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USAF Scramjet Hits Mach 6, Sets Record

s122604 writes "The [X-51A Waverider]'s scramjet engine accelerated the vehicle to Mach 6, and it flew autonomously for 200 seconds before losing acceleration. At that point the test was terminated. The Air Force said the previous record for a hypersonic scramjet burn was 12 seconds. Joe Vogel, Boeing's director of hypersonics, said, 'This is a new world record and sets the foundation for several hypersonic applications, including access to space, reconnaissance, strike, global reach and commercial transportation.'"

75 of 326 comments (clear)

  1. Why so short bursts? by Henriok · · Score: 3, Interesting

    Why are these engines burning for such short times? Are these engines so early in development that they really can't get them to be stable and safe for more than 12 seconds? Sounds a lot like fusion: it works but it's not yet useful.

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    1. Re:Why so short bursts? by grasshoppa · · Score: 5, Insightful

      Proof of concept. Scientists can only go so far on theory ( and it's impressive how far they do go ). At some point their research hits a point where they need to perform experiments.

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    2. Re:Why so short bursts? by MozeeToby · · Score: 5, Insightful

      Keep in mind that at mach six 200 seconds is 400 kilometers. That's already enough range to make a useful weapon (and yes I realize there was some acceleration time in there). Heck, that's already longer range than the most advanced missiles that many countries have. Increase the stability to just 10 minutes of burn time and you've got a missile that can go 5% of the way around the world.

    3. Re:Why so short bursts? by shadow349 · · Score: 4, Interesting

      Are these engines so early in development that they really can't get them to be stable and safe for more than 12 seconds?

      Are you talking about the scramjet or the events at Kitty Hawk in 1903?

      Because Wilbur already had the first chance, Orville took his turn at the controls. His first flight lasted 12 seconds for a total distance of 120 feet (36.5 m) - shorter than the wingspan of a Boeing 707.

    4. Re:Why so short bursts? by rufty_tufty · · Score: 3, Insightful

      Likewise you want to stop the test before failure so you can look for signs of component wear and material stress so that you know what to improve for next time. Stopping at 200 seconds and finding this out is very useful. Stopping at 201 seconds after it has exploded and you have to work out from the pieces what went wrong is not as informative.

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    5. Re:Why so short bursts? by ckaminski · · Score: 5, Insightful

      Except they're not recovering these vehicles for analysis.

    6. Re:Why so short bursts? by Pharmboy · · Score: 4, Informative

      Not only that, but you can't always be sure which part is the weak link, what will break. A few tests at hypersonic is guaranteed to make an engineer say "ok, that's an issue we weren't aware of", and confirm much of what they already knew. They may have to make some part that they *thought* would be ok out of a different, stronger alloy, etc. Of course, at this speed, every tiny error in engineering is amplified, as at Mach 6, you cross a lot of real estate in just a few seconds, so the word "precision" doesn't adequately describe the level of perfection required in the test system build.

      Being a pioneer at anything guarantees surprises, and best of all, learning new things.

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    7. Re:Why so short bursts? by icebrain · · Score: 2, Interesting

      A couple reasons:

      Testing scramjets on the ground is really, really hard, and you can only do it for a very short time (much less than a second).

      Testing scramjets in flight is really, really expensive. And when your funds are limited, you can only build subscale air-dropped missile-sized vehicles instead of full-sized, self-launching, reusable ones (in part because of the "cheaper now and more expensive long-term" being prefereable to "more expensive now and cheaper in the long run" thinking that brought us the Space Shuttle).

      Making things even more difficult is that we pissed away a huge amount of research (from both the US and UK) on scramjets and high-speed flight a couple decades ago. Companies like Marquardt basically specialized in ramjet-style engines, and were hard at work developing scramjets and other neat high-speed propulsion 40+ years ago. They were very close to having flying hardware. But now, all of the hardware, most of the documentation, pretty much all of the institutional/unwritten knowledge, and most of the personnel are gone. We're having to reinvent the high-speed flight wheel almost from scratch, just like we're doing with heavy-lift launch vehicles, manned lunar flight, and ballistic missile defense, all of which we had operational in the 70s.

      It's disgraceful, really, how we piss away useful technology and other exceptional things. There must be some kind of relationship to crabs in the human psyche that's responsible for this self-loathing anti-achievement personality trait.

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    8. Re:Why so short bursts? by DerekLyons · · Score: 3, Informative

      Likewise you want to stop the test before failure so you can look for signs of component wear and material stress so that you know what to improve for next time. Stopping at 200 seconds and finding this out is very useful. Stopping at 201 seconds after it has exploded and you have to work out from the pieces what went wrong is not as informative.

      Since the vehicle was deliberately crashed into the ocean and not recovered - there's nothing to examine for wear and stress, whole or in pieces.

    9. Re:Why so short bursts? by hargrand · · Score: 2, Insightful

      Except they're not recovering these vehicles for analysis.

      That's what datalinks are for.

    10. Re:Why so short bursts? by CyprusBlue113 · · Score: 2, Insightful

      ICBMs do not do any jetting at all, its not a comparison, as they are ballistic rockets. You can think of them as flying mortars more than missiles. The closest applicable missile would be a cruise missile, but honestly, they are designed more for distance than speed. You don't need your cruise missile to get there ridiculously fast, but you do want a ridiculous range for them, at a sufficient speed to not be destroyed or give advanced warning, while still making it to the target in time for intercept.

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    11. Re:Why so short bursts? by MozeeToby · · Score: 5, Insightful

      It's all part of the Prompt Global Strike program. Eventually the goal is to have scramjet powered missiles with a range of 12000+ miles. Allowing you to fire an obviously non-nuclear missile from Kansas to North Korea and have it hit the target in less than 3 hours. Basically, even launching a B2 for a direct strike takes days or weeks. Refueling planes need to be put into the air, mission plans drawn up, clearance over foreign airspace cleared, pilots briefed, etc. They want to be able to say "Fire" and have the missile in the air within minutes and at target within hours; with the added benefit of not putting any American lives in harms way.

    12. Re:Why so short bursts? by bkaul01 · · Score: 3, Interesting

      Scramjets have no moving parts; it's a duct and a fuel injector. That's it. Wear is a non-issue here.

      Figuring out what shape that duct needs to be in order to get stable combustion, however, is far from a trivial problem; it's not just the fluid dynamics of the supersonic flow that must be considered ... thermodynamic losses can be large enough to quench the flame, and where in the duct those losses occur is as important as their magnitude. With most sorts of engines, second-law analysis is only something you look at to refine the efficiency of the technology once it's mature and functional. With scramjets, it's critical to making them work at all. Building one of these, with all our modern computer modeling technology, is kind of akin to building the first rockets with no computers at all.

    13. Re:Why so short bursts? by Ragnarr · · Score: 2, Interesting

      If you think we can't launch aircraft within 24 hours and strike targets around the world, you're gravely mistaken. We have people whose jobs are to plan for missions such as this so that we can go out and do exactly that just by putting bombs on the planes and taking off. Not to mention that now days, with our capacities for SATCOM and other techniques, we're able to pass target information on the fly and build them in the air. As for the child thread below who wonders why we need air refueling; it's critical to all military operations. It's what sets us apart from all other air forces. Most aircraft are designed to take off with a certain weight, and getting that amount of stuff in the air usually is at the extreme end of an aircraft's capabilities. So, by fueling the aircraft just enough to take off and then refueling on the way you're able to take more hate to the bad guys. And, it extends the range of our aircraft. It's usually not comfortable, but most of our aircraft are capable of flying indefinitely if you can get them the gas to keep them there. Refueling is instrumental to our operations around the globe. Cheers!

  2. Re:Interesting... by AdmiralXyz · · Score: 2, Interesting

    How useful is this in the long run? What was the burn ratio compared to other scramjet vehicles of recent design?

    Are there even any other scramjet vehicles in the operational testing phase? I was under the impression that the X-51, and the other vehicles in the Hyper-X program, are the only ones that've actually flown. Scramjets aren't exactly easy to test in the lab.

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  3. For those of you who don't know how fast Mach 6 is by viking099 · · Score: 3, Informative

    From Wiki Answers:

    Mach is a relative measurment of speed and fluid temperature.
    example;
    Mach 1 at Sealevel (0 feet) is 761.2 MPH (Calibrated Airspeed) and 761.2 MPH(True Airspeed)
    Mach 1 at FL50 (Flight Level 50,000) is 285.8 MPH(CAS) and 660.05 MPH(TAS)
    Mach 6 at Sealevel (0 feet) is 4567.3 MPH(CAS and 4567.3 MPH(TAS)
    Mach 6 at FL50 (Flight Level 50,000) is 3147.97 MPH(CAS) and 3960.31 MPH(TAS)

    So that's like going from Atlanta, Ga to Honolulu in just over an hour.

  4. Waverider by Jeng · · Score: 4, Informative

    So not only does this do Mach 6, but it also uses its own sonic booms to help with propulsion? Or did they just choose Waverider because it sounds neat?

    http://en.wikipedia.org/wiki/Waverider

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    1. Re:Waverider by bcmm · · Score: 5, Informative

      So not only does this do Mach 6, but it also uses its own sonic booms to help with propulsion? Or did they just choose Waverider because it sounds neat?

      It uses it's own shockwave for lift, not propulsion. This does, however, help it go faster, by eliminating the drag that adding wings would cause.

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    2. Re:Waverider by Idiomatick · · Score: 4, Funny

      They chose waverider since the US army sided with the autobot scum back in the 80s.

  5. Re:Uh hu by ShadowRangerRIT · · Score: 5, Insightful

    Commercial applications do usually follow. Whether or not you agree with it, military research has led to an enormous number of scientific advances that were initially used by the military but later disseminated more broadly. Jet engines, the Internet, cryptography, GPS, nuclear reactors, etc. Mach 6 might be inefficient overkill for Earth-side transportation, but it may provide a viable means of launching spaceflights one day.

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  6. That's almost as fast as... by GeekZilla · · Score: 3, Funny

    ...how quickly my home declined in value in 2008 and 2009!

    --
    Veritas patesco per quaestio questio. Truth is revealed through questions.
  7. Still a long way to orbit by Baldrson · · Score: 3, Informative

    Mach 6 is still a long way from Mach 22. Mach 22 is orbital velocity.

    1. Re:Still a long way to orbit by sanosuke001 · · Score: 5, Informative

      No it isn't. Mach is the speed sound travels in a medium (the atmosphere). As there is no atmosphere in orbit, you can't associate a mach speed value to orbital velocities.

      --
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    2. Re:Still a long way to orbit by GeekZilla · · Score: 2, Funny

      An unladen African Swallow?

      --
      Veritas patesco per quaestio questio. Truth is revealed through questions.
    3. Re:Still a long way to orbit by Idiomatick · · Score: 2, Funny

      Because in space no one hears you zoom pass them in your badass scramjet missile?

    4. Re:Still a long way to orbit by slaad · · Score: 2, Informative

      The point is that mach 22 isn't a set speed. It depends on your altitude (or more specifically, the speed at which sound travels through your surroundings). If you're in orbit you could say that you're traveling the equivalent of mach 22 at an altitude of x feet, but you wouldn't actually be traveling mach 22. You can't express velocity in space using a mach number.

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    5. Re:Still a long way to orbit by element-o.p. · · Score: 2, Funny

      Crap. And I just bought the aftermarket exhaust cans for my personal scramjet, since they were advertised to have a way cooler than stock exhaust sound. At least you'll still be able to see the underbody lights I added as I zoom past...

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  8. Mach 5 - Not Mach 6 by Maddog+Batty · · Score: 5, Informative

    Boeing announcement here:
    http://boeing.mediaroom.com/index.php?s=43&item=1227

    "In its first flight attempt, the Boeing [NYSE: BA] X-51A WaveRider today successfully completed the longest supersonic combustion ramjet-powered flight in history -- nearly three and a half minutes at a top speed of Mach 5."

    My understanding is that it didn't reach the 300 seconds Mach 6 burn it was hoping for. 200 seconds and Mach 5 isn't all that bad though...

    More here:
    http://www.theregister.co.uk/2010/05/27/x51_first_shot/

    --
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  9. Re:Interesting... by gatechman · · Score: 2, Funny

    According to my sources scramjet technology has gone well past Mach 6. The govt. doesn't want you to know this.

  10. Jet - Scramjet - And Questions! by Anonymous Coward · · Score: 4, Interesting
    • Jet engines still have propellers to compress air, into which the propellant is injected where this mixture then ignites.
    • Scramjets just use their immense speeds to do the compression with a funnel, but that also means they need more conventional means to reach these high speeds (such as getting a ride on a B52 plus gravity)

    Questions

    • What is the fuel efficiency per kilometer traveled?
    • Can a scramjet reach escape velocity, or get close enough so that additional oxygen for the fuel doesn't make up more than half the payload?
    • Did they find a new way to lose heat at supersonic speeds? Otherwise these rides will remain short ones.
    1. Re:Jet - Scramjet - And Questions! by MartinSchou · · Score: 3, Interesting

      Can a scramjet reach escape velocity

      If it is capable of propelling whatever it's carrying to 11.2 km/s (just under Mach 33 at the Earth's surface). Since this one only goes to 6, there's still a ways to go.

      Just as a foot note - if you're travelling at 11.2 km/s in a circle with a 6,378 km radius (Earth's equator), you will experience an acceleration opposite to gravity of 19.67 m/s^2 (aka 2 g). Just slightly slower if you do it at an altitude of 10 km (19.64 m/s^2). At the altitude this one reached, you'd hit 19.6 m/s^2

    2. Re:Jet - Scramjet - And Questions! by BJ_Covert_Action · · Score: 5, Interesting
      With regards to question 3, they have developed some pretty tricky ways to help cool the engines and the body of the vehicle. For instance, they cool the engines by circulating the JP-7 fuel through the body to absorb some of the heat to help bring it to the combustion point. This is very similar to how rocket nozzles are currently cooled to slow melting/failure:

      The scramjet will circulate the fuel behind engine walls to cool the structures. Without such active cooling, the temperatures in a scramjet could reach 5,000 deg. Fahrenheit, high enough to melt virtually any metal on Earth. Solving the cooling challenge is a major AFRL/Pratt & Whitney achievement.

      Source

      My wager is that the entire vehicle took thermal control into its design considerations and it uses a combination of geometry, aerodynamics, and fuel management to help sink heat at an appropriately high rate to prevent too much for a build up. However, since I don't have the design specs, and I doubt anyone outside of the military will, for awhile at least, I can only speculate. You also have to understand that at those speeds, your gas dynamics become a problem of rarified gasses and heat management becomes a very tricky problem indeed, one that can't be approached by traditional cooling means. So in summation I would guess yes, they have probably found some very cool new ways to sink heat at hypersonic speeds.

    3. Re:Jet - Scramjet - And Questions! by blair1q · · Score: 4, Informative

      Atmosphere isn't just compression, it's reaction mass. The compression creates the conditions for acceleration when the fuel is burned, but it's heating of the compressed air that causes the high force that accelerates the air backwards, accelerating the vehicle forwards.

      You can bring your own oxygen, but it's just going to make a pretty flame coming out both sides of the combustion chamber unless there's mass flowing into the inlet and being pushed out through the nozzle.

      I said this above already, but what you do here is you use a first-stage rocket motor to get up to scram-jetting speeds. Then the second-stage motor gets you to a certain point in the atmosphere where it loses thrust. Then you light your third stage.

      This makes sense only if the specific impulse (look it up) from the scramjet exceeds that from a rocket motor, or it's ridiculously cheap and still gets the job done. I'm guessing it's not ridiculously cheap. But given that you don't have to bring the reaction mass for the scramjet with you, it might be more efficient than a rocket of the same mass. Meaning you can omit a heavy rocket motor and use a lighter scramjet and put the saved mass into the payload.

  11. Re:Interesting... by joggle · · Score: 4, Informative

    According to the article there's three more vehicles which will be tested in the fall.

  12. Re:Interesting... by Pojut · · Score: 5, Interesting

    Scramjets aren't exactly easy to test in the lab.

    Hell, even normal jet engines are tough to test. Have you seen the equipment used to keep those things stationary while testing them? Holy fuck .

  13. Re:Uh hu by Anonymous Coward · · Score: 5, Funny

    Fine. Except for jet engines, the Internet, cryptography, GPS, and nuclear reactors what has the military done for us?

  14. Re:Uh hu by Pojut · · Score: 4, Funny

    Little plastic Army Men

  15. Amazing by maillemaker · · Score: 4, Interesting

    It's amazing to me that they can make a machine who's parts are GLOWING they are so hot and the metal still functions without failing.

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    1. Re:Amazing by characterZer0 · · Score: 5, Funny

      Like incandescent light bulbs?

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    2. Re:Amazing by BobZee1 · · Score: 2, Interesting

      The company I work for makes the parts in what "they call" the hot section of the engine. These are some really awesome materials. I fly a desk so I don't get to play with the goodies.

      --
      dumber people are doing harder things everyday
    3. Re:Amazing by RobVB · · Score: 3, Funny

      You fly a desk and complain about the goodies? Your company must have some Awesome goodies.

      Just out of curiosity, what's the air-speed velocity of your unladen desk?

      Also, describe some of those goodies to me.

      --
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    4. Re:Amazing by GameboyRMH · · Score: 3, Funny

      Just out of curiosity, what's the air-speed velocity of your unladen desk?

      And, GP, do you have the European or African market version?

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    5. Re:Amazing by longacre · · Score: 2, Funny

      But they're SOOOO YUMMY.

      Oh, I thought you said Cinnabons.

  16. Re:FYI... by Anonymous Coward · · Score: 3, Insightful

    Assuming the acceleration is modest, her facial expression aqt Mach 6 should be identical to when she's sitting on her living room sofa.

  17. Re:Interesting... by beelsebob · · Score: 2, Informative

    Yes, but not scramjet technology that uses ordinary jet fuel to power the engine. Said scramjets used hydrogen instead, and can't maintain flight for long because of how bulky the large hydrogen tanks are.

  18. Re:For those of you who don't know how fast Mach 6 by vlueboy · · Score: 5, Interesting

    Mac 5 melts aluminum steadily
    Mac 6 melts steel

    And don't forget that keeping this friction heat down also requires a good deal of power.

  19. Re:Interesting... by geckipede · · Score: 3, Informative

    The differences are in how compact the engine is and exhaust velocity. Airliner engines are designed solely for efficiency and as such have bypass ratios that make start to look like a helicopter mounted sideways in a tube. The actual power generating bit of the engine is tiny and most of the thrust comes from shunting air through the outer parts at relatively low speeds without ever being compressed.

    Generating exhaust simultaneously at high rate, high velocity and in a compact package is vastly different.

  20. Didn't hit mach 6, just mach 5! by PeterM+from+Berkeley · · Score: 5, Informative

    Hello,

        The story is in error. Per this link, the plane only hit Mach 5, not Mach 6. This is still a pretty successful test, however.
    Link: http://www.msnbc.msn.com/id/37377401/ns/technology_and_science-space/

    --PeterM

    1. Re:Didn't hit mach 6, just mach 5! by slaad · · Score: 2, Interesting

      Most sources seem to be reporting mach 5, but that msnbc article is rather funny. The caption by the picture says mach 6 and then the article itself says mach 5.

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  21. Re:Uh hu by jeffmeden · · Score: 3, Informative

    Are you trying to point out that the internet wasn't a military innovation by stating its purpose was to track nuclear weapons (*military* nuclear weapons)?

    And for what it's worth, the original purpose was to allow communication between points with no single path of failure (insert beneficial military application here like giving combat orders in the event of a nuclear strike); it started in universities, national labs, and large military bases who had the budget to pull the wires, and before we knew it there were all kinds of fun uses for it like MUD games and e-mail and slashdot and finally facebook; the ultimate military weapon.

  22. Re:Uh hu by Dishevel · · Score: 4, Informative

    Radial Engines, Kevlar, Ceramic Technologies, Radar, Microwaves, Food Preservation, Someone else keep this going.

    --
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  23. Re:Interesting... by stjobe · · Score: 2, Interesting

    I agree that using the J58 as an example of a typical jet engine is rather like using an atom bomb as an example of an explosion.
    At the same time, since the J58 is essentially a turbojet/ramjet hybrid, it might be said to be the distant forefather of the X51 engine.

    Oh, and anything that makes me go look at pictures of the most beautiful aircraft in the world, the SR-71, is a good thing.

    --
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  24. Re:FYI... by Shakrai · · Score: 2, Funny

    If she's like my mother in-law she'll look at you with a blank expression and say "What's Mach mean?"

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  25. Re:Uh hu by newcastlejon · · Score: 2, Informative

    Rocketry. 'Nuff said.

    --
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  26. Re:Uh hu by OzRoy · · Score: 3, Funny

    Brought peace!

  27. Re:Interesting... by phoenixwade · · Score: 4, Informative

    Others have expressed the detail, so I won't be redundant, but the J58 is on the extreme end of Jet technology even today, and that was the point of my analogy. Those airliner engines you mention produce more thrust and are more economical to operate and to maintain, by a very healthy margin. However, they are only good up to about 500 kts or so, as opposed to the 2000+ kts the J58 is capable of. Nor will they function at all about 60000 feet, whereas the j58 will at full or nearly full thrust. So, in comparison, modern airline engines of which you speak are not in the same class of tech, nor would you expect them to be, since their purposes are far different. On a side note; it's note related to the tech of the engines themselves, of course, but those airline engines also will never push as pretty an airframe through the air, wich disqualifies them on the asthetic front too.... {smile}

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  28. Re:For those of you who don't know how fast Mach 6 by JMZero · · Score: 5, Funny

    Even at Mach 3, you want a layer of foam to avoid burning.

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  29. Re:So by gimmebeer · · Score: 2, Insightful

    The SR-17 had a combo turbojet/ramjet engine, it's forseeable that an updated engine could make the ramjet-scramjet leap.

  30. Re:FYI... by ElectricTurtle · · Score: 2, Informative

    Such epic pedantry does not deserve Troll moderation.

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  31. there *is* atmosphere by SuperBanana · · Score: 2, Informative

    No it isn't. Mach is the speed sound travels in a medium (the atmosphere). As there is no atmosphere in orbit, you can't associate a mach speed value to orbital velocities.

    You start out in the atmosphere, chief. Also, Wikipedia specifies a Mach number for LEO.

    Even in LEO, there is air- it's just very, very, very thin. The atmosphere doesn't end at a hard line.

    Why do you think objects in LEO gradually slow down and re-enter? Answer: aerodynamic (and solar) drag.

  32. Re:Interesting... by jabelli · · Score: 2, Informative

    If you're required to carry your own oxidizer, it's a rocket engine, not a jet engine.

  33. Glowing metal = black body radiation by spineboy · · Score: 4, Informative

    The temperature of objects produces (from what i recall of physics) black body radiation - meaning it produces light wavelengths. Just because we associate melted iron being red hot, doesn't mean other metals melt when they start to glow. It just means they are hot enough to produce enough black body radiation that we can see. Look at mercury for example as an opposite.

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  34. Re:Interesting... by element-o.p. · · Score: 4, Informative

    I think you misunderstand his point (or perhaps I am giving him too much credit for asking a really good question). Mach speeds are a ratio of the speed of the aircraft to the speed of sound. Mach 6 therefore means "six times the speed of sound". OK, nothing difficult there; most people here probably knew that already. Here's the rub: what is the speed of sound? Hint: it's not the same at sea level and at the 0.1Mm you mention, because the speed of sound varies with the density of the atmosphere. In other words, Mach 6 at sea level (~4500 mph) is not the same speed as Mach 6 at, say, 100,000 feet above sea level (~4100 mph).

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  35. Re:Uh hu by element-o.p. · · Score: 3, Funny

    Well, for one, neither German, Japanese, nor Russian is my native language...

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  36. Re:Sub-orbital transport dominates by Gilmoure · · Score: 2, Informative

    New Mexico's already building their space port. Will be interesting to see if sub-orb traffic takes off.

    --
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  37. Re:logical fallacy by mdarksbane · · Score: 2, Insightful

    It is almost assured that they would have happened later, though, since they didn't beat the military research to begin with.

  38. Re:Interesting... by Gravitron+5000 · · Score: 2, Insightful

    They weren't measuring speed relative to the ground. They were measuring speed relative to itself.

    Umm, I think it was stationary relative to itself.

  39. in the fall? by circletimessquare · · Score: 4, Funny

    you mean in the autumn?

    or in the spectacular screaming descent towards land?

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  40. Re:Uh hu by jimbolauski · · Score: 2, Funny

    and those guys who forcibly sent that kid back to Cuba.

    Janet Reno?

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  41. Re:Interesting... by fahrbot-bot · · Score: 2, Interesting

    How useful is this in the long run?

    The usefulness, overlooked in the summary and (brief) article, but reported in The Register (longer article), is that this vehicle used jet fuel (JP-7) instead of Hydrogen. Additionally, it apparently flamed out at Mach 5, not 6.

    The hypersonic X-51A ignited, burning a mixture of ethylene and JP-7 jet fuel, and once well alight switched over to all jet fuel operation.

    --
    It must have been something you assimilated. . . .
  42. Re:i find that hard to believe by h4rr4r · · Score: 2, Funny

    How much do you think is left after it hits the sea at Mach 6?

  43. Re:FYI... by Sique · · Score: 3, Insightful

    Or you just lie flat on the earth and let gravity do about the same.

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    .sig: Sique *sigh*
  44. Re:FYI... by Bobby+Mahoney · · Score: 2, Informative

    Not to be a stickler, but mach is a relative number based on air density (altitude/pressure), so unless they tested the thing at 5' above the waves or something, it's more like 220 miles in that 200 second time frame (assuming 50,000 ft). That makes it way less cooler, I know.

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    !#&*
  45. Re:Interesting... by Rei · · Score: 2, Insightful

    Useful??? They had to use a B-52 to get into the air. Then a rocket booster to go to 4.5Mach. Then this precious little stove pipe took it to 5.0 Mach.

    Yeah! How can you call that useful? And speaking of wastes of time during our war with the Japs and the Nazis, did you hear what those crazy eggheads over at Los Alamos are doing? They're trying to build a "nuclear bomb" -- but all they've managed to do so far is irradiate a bunch of scientists. How is that useful?

    (/snark)

    This is a *test program*, not a final product. It's designed to gather data. This was the first flight of a hydrocarbon-burning scramjet, yet it's already managed an acceleration and climb rate faster than a typical commercial aircraft -- but in conditions of orders of magnitude greater drag. It would have gone faster and higher, but it had a flameout 200s in -- again, not that unusual in a first-of-the-kind test.

    Scramjets are not designed to be standalone engines. They're meant to be a "mid stage" engine to orbital rockets or a final stage for high-speed intercontinental aircraft, operating in an . For orbital craft, the scramjet craft is either part of the first stage carrier rocket which launches payloads with a small kickstage, or itself has a small kickstage for final orbital maneuvers. Initial thrust for scramjet powered vehicles is to be provided by some combination of rockets, advanced jets, ramjets, or hybrids of the aforementioned techs. A particular hybrid of interest is the "dual mode" scramjet/ramjet combination, designed to operate from around Mach 1 or so up to 1/2 to 2/3rds of orbital velocity. To get up to Mach 1, cheap droppable rocket boosters are what will probably be used, at least early on. But what's really possible is at this point still a big subject of debate, and a lot more data is needed.

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    Present day. Present time.
  46. Re:Now can the truth come out? by Iron+Condor · · Score: 2, Informative

    There's as much concrete evidence the Aurora exists as there is evidence Bigfoot exists.

    --
    We're all born with nothing.
    If you die in debt, you're ahead.