swipes at your hair. Not sure how they do the .6 of a blade though... but from the commercials, the 3rd blade seems to essentially get as close to the skin as possible. So then the 4th blade must then (in a logical progression) take of the top layer of skin. The 5th blade then takes out the middle layer of skin. The 6th blade takes out the lower layer of skin. This is a highly good design as if you shave really fast, by the time it hits the 6th blade you should have shaved off all your nerves so it shouldn't even hurt anymore.

      Which leaves the 7th blade to shave off some bone, to polish it maybe. Now that .6 of a blade that is left... maybe its some new encryption scheme for their razor so no one can exactly copy their design, as who would want to make .6 of a blade? Perhaps it means its only 60% as sharp as the rest of the blade and used to buff your bone?

      Well then, this has to be the closest shave you'll get, and with your skin gone, you should have no growth after, as the bulbs should have been rooted with that skin by then.

    2. Re:Mach 7.6 !! by Anonymous Coward · · Score: 0

      "buff your bone"

      Err...I'll get my coat.

      Steve.

    3. Re:Mach 7.6 !! by Anonymous Coward · · Score: 0

      The .6 of a Blade is the new ceramic composite FRACTAL edge. The tiny wrinkley boundary gives almost infinite length & thus infinte sharpness. It would be in fact .66666 of a blade but given the trouble Proctor & Gamble had with their Moon & Seven Stars logo a few years ago maybe we won't go there.

    4. Re:Mach 7.6 !! by aengblom · · Score: 2

      Where's my +1 Disgusting!

      I mean come on /. editors! What were you thinking not including that!

      --


      So close and yet so far from the world's perfect ID number
    5. Re:Mach 7.6 !! by Rasta+Prefect · · Score: 2

      I knew there was a reason I still read the slashdot comments. Bravo!

      --
      Why?
    6. Re:Mach 7.6 !! by netwiz · · Score: 1

      We are all dumber for having read that.

      Can I get my 15 seconds back?

      heh. actually, I did find it amusing :)

  8. confusion by Anonymous Coward · · Score: 0

    This is a question posed out of honest ignorance. How can they be unsure of their success? You can tell if the jet broke the sound barrier by the sonic boom, and if you know supersonic speeds were obtained, you know the jet's propulsion system worked. What is the uncertainty about?

    1. Re:confusion by snatchitup · · Score: 3, Informative

      It's not how fast, but how did they fly that fast.

      The Scramjet theory has to have occurred. Which is basically an engine with no moving parts. The intake air has to hit the fuel so fast, and at such high density that some sort of "Critical Mass" combustion takes place that produces more thrust that drag of the air molecules hitting the craft at about 10kph.

      When you're on a shoe-string budget, it's hard to figure out if that really happened. It'll take a much more expensive project to figure this out for sure, hence, NASA's much more expensive project.

      Who needs this anyway, with
      Sydney's Mardi-Gras going bankrupt!

      Hello Frisco!

    2. Re:confusion by tony_gardner · · Score: 2

      When you're on a shoe-string budget, it's hard to figure out if that really happened. It'll take a much more expensive project to figure this out for sure, hence, NASA's much more expensive project.

      Not really, a pressure distribution along the combustion chamber was measured. You need to check two things. Is the gas supersonic, and was combustion achieved. Supersonic can be checked by comparing the pressure in the combustion chamber with that predicted due to wedge compression.

      Combustion is shown by comparing the signal in one chamber with no fuel, with the signal in the second chamber with fuel.

      In addition, supersonic combustion in a parallel combustion chamber gives a pressure profile which rises along the chamber, whereas subsonic combustion gives a pressure profile which drops along the combustion chamber.

      The real trick is to check that nothing else could simulate these signals.

    3. Re:confusion by AlecC · · Score: 1
      The scramjet works only at supersonic speeds. So the test vehicle had an ordinary booster which took it up to, and through, Mach 1. When they had a supersonic airflow, they turned on the scramjet - but for only 10 seconds (I can't think why so short, but that is what it said). Sop, from the ground, there would have been little differnce in what they saw - a change of a few miles in the 350 mile trajectory, but that might be experimental error. So they had to wait for the telemetry - e.g. a surge in acceleration as the scramjet fired.

      This is very interesting, but don't get too excited. This was basically a firework, and it is a loooong way from here to a flyable payload-carrying plane. The first objective, as they say, is probably cheap satellite launches - essentailly another firework. probably a good vehicle for Amsat-type launches.

      --
      Consciousness is an illusion caused by an excess of self consciousness.
    4. Re:confusion by snatchitup · · Score: 1

      This is very interesting, but don't get too excited. This was basically a firework, and it is a loooong way from here to a flyable payload-carrying plane.


      My sentiments exactly. And how far past Mach 1 must it go before it can actually work? Does it have to go all the way to Mach 7 first?

    5. Re:confusion by tony_gardner · · Score: 2

      Opinions vary. Estimates of starting Mach numbers range between Mach 4 and Mach 6.

    6. Re:confusion by Mt._Honkey · · Score: 2

      They didn't just bring it up to high speed and turn the engine on. They shot the thing up to an altitude of 314 km, pointed it to the ground, and let it fall, all the way (it is unclear to me if it was a powered dive (before the scramjet)). Only as it got near the ground did the engine activate, and then only for a few seconds before it heated up from re-entry. Then it cratered into the desert.

      --

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    7. Re:confusion by The+Dobber · · Score: 1

      "It'll take a much more expensive project to figure this out for sure, hence, NASA's much more expensive project"

      Don't you mean much more expensive failures? Or could this be the dawn of a new NASA era. Low-cost failures, followed by high cost successes.

  9. Sheesh... by Anonymous Coward · · Score: 0

    "the engine achieved combustion in flight after reaching Mach 7.6. "

    I'm quite sure I would combust as well when I'm going mach 7.6!!

  10. Read the article? by yatest5 · · Score: 1

    "A speed of Mach 7.6 would allow airliners to travel from London to Sydney in two hours, compared to more than 20 now."

    --
    • Mod parent up! [a] by Anonymous Coward (Score:5) Thurs, June 31, @13:37
    1. Re:Read the article? by Anonymous Coward · · Score: 0

      In order to do that you would have to fly over some form of land mass, and afaik no country allows passenger jets to fly mach 1 or higher over their airspace.

    2. Re:Read the article? by Xaoswolf · · Score: 3, Interesting

      You are correct, from start to finish, if you are traveling at mach 7.6 the flight would take 2 hours. But the question was, how long would it take to get up to mach 7.6. How far along on your flight would you be before you reached that speed.
      The test flight used a small craft, not a large passenger jet. It would be both easier and faster to reach that speed in a smaller light craft(and even then they used a MK 70 rocket engine, which I'm pretty sure isn't rated for passengers). Even if they were to just use a rocket or catapult(like on an aircraft carrier) to bring you to that speed faster, the G's would be immense, I'm not even sure if a G-suit would keep you from blacking out. And as stated earlier, if you gradually were to gain speed until you reached that point, you would be almost at your destination before you reached mach 7.6, and it would be time to start slowing down for landing.

    3. Re:Read the article? by AndrewHowe · · Score: 2

      How does Concorde get away with it?

    4. Re:Read the article? by AndrewHowe · · Score: 2

      OK, I checked, and it doesn't... Concorde only goes supersonic when it gets to the water. This is why it has so few routes.

    5. Re:Read the article? by k3n-54n · · Score: 1

      Acceleration would not be a big deal. Get real. A muscle car that gets to 60 in five seconds feels exhilarating, but no danger of blackout. 600 in 50 seconds, mach 10 in 10 minutes, no problems.

    6. Re:Read the article? by Xaoswolf · · Score: 2

      There happens to be a rather large difference between the engine on a scramjet and the engine in a muscle car. If the acceleration were not all that hard, I think that they would have found a getter way to do it than a MK70 rocket engine.

    7. Re:Read the article? by JohnPM · · Score: 2

      Yeah but they weren't trying to transport humans with the MK70, so why invent a low-G accelerator when all they wanted to do was test the scramjet?

      --
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    8. Re:Read the article? by k3n-54n · · Score: 1

      You are incorrect, apparently confusing acceleration with speed. Acceleration can be easily calculated by dividing final speed by time. It is not so bad. There is a problem of finding an engine that can go fast enough. The MK70 helped out there, where no typical engine would have.

  11. Photos, other links, and more by danish · · Score: 5, Informative

    There's a ton of photos at http://photos.cc.uq.edu.au/HYSHOT/ and also at http://www.mech.uq.edu.au/hyper/hyshot/HyShot_phot os.html. The former link has some friggin huge jpegs.

    There is also a page about the HyShot program itself at http://www.mech.uq.edu.au/hyper/hyshot/

  12. How does this affect global warming? by TeamSPAM · · Score: 1

    Consider the artilce we saw on here the other day. What would a Scramjet's exhaust do to raise the global tempature?

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    1. Re:How does this affect global warming? by Anonymous Coward · · Score: 0

      I hope it helps. I mean come on, I was swimming last night, and the water temperature didn't even break 80. It's mid-summer man! My water should be up to 84 degrees. Hopefully this Scramjet will warm things up real nice nice.

    2. Re:How does this affect global warming? by Oztun · · Score: 2

      It could actually help. If it takes a normal plane 20 hours to get from Sydney to London and this one 2 that is 18 less hours in the air per flight. Of course that all depends on the exhaust ratio of the two planes.

    3. Re:How does this affect global warming? by DigitalLogic · · Score: 1

      Well first, the hydrocarbons will be throughly mixed into the upper atmosphere with a double dose injection. Then the sonic compressions will blast the foul mixture miles wide in trillions of cubic meters of air per centimeter. This will contribue both to global warming and ozone depletion. Though, by the time scientists figure this out, scramjets will be the only mode of transportation.

  13. Mach speeds by andyring · · Score: 2, Interesting

    The thing I don't like about Mach numbers is it's not consistent. Reason being, the speed of sound changes based on your altitude. Higher, where the air is thinner, sound travels slower. So Mach 7.6 at 50,000 feet is a lot slower than Mach 7.6 at sea level. Sure, it's a cool sounding number, but I wish we'd see these numbers represented in miles or kilometers per hour as well as a Mach speed. When the author of the article gave the comparison of a London-Sydney flight, (2 hours vs. 20), was he/she figuring that based on Mach 7.6 at sea level or at 75,000 feet? (not to metion it'll be decades before, if ever, we see passenger planes anywhere near this speed)

    1. Re:Mach speeds by jamie · · Score: 5, Informative
      "The thing I don't like about Mach numbers is it's not consistent. Reason being, the speed of sound changes based on your altitude. Higher, where the air is thinner, sound travels slower."

      Untrue. Sound travels slower because the air is colder, not thinner. The speed of sound in the Earth's atmosphere is proportional to the square root of the temperature, nothing else. http://www.allstar.fiu.edu/aero/mach.htm

      Here's an atmosphere simulator where you can pick an altitude and see the speed of sound. As it says, "the speed of sound depends on the temperature and the gas," not on pressure.

    2. Re:Mach speeds by jshine · · Score: 1

      Hah -- very true, although I hadn't thought of that much before. It is meaningless (outside of certain fluid flow problems, anyway). At least I haven't come across anyone trying to apply Mach numbers to spacecraft yet. Now *that* would be funny.

    3. Re:Mach speeds by jshine · · Score: 3, Interesting

      Well, that's kinda deceptive really, because pressure and temperature are very related for a gas. If you model the gas as idea, then you get the relationship:

      P*v=R*T (where v=V/N) or, if you'd rather use density...

      density (rho) = P*M/(R*T)

      So, you can have temperature in terms of pressure, or pressure in terms of temperature. They are interrelated: with a gas, you can't change one of those parameters in isolation.

    4. Re:Mach speeds by Marx_Mrvelous · · Score: 2, Insightful

      His statement is entirely true; as altitude increases, the air does indeed grow thinner, and the speed of sound indeed decreases. And the sped of sound is definitely linked to density, which is why it travels so much faster in water than in air (even at the same temperature).

      --

      Moderation: Put your hand inside the puppet head!
    5. Re:Mach speeds by tony_gardner · · Score: 2

      Actually for Hyshot, the design temperature was 220 Kelvin. A weather balloon was sent up beforehand, to make sure that the air wasn't so cold as to suppress combustion.

      The Mach number is a similarity parameter. That is, all craft travelling at Mach 7.6 experience similar problems, regardless of the actual speed. Other similarity parameters include the Prandtl, Reynolds, Stanton and Damköhler numbers.

    6. Re:Mach speeds by Idarubicin · · Score: 1
      Sound travels slower because the air is colder, not thinner.

      Quite right. Temperature--and only temperature--determine the speed of sound in a given gas. (If we neglect certain very small effects.)

      Thinner doesn't affect speed of sound, and here's why in a nutshell.

      Loosely speaking, sound propagates through energy passed from one molecule of air to the next by collisions between molecules. (No one can hear you scream in space because there's no chain of colliding molecules between the screamer and the audience.) Large groups of molecules with a slightly larger (or smaller) than average amount of kinetic energy appear to be the regions of high (and low) pressure we know as sound waves.

      The speed with which these waves move is controlled by how quickly molecules can move their energy out from the sound source, to pass to molecules further out. Since this energy is transferred through collisions, each molecule must physically traverse the distance between interactions. The speed with which each molecule moves is directly related to its kinetic energy--in other words, its temperature. And only its temperature.

      Pressure will affect the rate of sound attenuation in a gas, but not the speed at which sound travels.

      --
      ~Idarubicin
    7. Re:Mach speeds by delcielo · · Score: 2

      Exactly. I think the difference between pressure and density is causing confusion.

      --
      Hot Damn! It's the Soggy Bottom Boys!
    8. Re:Mach speeds by Zathrus · · Score: 2

      Mach is an accepted measurement of speed, and when used as such it does indeed have a specific value. Reference Mach is measured at 15 deg. Celsius at sea level, yielding ~340 m/s or 1224 km/h (someone feel free to doublecheck the math, conversion and multiplication errors abound when you post).

      So while, yes, the speed of sound does indeed change with altitude (due to temperature changes, which is related to pressure changes), the reference Mach value does not. So Mach 7.6 was 9306 km/h or 5784 mph.

    9. Re:Mach speeds by tony_gardner · · Score: 2

      This is true in a closed system, without heat addition. This is not the atmosphere. In the atmosphere the Pressure dropps off logarithmically, but the temperature makes a kind of sinusoid.

    10. Re:Mach speeds by tony_gardner · · Score: 2

      No, actually you can work it out. The speed of sound in a gas in meters per second is equal to sqrt(ratio_of_specific_heats*8.314*Temperature/mas s_of_one_mole_in_kg)
      The only pressure dependance is a very small one, through the ratio of specific heats. Basically the speed of sound in a gas is independant of pressure and density.

    11. Re:Mach speeds by wordprocessing · · Score: 1

      Mach number should be consistant. It's just a way to make the number more relevant.. I am assuming that the author of the article was using speed of sound at sea level not at 75000 feet because who cares what the speed of sound is at 75000 feet?

    12. Re:Mach speeds by gilroy · · Score: 2
      Blockquoth the poster:

      Basically the speed of sound in a gas is independant of pressure and density.

      IANAAE (I am Not an Aeronautical Engineer), but isn't this due to the assumption of ideal behavior? In Physics, you learn that the speed of sound is proportional to sqrt(dP/dD), ie., dependent on the derivative of pressure with respect to density. This makes actual physical sense, as it connects the restoring force (via the pressure) to the inertia of the gas (via the density).


      In an ideal gas, P = DRT, so dP/dD = RT. And hence the dependance on temperature and the apparent independence from P and D.

    13. Re:Mach speeds by jshine · · Score: 1

      The pressure equation of state is true generally (if you make the ideal gas assumptions), whether the system is adiabatic, isothermal, isobaric, any particular set of (physically realistic) conditions you wish to choose. It is true that in the atmosphere there are some non-intuitive trends, but that's because it takes a *whole lot more* than a simple equation of state to model something as complex as the atmosphere. Heat transfer must be take into account: convection, conduction and radiation. Of course, an equation of state would be useful (and valid) also, but it's just not the whole story...

    14. Re:Mach speeds by Anonymous Coward · · Score: 1, Informative

      The equations you will find in most aerospace texts go as follows. There are, aparently, more complicated formulas but for 99% of the cases these are accurate.

      a = speed of sound (m/s)
      v = velocity of vehicle (m/s)
      M = mach number
      G = gamma - gas constant (1.4 for air)
      R = gas constant (can't remember units but =288 for air)
      T = Temperature (kelvin)

      a = sqrt(GRT)
      M = v/a

      speed of sound is directly related to temperature and type of fluid.

    15. Re:Mach speeds by Anonymous Coward · · Score: 0

      The thing I don't like about Mach numbers is it's not consistent.

      Mach numbers are dimensionless (m/s divided by m/s = no units). Dimensionless numbers are very important in engineering and physics because they describe physical phenomena for a wider variety of situations than the dimensional equivalent. If I say "an object traveling greater than 330 m/s creates shock waves," that's only true in air at the surface of the Earth. If I say "an object traveling greater than Mach 1 creates shock waves," that's true in any fluid (gas or liquid) anywhere in the universe.

    16. Re:Mach speeds by vladkrupin · · Score: 1

      Oh, yes, talking about mach speeds... Quoting from the article:
      "We do believe we achieved supersonic flight for the first time," Mr Paull said
      Huh? So, how fast does, for example, Concorde fly?

      --

      Jobs? Which jobs?
    17. Re:Mach speeds by grgyle · · Score: 2, Interesting

      "Untrue. Sound travels slower because the air is colder, not thinner.." No. First off (for qualification's sake), I have degrees in Physics and Astronomy and work professionally as an engineer. You are misunderstanding the pressure/volume/temperature relationships of the gas laws (freshman physics material). One can express mach number in terms of a pressure dependency, a temperature dependency, or a density dependency. For an ideal gas, the parameters are interrelated. Go back and really read the equations on the web page you quoted. It is equally as true to say mach is density dependent as it is to say it is temperature dependent for a given gas.

      --
      ----- And all that the Lorax left here in this mess was a small pile of rocks, with one word...UNLESS.
    18. Re:Mach speeds by colonel_zentor · · Score: 1

      actually, the speed of sound doesn't change that much from sea level to 100,000 ft (even up to 260,000). at sea level the speed of sound is 1,117 ft/sec and at 100,000 ft it is 971 ft/sec. thus there is about only a 15% differece between the two. so to make it easy, just figure that the speed of sound is roughly 1000 ft/sec (681 mph) for any altitude. so mach 7.6 is about 7,600 ft/sec or 5,181 mph. mach number is typically quoted because engineers love non-dimensional numbers.

    19. Re:Mach speeds by Anonymous Coward · · Score: 0

      I suspect the qualifier "...with scramjet propulsion" was omitted by the speaker or the writer. Concorde is supersonic (as are any number of military aircraft), of course, but not a scramjet.

    20. Re:Mach speeds by WolfWithoutAClause · · Score: 2
      Actually, I feel you're the one being deceptive.

      The temperature is given in terms of pressure AND volume, or density and pressure. For any given temperature you can have any pressure at all by varying the volume. THERE IS NO DIRECT RELATIONSHIP BETWEEN PRESSURE AND TEMPERATURE.

      The volume of the atmosphere can and does vary.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
  14. A matter of practicality by ArmenTanzarian · · Score: 0

    1. You can get from England to Australia in two hours, but what about going to America. You'd be up there for all of like 5 minutes and pay millions of dollars to do it.

    2. Military applications, huuuge negative. Yeah, we might be able to move people and equipment faster. But then again crazies in various countries will be able to lob things at us faster. The Star Wars program isn't really ready to stop this yet.

    3. What do they feed you on these things, roasted peanuts or Tang?

    1. Re:A matter of practicality by Anonymous Coward · · Score: 0

      Until Mr. Hussein and Co. can build thier own scramjets...

      We could have had troops in Kuwait City hours after the first Iraqi tank crossed the border.

    2. Re:A matter of practicality by MaxVlast · · Score: 1

      Don't forget the two hour airsickness puking recovery time before the troops would be ready for action.

      --
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    3. Re:A matter of practicality by nochops · · Score: 1

      1. Then use a normal plane, dumbass. Trust me, no one will force you to use this.

      2. Crazies in various countries? This is being developed in Australia, not the US. So it's already in one "various" country.

      --
      "A terrorist is someone who has a bomb but doesn't have an air force." -William Blum
    4. Re:A matter of practicality by mprinkey · · Score: 2, Interesting

      Um, just as a point of reference, ICBMs travel much faster than Mach 7. On suborbital trajectories from the other side of the globe, you might see a time of flight of 30 minutes or less. Think 20,000 km/hour.

      Scramjets are not really interesting as strategic weapons. Extra-atmospheric vehicles (MVRs) are faster and proven 30-year-old tech. Scramjets are going to be useless for cruise missiles, because a Mach-7 shock cone will standout rather nicely even if the missile itself were stealthy. Depending on the altitude, it could also cause ionization of the atmosphere which would show up on radar!

      Military applications here are going to be reactive in nature...fighter-bombers that can reach any corner of the globe in two-hours is a big selling point, as is the (literally) stratospheric flight ceilings such crafts would have. But I don't know what form a scramjet-based weapons system might need to take or what niche it might fill.

    5. Re:A matter of practicality by Anonymous Coward · · Score: 0


      yes but in the future movie version it will take place in America

  15. Mach 7.6- isn't that a little tough for travellin? by glh · · Score: 2

    While scramjets raise the possibility of Sydney to London flights in two hours, they are set to revolutionise the launch of small space payloads, such as communications satellites, by substantially lowering costs. They have the added benefit that they do not even have to carry most of their propellant as they use oxygen from the atmosphere.

    Just wondering, but wouldn't travelling at Mach 7.6 be a little tough on a human? I'm no physisct, but it seems like the G's would be something really painful for a human. Of course, maybe the two hour flight from London to Sydney wouldn't require Mach 7.6 speeds.

  16. Just a question: by Space_Nerd · · Score: 1

    What's the difference between a normal jet engine and a scramjet?

    --
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    1. Re:Just a question: by smagoun · · Score: 4, Interesting
      What's the difference between a normal jet engine and a scramjet?

      Almost everything. Normal jet engines have lots of moving parts - turbines, compressors, etc. Ramjets and scramjets don't have any moving parts. They also require very high velocities to work properly, whereas a turbojet/turbofan is quite happy running all day long without moving.

    2. Re:Just a question: by YaRness · · Score: 2, Funny

      remember, google.com is your best friend.

      scramjet

    3. Re:Just a question: by jedman · · Score: 1


      >> whereas a turbojet/turbofan is quite happy running all day long without moving

      Sounds like the last time I was stuck all day on an airport taxiway due to weather delay :)

    4. Re:Just a question: by WolfWithoutAClause · · Score: 2
      Main difference?

      Scramjets melt in a few minutes. Jets usually don't melt.

      ;-)

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    5. Re:Just a question: by jake-in-a-box · · Score: 1

      A scramjet is a supersonic combustion ramjet. A ramjet is a very simple (mechanically) jet engine that relies on the speed of the vehicle to force air into and compress air in the combustion chamber.

      The key is the supersonic part. Conventional jet engines - all of them, pulse jets, turbojets, ramjets etc. - combust at subsonic velocities. That's a problem, because when a vehicle travels at supersonic velocity, it must slow the air coming into the engine to subsonic velocity (relative to the vehicle, that is). This requires complex inlet shapes, and the right shape varies as the speed of the vehicle does - and obviously there's the subsonic/supersonic transition to consider too. The variable geometry inlets that you see in vehicles like the SR71 are the means that engineers do this. Obviously it adds weight and comlexity, but it also limits the speed of the vehicle, because at some point you get a diminishing return, slowing the air causes drag, which becomes more of a problem as you go faster. Result, subsonic engines have a speed limit. The solution is supersonic combustion.

      Supersonic combustion is a neat trick. The fluid mechanics courses courses I attended in engineering school, for the sake of convenience, basically viewed supersonic combustion as an oxymoron and not possible. After all, the flamefront moves as molecules collide, and molecules colliding is the definition of the speed of sound in that medium. Therefore you can't have combustion moving through a medium faster than the speed of sound in that medium.

      So how does a scramjet work? Beats me, that's a miracle I was never exposed to. Another neat trick is that some scramjet designs do not even enclose the the combustion area, just shape the fuselage correctly. This is an esoteric field. The Russians used to be the leaders back in the cold war days. I guess they don't have enough cash to keep up the work now.

      Post Comment

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  17. Where to land it by imperator_mundi · · Score: 1

    I'm just wondering at what a speed would these planes land and how long must a slope be to allow a non catastrofic landing.

    If I'm not wrong shuttles land on slopes of 15 km, but they're much faster than mach 7

    1. Re:Where to land it by jlharris_50010 · · Score: 1

      I am pretty sure that the shuttle isn't going Mach 7 when it lands... How can that little plane be flying next to it?

  18. Re:Mach 7.6- isn't that a little tough for travell by azadrozny · · Score: 1
    I would have to aggree. Mach 7.6 would be a bit too much for your average passenger. Fighter jet pilots train for hours on how to keep concious, they are also in excellent physical shape and have a lot of equipment to help them.

    Even if you did find a few willing souls, would it be enough to make any kind of profit? If I am not mistaken, it costs about $8,000 USD to fly on the Concord and they still have problems making money.

  19. Who the hell modded this up? by Arcturax · · Score: 3, Insightful

    Seriously, read the damn article! It says that it cuts the travel time from London to Sydney from 20 hours to 2! Obviously you are not getting there the moment you take off. The Earth is a huge huge place and even at Mach 7.6, it will take you a while to get somewhere.

    --

    --Won't that be grand? Computers and the programs will start thinking and the people will stop. - Dr. Walter Gibbs
  20. Re:Mach 7.6- isn't that a little tough for travell by antar · · Score: 0

    It doesn't matter as long as you don't accelerate too quickly, I guess.
    Btw - did you know people raised the same point you just did about cars: "what? 60 km/h - no man can survive that!".

  21. Re:Mach 7.6- isn't that a little tough for travell by Anonymous Coward · · Score: 1, Informative
    I'm not sure if this is a troll, but as long as you're enclosed, the SPEED has nothing to do with it, you sound like those guys from the 19th century who thought train travel above 30 miles an hour would suck all the air out of people's lungs...

    Acceleration, on the other hand, is a problem. Ever been in a jet? I don't think it'll be worse than that.

    Big difference between speed and acceleration. What's Earth's orbital velocity again?

    You were right, though, you're no physicist.

  22. hmmm... by i_have_no_name · · Score: 0

    what are military applications of this technology? when used in commercial flight (if it is possible) jobs will be lost and no more plane food and crappy movies!

  23. Re:Mach 7.6- isn't that a little tough for travell by f3lix · · Score: 2, Informative

    It's only a high rate of acceleration that causes passengers to experience excessive G force. Once you've reached Mach 7, so long as you remain at a constant velocity nobody should notice how fast you're going.

  24. Re:Mach 7.6- isn't that a little tough for travell by Milk+and+Cookies · · Score: 0

    There's nothing physically stressfull about traveling at high speeds. The g force would only come into play when the plane changed speeds. This leads to the question of how long does it take to accelerate to Match 7.6? 7.6 G's would be bad for you, but a constant 1 G over a period of time would not. IIRC, a scramjet needs to be at very high speeds to work at all, so acceleration probably would pose a problem for commercial flights.

  25. Re:Mach 7.6- isn't that a little tough for travell by dj28 · · Score: 1

    Special suits are made for high G's. Once you reach high G's, the special suit squeezes the blood from your feet back up to your brain so you won't pass out. The human body (while wearing this suit) can handle around 9 G's. So I don't think this is feasable for passenger travel, as it takes special training with the suit and it costs a lot of money for the equipment.

  26. Re:Mach 7.6- isn't that a little tough for travell by GypC · · Score: 4, Funny

    G-force is created by acceleration, not speed. Otherwise the speed of Earth's orbit around the sun would crush us all.

    Nonetheless, I'd rather be in Sydney in 2 hours with a bloody nose and bruised ribs than endure a 20 hour flight with a bunch of Englishmen...

  27. Re:Mach 7.6- isn't that a little tough for travell by Dark+Nexus · · Score: 2

    I've been wondering that myself, and have been trying to find info on the limits of the human body (with no luck yet).

    At best, it would probably be uncomfortable, and that would make it unsuitable for commercial flights.

    It's the same reason we don't have flying wings for commercial flights - many of the passengers would be made uncomfortable during turns.

    --
    Dark Nexus
    "Sanity is calming, but madness is more interesting."
  28. Warp 7.6!! by Tottori · · Score: 1

    So when do we get to seek out new life?

    --
    use constant PERL_IS_BROKEN => $] >= 5.006;
  29. Re:Mach 7.6- isn't that a little tough for travell by Anonymous Coward · · Score: 0

    Gs are NOT MACH NUMBERS!!!!! SPEED is NOT ACCELERATION! Please, people, buy a CLUE.

  30. other applications? by Alien54 · · Score: 3, Interesting
    Some how I can imagine the military trying to figure out how to make this cheaply enough to use in something like an upgraded version of the Tomahawk Missile. (which currently run at about 600mph or so)

    Something like that would be impressive, and also would have definite mind bending impact on the popation below, just due to the sonic boom.

    --
    "It is a greater offense to steal men's labor, than their clothes"
    1. Re:other applications? by tony_gardner · · Score: 2

      Scramjets are not the ideal engine for missiles. Amongst other things, the whole front of the engine is required for the air intake, which doesn't leave much room for a guidance package. The next is that the nose of the missile itself would be hot, complicating any heat seeking guidance. the last is a practical issue. Solid rockets are incredibly reliable, and it would take a lot to trade reliability for a possible increase in range.

    2. Re:other applications? by mprinkey · · Score: 1

      You missed the biggest reason. Cruise missiles only fly at subsonic speeds by design. They are to be quiet and stealthy. Any supersonic signature is detectable with a simple network of microphones. Once you know it is coming, a cruise missle is easier to shoot down than a jet aircraft as cruise missiles typically don't have active countermeasures and certainly don't have a pilot to perform evasive manuevers.

    3. Re:other applications? by tony_gardner · · Score: 2

      Maybe... Say a missile is cruising at Mach 8, and Altitude 35km. The weak Mach angle is then 7 degrees, meaning that the missile would have gone 280km past the sensor before it was detected, now extend that to Mach 20 and 50km altitude, and you're up to 1000 km past the sensor.

    4. Re:other applications? by mprinkey · · Score: 1

      At Mach 20, you are definitely going to have atmospheric ionization. That is going to make your "cruise" missile light up a radar display.

      But your point is quite valid. It is the issue of detection versus tracking. If I have listening posts a few hundred km from my borders, I would be able to know that something was coming. If I have a fine grained detection network, I can know a lot about its flight path at the point of detection. But, I am not going to have a lot of time to react if it is travelling at Mach-8.

      Although, the missile will need to decelerate as it closes. The cruising altitude is going to be quite high, else the thing will burn up. So, it will have to fall much like a MRV.

      OK, I guess you could build a decent missile out of one of these, but I don't see how would be superior to a ICMB or MRBM.

      I am beginning to realize that I have read entirely too many Clancy novels. 8)

    5. Re:other applications? by tony_gardner · · Score: 2

      That is really the core of the problem. If its a missile, the engine can be sacrificed, so it doesn't really need to slow down at its destination, but a non-ballistic missile does need guidance, which is a challenge. The idea is that it would be superior to a rocket because it would be only 35% of the takeoff weight for the same payload. Launching civilian payloads to space is probably the best goal. It's not like the world desparately needs more methods of raining down destruction.

    6. Re:other applications? by delong · · Score: 2

      There are already supersonic cruise missiles and anti-ship and anti-air missiles. Russia especially has invested alot of capital into this area of weapons research.

      They aren't scramjets, but Mach 2.5 - Mac 5 ain't nothin to laugh at, either. ;)

  31. Re:Mach 7.6- isn't that a little tough for travell by Urban+Garlic · · Score: 3, Informative

    Assuming you weren't trolling:

    Mach 7.6 is a speed, not an acceleration. A hypersonic passenger vehicle will presumably travel with moderate acceleration until reaching high speed.

    At 1/2-earth-gravity acceleration, you get one sea-level Mach number per minute, more or less, so you'll be at Mach 7.6 a few minutes after launch.

    --
    2*3*3*3*3*11*251
  32. Lost by Seawolf359 · · Score: 1

    "We received data for the full length of the 10-minute flight. All indications are that supersonic combustion occurred."
    Read: After ten minutes it exploded. :-)
    No seriously this is cool.
    Although it leaves me with one fear of how it will be used.
    http://www.darwinawards.com/darwin/darwin1995-04.h tml

    1. Re:Lost by Anonymous Coward · · Score: 0

      no After 10 minutes it burnt up on re-entry. It doesn't have heat shields to save weight. And while it was already in the atmosphere, it was rapidly accelerating straight down. The friction would have been enormous.

      ie: This is the opposite of a meteour, A meteour enters the atmosphere and slows down via friction, slowly burning up. Imagine strapping an engine on the back of the meteour so that it accelerates. Do you think it will burn up faster or slower?

    2. Re:Lost by Anonymous Coward · · Score: 0

      I believe it slammed vertically into the ground at the end of the experiment (cut to picture of a flatened metal pancake) but they are yet to find the wreckage....

      Presumably they need to find the hole in the south australian desert...

      Q.

    3. Re:Lost by redcliffe · · Score: 2

      Well actually the scramjet was lit on the way down. Straight down. So it would have hit the ground and damn near Mach 7.6. That's got to make a good lawn dart.

  33. popation = population by Alien54 · · Score: 1

    doh

    --
    "It is a greater offense to steal men's labor, than their clothes"
  34. hmmm..nice but not practicle by JoeBlows · · Score: 1

    at least for the near future.

    all this is is a proof of concept. I mean, you are still wasting tons of fuel getting the enguine up to a speed at which the scoop and compression will work.

    --
    True capitalism = lots of similar companies = jobs for everyone who wants one.
    1. Re:hmmm..nice but not practicle by Mt._Honkey · · Score: 2
      all this is is a proof of concept.
      Well, duh. What more do you expect from the very first flight of a completely new technology. As underfunded as these people were, you couldn't dream of anything more. The data gathered from this flight and subsiquent flights (they're hoping for 7 more) will lead to a much more practical model. I assume that that model would be for more research, until we get it safe and predictable. Then I would think that either the military or various satilite-launching organizations would jump on it and start using it.

      This is just the first baby-step.
      --

      Don't Bogart the fish sticks
    2. Re:hmmm..nice but not practicle by Anonymous Coward · · Score: 0

      The test was to get data to correlate test data between flight and their shock tunnel facilities. Since they can determine how it performs in flight and can then put it into the shock tunnel and see how it performs there.

      The best design they have for a scramjet looks nothing like the one that flew. In fact instead of being quasi-2d it's axisymmetric. Pretty cool looking thing too.

    3. Re:hmmm..nice but not practicle by Anonymous Coward · · Score: 0

      > As underfunded as these people were, you couldn't dream of anything more.

      TRY AGAIN. These are the latest in a long line of money-wasting projects. Britain sank big bucks into scramjets. NASA wasted serious dollars on the National Aerospace Plane. And those projects happened decades ago. These researchers didn't invent the idea: they're just trying to breathe life into a corpse. It should stay dead, thanks.

  35. Just one problem... speedbumps by Dark+Nexus · · Score: 3, Interesting

    Ever hit a speedbump at low speeds?

    Not that bad.

    Ever hit one at a higher speed? Say, at least twice it's rating (hitting a 15km/h bump at 30km/h, for example)?

    It's not the most pleasant things.

    Now, you're saying that "Planes don't have to worry about speed bumps!", and you're right.

    But what about turbulence?

    You can hit turbulence at Mach 0.76 that's pretty rough. What would that same turbulence to do a large plane at Mach 7.6?

    --
    Dark Nexus
    "Sanity is calming, but madness is more interesting."
    1. Re:Just one problem... speedbumps by gunnk · · Score: 2, Informative

      One of the interesting footnotes from aviation is the first attempt at breaking the sound barrier. As you approach the speed of sound turbulence increases dramatically. However, when you break it you are in a new aerodynamic regime and suddenly the turbulence plummets. A very pleasant surprise to Chuck Yeager, the first supersonic pilot.

      You can find more information about the "Wall of Air" that was believed to prevent supersonic flight, as well as Yeager's breaking on the barrier here:

      http://www.capstonestudio.com/supersonic/main.ht ml

      --
      Life is short: void the warranty.
    2. Re:Just one problem... speedbumps by Joseph+Vigneau · · Score: 3, Interesting
      You can hit turbulence at Mach 0.76 that's pretty rough. What would that same turbulence to do a large plane at Mach 7.6?

      Planes fly Mach 0.76 at 30000ft. A plane flying Mach 7.6 would be much higher, upwards of 100000ft, where there is very little air to cause turbulence. Friction becomes an issue. When the X-15 flew Mach 6,

      Air friction at speeds much above Mach 6.0 would weaken even the X-15's chrome-nickel Iconel X skin, so a special resin-and-glass-bead ablative coating was developed that would gradually sear away in flight, carrying with it the excess heat.
      Let's hope they get that problem worked out...
    3. Re:Just one problem... speedbumps by blancolioni · · Score: 1

      At the altitudes that the aircraft will be flying at, there is no turbulence. I'm surprised that having taken the time to tell your little story, you didn't bother looking that up.

      Oh, wait, it's Slashdot. Sorry.

    4. Re:Just one problem... speedbumps by Anonymous Coward · · Score: 0

      This was certainly not the first attempt at breaking the sound barrier, not even the first _successful_ attempt, well i guess it depends on what you mean by "successful" :-) The WWII propeller aircraft were capable (just) of reaching the speed of sound in a dive, and sometimes people did. It was always fatal though, as none of the control surfaces would work anymore....

    5. Re:Just one problem... speedbumps by Dark+Nexus · · Score: 1

      No turbulence? Wrong.

      Turbulence can happen anywhere there is atmosphere (generally accepted as being ~50 miles).

      Smaller chance of turbulence? Yes.
      But it still exists.

      --
      Dark Nexus
      "Sanity is calming, but madness is more interesting."
    6. Re:Just one problem... speedbumps by Pingo · · Score: 1

      There are military aircrafts that has experienced such things and got their wings pretty deformed.

      I have heard a true story about such an incident where the pilot woke up after being unconscious and was in fact able to land the aircraft.

      The wing deformations was severe and indicated that the aircraft experienced at least 24 g load.
      Pretty scary isn't it. //Pingo

      --
      --- Linux or FreeBSD, it's like blondes or brunettes. I like both. ---
    7. Re:Just one problem... speedbumps by snatchitup · · Score: 1

      Right at the speed of sound, all the loud sound waves your craft is generating are building up around you. You are chasing your own waves, and have actually caught up to them. Well, so, we go through the speed of sound and suddenly your sound waves can't keep up with you. Yes aerodynamics changes then, but it's still there.

      Right at the speed of sound, you get something like an additive standing wave. You're in your own sonic boom.

    8. Re:Just one problem... speedbumps by Anonymous Coward · · Score: 0

      Well, if you really want to be nitpicky, the first time the sound barrier was broken was the first time someone used a whip.

      The "Crack" of a whip is caused when the tip accelerates beyond the speed of sound.

    9. Re:Just one problem... speedbumps by rschwa · · Score: 1

      Come on, Everyone knows that speed bumps are ineffectual at twice their rated speed. Suspension just soaks them up. That's why they started building those damn big speed mounds.

    10. Re:Just one problem... speedbumps by Anonymous Coward · · Score: 0

      They will probably use ceramics like the shuttle uses. They can handle high amounts of heat.

    11. Re:Just one problem... speedbumps by elliott666 · · Score: 1

      what about contrails and wake turbulence? I know that a 757 will leave a wake trail miles long behind it, now what will happen at 100,000 ft (~30km) where the air is thin and the plane is travelling at mach 7.6. Also, what sort of contrails would be formed, and considering contrails effect the climate, and the fact that the primary ozone depletion is between 15km and 20km up, how would having planes routinely flying through this chunk of the atmosphere effect our planet?

    12. Re:Just one problem... speedbumps by cachorro · · Score: 1

      At Mach 7.6, you are the turbulence!

    13. Re:Just one problem... speedbumps by black_widow · · Score: 1

      once you get above the jetstream and any mountain waves, it's smooth sailing up there.

      Besides, this thing has no wings and a very high mass. But of course, the HALE aircraft don't look like the studiest things

    14. Re:Just one problem... speedbumps by black_widow · · Score: 1

      It's hard to generate such loads when you have no "wings", extrememly high aerodynamic loading (very low surface area, very high mass), and airflow separation due to the shockwaves generated by high speed flight.

      It's just not a big deal.

    15. Re:Just one problem... speedbumps by Anonymous Coward · · Score: 0

      Wel, the first thing you will have to worry about is the fact that hypersonic vehicles create massive shock waves, acress which there is a huge presure and static temperature gradient. I.e. kinetic energy of the vehicle is transformed into vibrational and translational energy of the indivisual atoms of atmospheric air. Under such conditions O2 becomes O3- meaning that if hypersonic transportation becomes commonplace we wil have to discover new and innovative ways of getting rid of all the excess ozone.

      No, I am not kidding.

    16. Re:Just one problem... speedbumps by Nehemiah+S. · · Score: 2

      To continue your airplane/speedbump analogy (actually quite a good one) the way to determine how well an airplane will handle turbulence, simplified grotesquely of course, is to compare the ratio of wing area to the weight of the plane. Think of wings as a sort of inverse shock absorber- the bigger the wings, the more load is transferred from the atmospheric turbulence to the aircraft structure. The weight of the aircraft acts as a damper on this force (higher m means less a for a given f). This is why airplanes like the F-105 make great attack aircraft- they are stable as a rock when flying fast down low. They are quite heavy and have tiny stubs for wings. They also have huge drag coefficients when flying slow because they have to fly at a very high angle of attack.

      Planes like the F-106, on the other hand, are only useful at high altitudes because they will literally shake the pilot to death flying low and fast. However, they have lots of wing area, which makes them more maneuverable and much more efficient.

      Hypersonic aircraft will be huge- on the order of 1.5 to 2 million pounds- and will have wing areas comperable to modern civil transport aircraft. Whereas modern aircraft have wing loadings on the order of 70-160 lb/ft^2, hypersonic vehicles will be on the order of 15-30.

      Al this is moot anyway because, as an earlier poster pointed out, turbulence is primarily a concern at altitudes much different than what a scramjet powered pane will likely cruise at, and also because the dynamic pressure at mach 8 is on the order of 100,000 psi - high enough that tiny differences in thrust caused by impurities in the fuel will have more effect than atmospheric pressure gradients.

      Finally, pressure gradients in the atmosphere follow a normal statistical distribution. the faster you go, i.e. the more linear distance you cover per second, the larger the sample of pressures becomes and therefore the lower the expected standard deviation. All other things considered, you will see less effective turbulence the faster you go.

      --
      ... and there is no doubt, that one day he will be
      where the eye of his telescope has already been
  36. Poor Aussies. They must not even have jets yet. by agilen · · Score: 1

    "We do believe we achieved supersonic flight for the first time," Mr Paull said.

    Hmmmm. Musta never met Chuck.

  37. Re:Mach 7.6- isn't that a little tough for travell by glh · · Score: 1

    Cool, that was my next question too. Thanks for the info. I slept through most of my physics classes in college.. (although I remembered speed vs. acceleration after a few minutes of posting).

  38. Re:Mach 7.6- isn't that a little tough for travell by Joseph+Vigneau · · Score: 3, Informative
    Just wondering, but wouldn't travelling at Mach 7.6 be a little tough on a human? I'm no physisct, but it seems like the G's would be something really painful for a human.

    Mach is a measure of speed relative to the speed of sound at a given elevation, it is not a measure of acceleration. So, at sea level, Mach 7.6 is roughly 5800mph (~2600m/s), but at 25000ft, where the air is thinner, Mach 7.6 is about 5000mph (~2250m/s).

    The gravitation of earth (ie, the amount of force we feel from gravity) is 9.8m/s^2. So, a constant 1G force (which the body won't find too uncomfortable) would accellerate a body to 2250m/s in about four minutes... If a genter push is desired, say .5G, that level of acceleration would need to be maintained for a bit over seven and a half minutes...

    Unless, of course, my physics is rusty.. :^)

  39. Now if we just by littleRedFriend · · Score: 1

    attach this engine to the flying robot three atricles down, he would be able to lift himself. Good stuff for Terminator III though.

    --
    IANAL, but imagine a beowulf cluster of in Soviet Russia all your belong are base to us welcoming the new SCO overlords.
    1. Re:Now if we just by Sloppy · · Score: 1

      Ugh. You're making me think Terminator 3 is going to be as bad as Robocop 3.

      --
      As copyright owner of this comment, I authorize everyone to defeat any technological measure which limits access to it.
  40. Ouch... by littleRedFriend · · Score: 1

    Scientists were hoping the engine would work under its own power on its descent to Earth - reaching a target speed of Mach 7.6 just before hitting the ground.

    Nice landing speed for a passenget jet.

    --
    IANAL, but imagine a beowulf cluster of in Soviet Russia all your belong are base to us welcoming the new SCO overlords.
  41. Re:Mach 7.6- isn't that a little tough for travell by Morphine007 · · Score: 1

    Mach 7.6 would be a bit too much for your average passenger. Fighter jet pilots train for hours on how to keep concious, they are also in excellent physical shape and have a lot of equipment to help them.

    here's a little lesson from Einstein k?

    if I am going nearly the speed of light in one direction and you are going nearly the speed of light in the other direction, who dies because their body can't handle the speed?? NEITHER OF US DIPSHIT!! it's the accel that fscks up the body... and not the velocity... so as long as you aren't pulling more than a G or two in the acceleration process, you're golden...

  42. An interesting route for science by windside · · Score: 2, Interesting

    This is a really cool idea and I'm glad it's beginning to pan out. If the global scientific community wants to continue to move forward during this century as rapidly as it did during the last, it needs to tackle problems with innovations like these instead of simply trying to ameliorate other people's ideas.

    For instance, a friend of mine thinks that the future of the computer industry lies in abandonning the binary basis that has been established and beginning to work with, perhaps, a 4-state diode... Granted, it's not exactly the best idea, but a good example to illustrate my point: it's only a matter of time before old ideas get stale. How many of us have even considered Base n != 2 computing?

    --
    ...Whether my Maker is prepared for the great ordeal of meeting me is another matter.
    Churchill
    1. Re:An interesting route for science by Anonymous Coward · · Score: 0

      This is a troll. Some of the early computers were base 10 for example.

      Base 4 is completely trivial, it just means one 4-digit in the new machine is equivalent to 2 bits of a binary computer.

      A non-integer (or even irrational) base might be a bit more interesting. Even then, there is nothing new here, the Church-Turing thesis still applies.

    2. Re:An interesting route for science by Anonymous Coward · · Score: 1, Interesting

      How many of us have even considered Base n != 2 computing?

      One Mr. Alan Turing. His mathematical model of computing, the Turing machine, can be used with an alphabet of any number of symbols, (2 (binary), 4, 77926, whatever). It can also be proven that any computation done on a machine with 4 symbols or 77926 symbols can be emulated on a machine with just 2 symbols, so there are no fundamentally new problems that can be solved with base 4 that cannot with base 2.

      From an efficiency standpoint, base 3 is far more interesting than base 4. Since any base 4 symbol can be encoded by exactly two bits, there is no gain in efficiency in memory or communications bandwidth. I think it was Shannon who proved that it takes twice as much bandwidth to send a base 4 symbol, or in general, log2(base) times as much for an arbitrary base, so in your case, you would have to send half the symbols, but each one would take either twice the time or twice the frequency bandwidth to transmit, so there is no gain. Undoubtedly this caries over into memory architecture also, you need fewer memory cells, but each cell would probably take up twice as much silicon area, so again, no gain. A base 3 digit (trinary digit, trit) has many useful purposes (yes, no, don't know/care) and has the information content of log2(3)=1.58 bits, so there is a good deal of efficiency to be gained here by transmitting 1 trit instead of the two bits needed to encode it to binary.

    3. Re:An interesting route for science by Anonymous Coward · · Score: 0

      How many of us have even considered Base n != 2 computing? The ENIAC, the first functional fully-electronic computer in the modern sense, used base 10 logic. The designers knew about binary and that it would probably make construction of the system simpler, but chose base 10 to minimize difficulties in converting from the problem space to the program space.

    4. Re:An interesting route for science by Jack+Brennan · · Score: 1

      "How many of us have even considered Base n != 2 computing?"

      Ever heard of an analog computer?

    5. Re:An interesting route for science by Anonymous Coward · · Score: 0

      You might want to look up the definition of "ameliorate". It doesn't mean what you think it does. Dictionary

  43. But what about turbulence? by oliverthered · · Score: 2

    Well that depends on how turbulance works when you that supersonic

    --
    thank God the internet isn't a human right.
  44. The first time? by macdaddy357 · · Score: 1

    Quoting the article... "We do believe we achieved supersonic flight for the first time," Mr Paull said. Chuck Yeager didn't do that in the fifties did he? Naaaaw! That is just an urban legend, like the concorde.

    --
    How ya like dat?
    1. Re:The first time? by MtViewGuy · · Score: 2

      I don't think it's the first time that scientists have tested a functional scramjet.

      Back in the 1990's, Russian scientists put a model of a scramjet engine on top of a former SS-20 missile and I believe they did manage to get some test results from these fights.

    2. Re:The first time? by Anonymous Coward · · Score: 0
    3. Re:The first time? by zoiblot · · Score: 1

      I think they were referring to testing their own technology, not the first time EVER.

  45. Star wars can cope by AlecC · · Score: 1

    I would reckon these things would be easier for a Star Wars system to defend against than true ICBMs. They have to come through the upper atmosphere, which gives you a releatively thin slice of directions it must be coming from (say 50,000 ft vertically) compared to the wide angle (bauically, anywher up) an ICBM is coming from. And an ICBM will come in faster: plummetting from 100 miles up should beat even Mach 7.6, and the heat sahileds have to last for only the last minute or two of the flight rather than the whole flight.

    Actually, defence wise, I seee these as increasing the techno-advantage of the high-tech states. High tech states could build very fast bombers, cabable of responding from (say) the US to (taking a radom example) Iraq in 45 minites or so. Which means that a surprise attack has to be launced in an even narrower window than before if it is to get away before vengeance arrives.

    --
    Consciousness is an illusion caused by an excess of self consciousness.
    1. Re:Star wars can cope by ThereIsNoSporkNeo · · Score: 1

      Dropping a bomb at mach 7 would cause all sorts of problems.

      First of all, aiming it. The computer didn't time it to the nanosecond? You missed the factory and hit the orphanage.

      Secondly, having bombs strapped to the outside would screw up the aerodynamics of the plane horribly. Having a bomb door open while the plane is traveling at mach 7 would probably rip it apart.

      Of course, you could just fly real low over the town and do damage via sonic-boom.

      --
      With my dying breath, I curse Zoidberg!
    2. Re:Star wars can cope by Anonymous Coward · · Score: 0

      It's true some people get Karma by trolling, but usually metamoderation would step in and curb this. Your kind of truly is pretty pathatic, catch-word compliant, war call, etc is just so 00's.

      Go somewhere else to troll btw.

    3. Re:Star wars can cope by AlecC · · Score: 1

      Excuse me - please can you explain why you considered my post a troll? It was purely a technical response to a point made someone else.

      The only thing I can think is that you are taking it as approval of Star Wars, or Star Wars 2. Actually, I do not - I think it a damned bad idea; basically the military-industrical complex is taking the US taxpayer as suckers with a bottomless wallet. Buit that doesn't stop me making reasoned technical comments about the proposed system.

      If we are to discuss such things, we should do so without knee-jerk reactions.

      --
      Consciousness is an illusion caused by an excess of self consciousness.
  46. Not really impressed about this by Anonymous Coward · · Score: 0

    I throught the computer evolved and created the wings itself.
    Only how to control muscle, most of us learn that in a couple months.

  47. Re:Poor Aussies. They must not even have jets yet. by Anonymous Coward · · Score: 0

    they mean 'supersonic combustion' - conventional jet engines have to slow the air down in order to ignite it. A scramjet does not.

  48. Re:Mach 7.6- isn't that a little tough for travell by Anonymous Coward · · Score: 1, Funny
    Nonetheless, I'd rather be in Sydney in 2 hours with a bloody nose and bruised ribs than endure a 20 hour flight with a bunch of Englishmen...

    ... you can tell when a plane full of English people arrives because the the whining continues after the engines stop.

    Old joke. Sorry.

  49. Did They Achieve Acceleration or Even Thrust? by Nit+Picker · · Score: 1

    As I read the article, I see that they ignited the fuel, but I have yet to see anyone claim that the burning fuel produced any thrust. Can someone point to more info?

    1. Re:Did They Achieve Acceleration or Even Thrust? by tony_gardner · · Score: 2

      If the fuel burned, of course thrust was achieved. However, to answer your real question, this engine was not designed to produce net thrust. It was designed to achieve supersonic combustion within the simplest possible configuration

    2. Re:Did They Achieve Acceleration or Even Thrust? by Anonymous Coward · · Score: 0

      > If the fuel burned, of course thrust was achieved.

      TRY AGAIN. Calculate just exactly how long a given molecule of the airstream resides in the engine. At those speeds, we're talking *milliseconds*. The fuel would have to burn amazingly well to generate enough thrust to compensate for the drag caused by the air intake. Net thrust could easily have been *negative*.

    3. Re:Did They Achieve Acceleration or Even Thrust? by Anonymous Coward · · Score: 0

      Yep, but thrust must, by definition have been positive. cf difference between net thrust and thrust. If energy has been added, thrust was produced, as simple as that. At these conditions, the combustion time of H2 and O2 is about 10 microseconds.

  50. I dig the tech by the+bluebrain · · Score: 2

    I dig the tech ... but from preceding comments I believe that a somewhat false impression has been made on a few people: There is indeed this fantastic engine which can reasonably efficiently propel you around the globe at speeds exceeding that of sound by a factor greater than the number of finger most people have on one hand - but: it has to be accelerated to more than twice the speed of the fastest jet aircraft built to date for it even to ignite.

    I once had this motorbike I always had to push start. It was quite annoying.

    --
    yes, we have no bananas
    1. Re:I dig the tech by Anonymous Coward · · Score: 0

      Maybe they will start it like a roller-coaster. You will accend to 75000 feet, fall to 50000, turn on the engine and level it out. I just wonder how many air-sick bags they will need.

  51. Re:Mach 7.6- isn't that a little tough for travell by trixillion · · Score: 1

    While we are on the subject of gravity, the effective gravity you would feel while in flight at mach 7.6 at 250000 ft is about 90% g. This happens because of two effects, the reduced gravity from the height (about 25% of the effect int his case) and the centripital forces due to your rotating reference frame (the other 75%).

  52. good luck by asv108 · · Score: 2
    Realistically, we probably won't hit Mach 7 in commercial flights for some time, and there will probably be "low-speed" versions for shorter distances.

    Considering the Concorde is banned from most airports due to polution and especially noise problems, I doubt you will be seeing this thing on a runway near you, anytime soon.

    1. Re:good luck by operagost · · Score: 1
      The whole point of the scramjet is that it's highly efficient, making it practical for commercial airliners. It follows that a radically efficient engine would produce fewer emissions.

      As for noise, who knows.

      --

      Gamingmuseum.com: Give your 3D accelerator a rest.
    2. Re:good luck by gilroy · · Score: 2
      Blockquoth the poster:

      As for noise, who knows.

      Um, as it travels Mach 7.6 -- 7.6 times the speed of sound -- we do know: BOOM as it goes past.
    3. Re:good luck by Grape+Shasta · · Score: 2
      Um, as it travels Mach 7.6 -- 7.6 times the speed of sound -- we do know: BOOM as it goes past.

      Actually, I thought the sonic boom only happens when you accelerate through Mach 1, because at that point the airplane is travelling at the same speed as the sounds it is making, and therefore the sounds all build up on top of each other. But once you're well past Mach 1, this isn't a problem. Am I right? (So, we still have a sound problem, but it's only at two points during the flight, not over the course of the whole flight.)

      --

      "I am a cipher, a cipher, wrapped in an enigma, smothered in secret sauce" -Jimmy James
    4. Re:good luck by mlh1996 · · Score: 1
      Am I right? No.

      The "sonic boom" is the sound of the supersonic plane's shock wave as it passes along the ground. This shock wave is present throughout the time the plane is supersonic.

      --
      Lack of creativity is no excuse for not having a .sig
    5. Re:good luck by gilroy · · Score: 3, Informative
      Blockquoth the poster:

      Am I right? (So, we still have a sound problem, but it's only at two points during the flight, not over the course of the whole flight.)

      No. Years of Star Trek have mislead people by analogy, but the "sonic boom" is not the sound of you piercing the sound barrier. It's the result of a massive spike-and-fall of pressure across your ears. You are right that it comes from a superposition of pressure maxima (a "piling up") but that happens along a cone of air.


      Without touting my own horn too much -- and believe me, there are equally good or better animations -- but I have a set of animated GIFs that show this.

  53. G-suits by Scratch-O-Matic · · Score: 2

    I'm not even sure if a G-suit would keep you from blacking out.

    Generally speaking, g-suits are designed to protect you from g's that press you down into your seat, in a turn for instance, not g's that press you into the back of your seat. G's from lateral acceleration, as would be experienced on this scramjet, would be unlikely to cause unconsciousness because blood is not being drained from the heads of the passengers. It would still be mighty uncomfortable, though.

    --


    Evil is the money of root.
  54. Re:Mach 7.6- isn't that a little tough for travell by damien_kane · · Score: 1

    if I am going nearly the speed of light in one direction and you are going nearly the speed of light in the other direction, who dies because their body can't handle the speed?? NEITHER OF US DIPSHIT!!

    EEENH!!! Wrong Answer, thanks for trying. If you're going nearly the speed of light, and you're friend is going nearly the speend of light, you both die.
    As you approach the speed of light, a finite mass will actually weigh more, by many, mnay orders of magnitude. The forces your own molecules would be exerting on themselves would cause your body to implode itself.
    If your body no longer exists in the form it currently is, instead being either a) a group of atoms violently moving apart or b) a superdense chunk of matter, I don't think you'll be alive...

  55. HyShot Scramjet Test by sagavia · · Score: 4, Informative

    As I read the comments, it seems that some people don't get the implications. In a normal jet engine the flow has to be slowed to less than Mach 1 for compustion to occur. Faster, and it goes out. This limits the range of velocity that can be attained. So, there is a range of velocity that can only be attained with rockets. With a working Scramjet it becomes possible to fly most of the way to orbit. From an energy consideration, once you are in low earth orbit you are half way to anywhere in the solar system and can use low acceleration, high efficency engines to get anywhere.

    Scramjets are the realistic key to space exploration.

    --
    Eschew Obfuscation
    1. Re:HyShot Scramjet Test by WolfWithoutAClause · · Score: 2
      Ok, Einstein, you've got the basic theory. Now explain:

      a) the difference between mach 7.6 and mach 25

      b) how you stop the thing melting at mach 10-20

      c) why the term 'dry mass' is rather important to something that wants to achieve orbit and compare and contrast the thrust/mass ratio of a scramjet with a rocket engine

      d) how you accelerate up to the minimum speed this engine needs to begin to work (hint: it's called a "rocket", or a jet engine (see point c))

      e) how drag ultimately limits how long you can spend in the atmosphere (hint: drag goes as a square law with velocity, but oxidiser input from the air only goes linearly).

      In a normal jet engine the flow has to be slowed to less than Mach 1 for compustion to occur. Faster, and it goes out.

      Actually I thought the main problem was that the compressor blades tend to melt...

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    2. Re:HyShot Scramjet Test by toby360 · · Score: 1

      Also, theoretically if they were to modify the shape and length of the combustion area as its in action, you could fly far past mach 7. By using the air coming in at faster and faster and faster speeds, the system could adjust the point of combustion, and amount of fuel to futher increase thrust. I wouldn't be surprised if we were flying at mach 20 in test flights a few years from now... and throwing payloads into space with ease..

    3. Re:HyShot Scramjet Test by WolfWithoutAClause · · Score: 3, Informative
      The big problem is that the whole aircraft tends to melt. At anything above about Mach 6 cooling becomes really, really tricky. Above about Mach 10 cooling is getting to be nearly impossible. Orbit is mach 25.

      Rockets work around this, by avoiding staying in the atmosphere at high speeds for long.

      Scramjets can't- because they need the air to breath.

      There are techniques that may help- 'skip trajectories', using the fuel to cool the skin of the aircraft, and burning off the skin of the aircraft (ablative). But ultimately they're all a bit awkward.

      All the time you are in the atmosphere you are fighting drag- and that costs fuel. Beyond a certain point, you are probably better off using a rocket. And they atleast work at Mach 0-3 and up, which scramjets don't.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    4. Re:HyShot Scramjet Test by Sloppy · · Score: 1
      At anything above about Mach 6 cooling becomes really, really tricky. Above about Mach 10 cooling is getting to be nearly impossible.
      No problem, just put a heatsink and fan on it.
      --
      As copyright owner of this comment, I authorize everyone to defeat any technological measure which limits access to it.
    5. Re:HyShot Scramjet Test by WolfWithoutAClause · · Score: 2
      No problem, just put a heatsink and fan on it.

      You don't understand. This is really hot. Hotter than a Beowolf cluster of 2.2 Ghz Athlons overclocked to 4.4 Ghz running Apache with the latest Red Hat distro on it, when it's being Slashdotted.

      It needs water cooling anyway.

      --

      -WolfWithoutAClause

      "Gravity is only a theory, not a fact!"
    6. Re:HyShot Scramjet Test by Skuggan · · Score: 1
      You don't understand. This is really hot. Hotter than a Beowolf cluster of 2.2 Ghz Athlons overclocked to 4.4 Ghz running Apache with the latest Red Hat distro on it, when it's being Slashdotted.

      It needs water cooling anyway.


      Wait until it rains, then you get free water cooling...
      --
      http://www.millnet.se/ GO/U d- s+:+ a C++ UL++++ P- L+++ E W+++ N+ w++ M-- PE+ t+ X++
    7. Re:HyShot Scramjet Test by Anonymous Coward · · Score: 0

      I believe the proper sarcastic idiom would be to call him an "Oppenheimer" rather than an "Einstein", since Einstein came up with the theories, and Oppenheimer made them practical. =)

  56. Ummm, no by andyring · · Score: 1
    Keep in mind that this thing burned up near the end of it's journey. About the shuttle landing, your reply makes no sense. A slope of 15 km? All the shuttle needs to land is a long enough runway. Heck, where I live, Lincoln, Neb., one of three runways at our airport (also used by the Air Guard base here) is 2 1/2 miles long, and it's actually one of the alternate shuttle landing sites (something like 10th on the list). Sure, it's coming in faster than Mach 1, but not anywhere near Mach 7.

    Also, for the trivia-minded, Lincoln was also near the top of the list to be nuked by the Commies during the cold war, as that particular runway could serve as a base for B-52s, etc.

    1. Re:Ummm, no by filtrs · · Score: 1

      Actually, I've seen many shuttle landings, and it doesn't come in anywhere near Mach 1.

      From
      NASA

      "The orbiter differs in at least one major aspect from conventional aircraft; it is unpowered during re-entry and landing so its high-speed glide must be perfectly executed the first time -- there is no go-around capability. The orbiter touchdown speed is 213 to 226 miles (343 to 364 kilometers) per hour."

      --
      My mother always used to tell me: If you can't find anything nice to say, say something bad about Windows.
  57. Re:Mach 7.6- isn't that a little tough for travell by timeOday · · Score: 1

    So what would it be like to hit turbulence at Mach 7.6? Or for that matter if a rivet was not quite flush? I'll bet you'd get a lot of Gs then, maybe too many to notice.

  58. Funding? by timeOday · · Score: 2, Interesting

    I'm very impressed that this was headed by a University (versus, say, Lockheed-Martin or Nasa). The article says there were collaborators from around the globe, but who picked up the tab?

  59. Ah, but... by gilroy · · Score: 2
    Blockquoth the poster:

    The speed with which these waves move is controlled by how quickly molecules can move their energy out from the sound source, to pass to molecules further out. Since this energy is transferred through collisions, each molecule must physically traverse the distance between interactions. The speed with which each molecule moves is directly related to its kinetic energy--in other words, its temperature. And only its temperature.

    Yet... the average distance the molecules must mobe -- their mean free path -- moves inversely with the density: the lower the density, the greater the separation of molecules. At larger distances with a given speed, the rate of energy transfer would of course be lower. So shouldn't density matter?


    Well, as I pointed out elsewhere, the crux of the matter is that pressure and density do matter. But for an ideal gas, their effect cancels out, and indeed, yields the temperature dependance everyone is so worked up over.

    1. Re:Ah, but... by Idarubicin · · Score: 1
      At larger distances with a given speed, the rate of energy transfer would of course be lower. So shouldn't density matter?

      Sure, the rate of energy transfer would be lower. But we're not interested in how much energy moves, just how fast the wavefront (region of higher pressure) moves out from the sound source.

      Whether the molecules travel large distances between collisions or short distances has a nearly negligible effect. Many short steps or a few long ones take essentially the same amount of time, since under normal conditions, collisional transfer of energy is an extremely fast process. The molecules themselves are still travelling at the same speed, because for a given gas that's a function of temperature alone. (Temperature is tied directly to the average kinetic energy per molecule.)

      This interpretation gets us away from questions about non-ideal gases and on to the firm (*wink*) footing of statistical mechanics. We only get into trouble at extremely high densities--not really a problem at an atmosphere or pressure or less.

      --
      ~Idarubicin
    2. Re:Ah, but... by Anonymous Coward · · Score: 0

      And I'm going to tell you that from the perspective of an aerospace engineer for a given gas, we deal with the gas constant (R), the ratio of specific heats (Gamma) and the temperature (T) and the equation works as speed of sound = sqrt(Gamma x R x T). From four years of expensive aerospace engineering education that's as complicated as it got, and I still haven't seen anything more complicated.

    3. Re:Ah, but... by gilroy · · Score: 2
      Blockquoth the poster:

      Whether the molecules travel large distances between collisions or short distances has a nearly negligible effect.

      I disbelieve this. Shorter hops = more collisions = more opportunities for reversal/deflection. Remember that this is essentially a random-walk process. Imagining a one-dimensional gas :), the total expected distance is something like L sqrt N, L being the mean free path and N the number of steps. Let's say we halve the mfp but this doubles the steps. Then the expected distance becomes sqrt(2)/2 times what it was.


      Blockquoth the poster:


      (Temperature is tied directly to the average kinetic energy per molecule.)

      Sorry, pet peeve of a physics teacher: Temperature is not tied to the kinetic energy. It's tied to the dispersion in the kinetic energy. Throwing a snowball doesn't heat it (neglecting air friction), because you add the same KE to every atom and hence the dispersion is the same.


      The whole "T proportional to average KE" thing comes from a century of chemists, whose samples had a center-of-mass velocity of zero and hence a dispersion of KE equal to the average KE.


      As an analogy, take a group of 1st graders walking down the street. If they're all tired, they stay clumped. If they're full of sugar, they bounce around a lot. In either case, they might maintain the same average forward velocity (KE) but in the latter, there's more dispersion.

  60. marketdriods by nege · · Score: 1

    Now is the proper time for me to reveal my patented SPAM-JET - delivering accrate and timely spam to email users at the speed junk!

  61. Re:Mach 7.6- isn't that a little tough for travell by gilroy · · Score: 3, Informative
    Blockquoth the poster:

    if I am going nearly the speed of light in one direction and you are going nearly the speed of light in the other direction, who dies because their body can't handle the speed?? NEITHER OF US DIPSHIT!!


    EEENH!!! Wrong Answer, thanks for trying.

    Bzzzt. But thank you for playing. Since forces are dependent on acceleration, moving at constant speed is indistinguishable from being at rest. That's not even Einstein -- that's Galileo.

    As you approach the speed of light, a finite mass will actually weigh more, by many, mnay orders of magnitude. The forces your own molecules would be exerting on themselves would cause your body to implode itself.

    Bzzzt again. This just isn't your day. First, modern physicists don't even talk about mass increasing as velocity increases. Mass is mass is mass; ie., what used to be called "rest mass". The observed kinetic energy increased with velocity, of course. But we don't use relativist mass because it implies things like, "Oh, Newton's laws are OK if you just put a factor of gamma in", which is not true. It can be shown that in fact, there would be two relativistic masses, a "parallel component" one and a "transverse component" one. This complicates the idea of mass and force so much it's of no use whatsoever.


    Second, even if your mass seems to increase as measured by an observer, it wouldn't for you... All of your molecules will be traveling at the same speed, so each sees the others at rest and therefore, by the first principle of relativity, can see no mass effect.


    Third -- and now I'm just being obnoxious -- you seem to confuse "mass" and "weight".

  62. ?Que Pasa? by pmancini · · Score: 2

    "After everyone had gone home, the researchers faced a nail-biting wait for the telemetry officers to come in from the dust with their precious data, before analysis could occur."

    Don't they have some form of high speed network they can just FTP the data over? Why did they have to wait for these guys to come back from remote tracking stations? Anyone know?

    --P

    1. Re:?Que Pasa? by p3d0 · · Score: 2

      The data was recorded in a little black box that parachuted back to earth, somewhere within an n-kilometer radius for some moderately large value of n, and so it took some time to find it.

      --
      Patrick Doyle
      I mod down every jackass who puts his moderation policy in his sig. Oh, wait a sec....
  63. Success? by FJ · · Score: 3, Funny

    It isn't too often you hear the word "success" in the same article as until it began to burn up

    1. Re:Success? by Craigj0 · · Score: 1

      How about: It was a great sucess until it began to burn up.

  64. Great... by utexaspunk · · Score: 1

    So when the terrorists hijack one of these after the 10 years of flight school or whatever they would have to take to be able to handle one...

  65. The new Wright Brothers by blair1q · · Score: 2


    This will revolutionize worldwide air transport.

    --Blair

  66. Re:Mach 7.6- isn't that a little tough for travell by damien_kane · · Score: 1

    Bzzzt again. This just isn't your day. First, modern physicists don't even talk about mass increasing as velocity increases. Mass is mass is mass;
    No shit, which is why I said a finite mass weighs more, that that the finite mass gains more mass.
    IIRC a person weighs less on the moon, with respect to the moon, because the gravitational forces (cause by the mass of the moon) are smaller.
    As you approach the speed of light, you weigh more, not in respect to eh earth, but in resepct to yourself.
    Your molecules, having the same mass as they did at rest, have a much stronger force of attraction between them.
    I said nothing about mass increasing, that is both physically and theoretically impossible, without actually adding mass of course.

    Third -- and now I'm just being obnoxious -- you seem to confuse "mass" and "weight". Now I can be obnoxious... Everyone always complains about people not reading the articles and posting a reply to a front-page story, but it seems you have not even read the comment you are replying to... or your 5th grade english skills make it impossible for you to comprehend.
    Either way, I'm not the one at fault.

  67. Fascinating, but who does it really benefit by Wierd+Willy · · Score: 1
    While scramjets raise the possibility of Sydney to London flights in two hours, they are set to revolutionise the launch of small space payloads, such as communications satellites, by substantially lowering costs. They have the added benefit that they do not even have to carry most of their propellant as they use oxygen from the atmosphere.
    This is a nice fairy tale but when the military decides to use this technology it will become unavailable for use by the general public. The most obvious use would be lightening fast attack jets that could hit a target from a base 15,000 miles away and 30 or 40 miles altitude and be back to base before the news hits the media. Then the attacker could say something like "it wasn't us man, all our planes are here at home." Never underestimate the evil of the military-industrial complex or the politicians that profit from it.
    --
    Stupid Humans.....
    1. Re:Fascinating, but who does it really benefit by Anonymous Coward · · Score: 0

      1. We can ALREADY hit stuff from bases 15,000 miles away from the targets(not at 30 miles up, but who cares).

      2. I doubt you'd be able to make a military aircraft that could use this effectively. At Mach 7.6, you wouldn't be able to TURN the machine without busting it into a million pieces, which makes it kind of hard to get over the target, to say nothing of getting home again.

      I'm not saying it will never be possible to build a military scramjet, but I doubt it will be cost effective in my lifetime.

      Sean

    2. Re:Fascinating, but who does it really benefit by Anonymous Coward · · Score: 0

      The most obvious use would be lightening fast attack jets that could hit a target from a base 15,000 miles away and 30 or 40 miles altitude and be back to base before the news hits the media.

      Umm... no place on Earth is 15,000 miles away from any other place on earth. The farthest any point on Earth's surface is from any other point is a little less than 12,600 miles.

  68. Re:Mach 7.6- isn't that a little tough for travell by surfcow · · Score: 1

    ... Nonetheless, I'd rather be in Sydney in 2 hours with a bloody nose and bruised ribs than endure a 20 hour flight with a bunch of Englishmen...

    Part of that can be easily arranged.

    =brian

  69. Allan Paull... by Frank+of+Earth · · Score: 2

    ... is mysteriously close to Paul Allen! Come on, who spells there name with all those extra L's

  70. Your post is the first good news I have heard.. by Weezul · · Score: 2

    ..about low speed scram jets. I had always been told that the shock was totally impossible bellow Mach 4. They should eventually get the speed down if its only a stability issue. AEs seem to be good at designing arround stability problems. Perhaps they could even lower it further by including compressed oxygen on the plane? The oxygen could be used to help with the standing shock.

    Perhaps something like this: Normal jet engines from take off to mach n (n 4), compressed oxygen "rocket mode" version of the scram jet enginee up to mach m, real scram jet mode on up. You would get three diffrent types of engine for the cost of two.

    --
    The Christian religion has been and still is the principal enemy of moral progress in the world. -- Bertrand Russell
    1. Re:Your post is the first good news I have heard.. by mprinkey · · Score: 1

      No, it is not only a stability issue. The strength of the shock determines the pressure jump. The point is to use the shock as a pressurization mechanism, rather than a spinning compressor section as in a normal turbofan engine. There is certain level of pressurization that needs to occur before this is effective. Just like an IC engine, if you cannot get a high enough compression ratio, you cannot have an efficient engine. In this case, lack of sufficient pressurization can cause reversal of the combusted material back through the intake rather than expanding and accelerating out the nozzle to the rear. This is a problem for both ramjet and scramjet engines

      AFAIK, stability is the primary issue in moving from ramjet to scramjet. Supersonic combustion, acoustic coupling, etc. can make for lots of stability problems. Getting good mixing of air and fuel prior to the combustion/shock surface is critical and not all that easy, considering the high inlet velocities.

      Also, the presence of a compressor section tends to lead to predictable inlet conditions for the combustor section because effects of turbulence at the intake are muted. For a scramjet, there is no similar buffer, so inlet turbulence adds even more perturbations to the shock/combustion surface. Right now, we have no control systems that can actively control turbulence. This is just a very hard engineering problem...deceptively so even. At least on paper, scramjets are nothing more than a carefully shaped duct and some fuel jets.

      IAAMechanicalEngineer.

  71. first? by qoncept · · Score: 1

    What? Why is that article saying this is the first supersonic flight? Didnt that happen in like 1960 (roughly??)?

    --
    Whale
    1. Re:first? by reallocate · · Score: 1
      The first manned supersonic flight was Chuck Yeager's in 1947. In World War II, the Nazi's V-2 had a top speed of about 3,600 mph, several times the speed of sound.

      In light of the, uh, apparent lack of historical perspective illustrated by many of these posts, here's a rough timeline:

      Orville and Wilbur fly -- 1903
      World War II -- 1939-1945
      Chuck Yeager flies the X-1 beyond Mach 1 -- 1947
      First Artificial Satellite Launched -- 1957
      First manned satellite launched -- 1961
      First manned lunar landing -- 1969

      --
      -- Slashdot: When Public Access TV Says "No"
    2. Re:first? by Anonymous Coward · · Score: 0

      Umm...no, I think the first poster was right. Supersonic, meaning faster than the speed of sound (aka Mach 1+). Now...I know that Yeager flew the first jet engine plane...It could also be the first supersonic...and the timeframe of the late 40s is about right.

  72. Mach 7.6 and three headed fish by Anonymous Coward · · Score: 0

    One quick thought - isn't 100,000ft high enough where radiation becomes a problem?

  73. Why does this matter? by Anonymous Coward · · Score: 0

    I read the whole article.. but it doesn't seem very interesting. Hooray for engines that need rockets to take off, go faster than is even useful, and destroy themselves after flight.

    I can't wait 'til these hit the market, boy oh boy. How long has the Concorde been around? When was the last time you flew on it? That's what I thought.

    1. Re:Why does this matter? by reallocate · · Score: 2, Insightful

      Too bad you were bored. Going faster for less money is usually considered a good thing. This is a proof of concept of a technology that promises to dramatically lower the cost of getting payloads to orbit. The fact that it plowed into the ground is irrelevant: the point was to get the scramjet to ignite. We know how to land aircraft. (BTW, the Concorde is expensive because it uses 40-year old technology. France and the UK subsidized development for reasons other than creating cost-effective travel. If someone would market a commercial aircraft that could do New York-London at 1,500 mph and cost no more to operate per passenger than a 747, that would be interesting, too.

      --
      -- Slashdot: When Public Access TV Says "No"
  74. ...and when you don't have any wings! by black_widow · · Score: 1

    I won't comment about hypersonic dynamics because I have no experience in the field, but lifting bodies have such high aerodynamic loading anyway, turbulence has little relative effect.

  75. Re:A matter of practicality--Not 5 Minutes by reallocate · · Score: 2, Informative
    >> 1. You can get from England to Australia in two hours, but what about going to America. You'd be up there for all of like 5 minutes and pay millions of dollars to do it.>

    If you're flying at about 5,000 mph, you could cover the London-New York distance in about 40 minutes. Add a bit more time for acceleration and decceleration.

    --
    -- Slashdot: When Public Access TV Says "No"
  76. Re:Mach 7.6- isn't that a little tough for travell by reallocate · · Score: 1
    Traveling at mach 7.6., or higher, poses no risk by itself. Getting to that speed is a different matter. Extra g's come from rapid acceleration or deceleration, not constant speed. E.g., run your car into a brick wall at 40 mph and you will feel some serious g-forces.

    Keep the acceleration at the one-gee level and everyone would be as comfortable as they are in their living room. (Believe me, a space propulsion system that could maintain a constant one-gee acceleration level would revolutionize space travel.

    --
    -- Slashdot: When Public Access TV Says "No"
  77. I'm with you so far... by nyet · · Score: 2

    .. but why do they always say "at sea level" when qualifying the speed of sound?

    1. Re:I'm with you so far... by gilroy · · Score: 2
      Blockquoth the poster:
      .. but why do they always say "at sea level" when qualifying the speed of sound?

      Because properties of the atmosphere vary remarkably with height. You need a reference point, and by amazing coincidence :) "sea level" is where the majority of experiments are done (more or less -- we're talking about variations in height for the airplane that are much greater than the variation in altitude of fixed installations).
    2. Re: I'm with you so far... by nyet · · Score: 2

      ... so being that those properties are a secondary effect compared to temperature, why is "at sea level" stressed more than "at X degrees C", or is that just my perception?

    3. Re: I'm with you so far... by gilroy · · Score: 2
      Blockquoth the poster:
      ... so being that those properties are a secondary effect compared to temperature, why is "at sea level" stressed more than "at X degrees C", or is that just my perception?

      IANAAE, but my assumption is this: Above the troposphere, the temperature is actually pretty close to a function of height. On the other hand, a lot of this data was probably amassed by weather balloon, and there's a good reason -- which I misremember -- as to why the pressure data is used as the yardstick. I think the boundaries between layers varies somewhat with time, but I'm not sure.


      Actual answer: It's probably just habit and social inertia.

  78. Why do we need air? by Guru1 · · Score: 1

    The main reason the scramjets are melting is the friction with the air correct? Why not use them in a vacuum?

    Build large systems of vacuum tunnels (overseas would be difficult) for continent travel. Inside the vacuum you wouldn't have friction, so you could get to these higher speeds easily yes? Magnet levitation and all that should make them fairly efficient. Imagine having an hour trip from New York to California.. I gotta imagine that would bring in some extra business. I'd sure as hell go on vacations every weekend if I could be back in time for supper.

    1. Re:Why do we need air? by pigeon768 · · Score: 1

      It needs air containing oxygen coming in at mach 6-7 or whatever in order for the engine to ignite. It's a jet, not a rocket- it can't operate in a vacuum.

      And magnet levitation wouldn't work because you'd need a "railway" suspended at whatever altitude the thing operates at.

    2. Re:Why do we need air? by Dyolf+Knip · · Score: 2

      We don't have trans-continental tunnels because continental drift is a bitch. Sure, it's only a few centimeters a year, but a high-speed vacuum tunnel has to be made to rather close tolerances. Those few centimeters per yr would add up rather quickly.

      The moon and other tectonically (sp?) dead bodies are where you could get away with something like that.

      And as was pointed out, a scramjet is not a rocket. Needs oxygen. In fact, that's one of the big advantages it has over rockets. It can breathe the surrounding atmosphere without having to carry it's own oxidizer.

      --
      Dyolf Knip
  79. Re:Mach 7.6- isn't that a little tough for travell by gilroy · · Score: 2
    Blockquoth the poster:

    No shit, which is why I said a finite mass weighs more,

    With respect to whom? If you don't answer that question, then you're justing spouting gas... once speeds around that of light are involved, relativity is king and you must always keep your reference frame clear. Do you? No, because very soon after, you say,

    As you approach the speed of light, you weigh more, not in respect to eh earth, but in resepct to yourself.

    which is not even bullshit -- it's just wrong. With respect to yourself, by definition you are rest (that's what "with respect to" means). And relativity says that things can't look odd for anything at rest. There is no mass increase because with respect to yourself, you're not moving near lightspeed. With respect to yourself, you're not moving.

    No shit, which is why I said a finite mass weighs more, that that the finite mass gains more mass.

    I don't know if you're sloppy or silly. First you say "I was talking about weight, not mass". Then you immediatel say, "The finite mass gains more mass." Which is it?

    Either way, I'm not the one at fault.

    Bzzzt. But thank you for playing again.
  80. I wish you'd stop hyping technology with NO HOPE by Anonymous Coward · · Score: 0

    Admittedly, this isn't a perpetual motion machine, or that antigravity scam.

    But a scramjet is simply a stupid idea. A vehicle using them would be *less* practical than a rocket, because it would weigh more, and it would be more complicated. And its shape would be heavily contrained, since the vehicle's shape contols the airflow to the scramjet intake. A rocket's shape is much less constrained, which is important because the designer also has to cope with heat shielding, and multiple constraints often mean a bad design.

  81. Re:Mach 7.6- isn't that a little tough for travell by spike+hay · · Score: 2

    So what would it be like to hit turbulence at Mach 7.6? Or for that matter if a rivet was not quite flush? I'll bet you'd get a lot of Gs then, maybe too many to notice.

    The higher the altitude, the less turbulence. The Concorde travels at 50,000 feet. It has almost no turbulence. This scramjet would travel more in the neighborhood of 80,000 feet. The turbulence would basically be zilch.

    In response to an earlier poster: Humans can withstand Mach 7.6. The withstand Mach 25 in rockets. What matters is the acceleration. This scramjet would likely accelerate no faster than a regular jet liner. Fighter pilots only need pressure suits when they do high-g turns. No jet engine has enough thrust to cause blackouts during acceleration.

    --
    If you don't understand any of my sayings, come to me in private and I shall take you in my German mouth.
  82. Cruise: a nitpick by fm6 · · Score: 2

    Is "cruise" a synonym for "nonballistic"? To me the word implies that speed is not an issue -- and ramjets, though slower than ballistic missles, are certainly faster than the fanjets used on cruise missles.