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Second Test of X-43A Scramjet Tomorrow

pinkUZI writes "NASA says its new Hyper-X, a jet capable of flying some 5,000mph - seven times the speed of sound - will be ready to take a test cruise across the Pacific this Saturday. This is actually NASA's second attempt; the first, in 2001, failed when stabilizing fins flew off the plane's booster rocket and controllers ordered the craft destroyed. CNN has the story." NASA's mission web page has more information, photos, etc.

325 comments

  1. Darwin Award winner by wawannem · · Score: 1, Offtopic

    Is this where someone is supposed to make a reference to the urban legend about someone attaching a jet engine to their car and crashing into the side of a mountain? You know, the one where they say that they only found a few teeth and fingernails embedded in the dashboard.

    1. Re:Darwin Award winner by intertwingled · · Score: 2, Informative

      Happened in Arizona, reputedly. I quick google yields: http://www.snopes.com/autos/dream/jato.asp

      --
      -- SKYKING, SKYKING, DO NOT ANSWER.
    2. Re:Darwin Award winner by dave420 · · Score: 1

      The dude in the caddy with the JATO (jet-assisted take-off)? That one was debunked ages ago. The problem with the darwin awards is it attracts so many fakes. Nearly every example of a darwin-award nominee is faked. It's annoying, as it's really philosophically (and comically) interesting...

    3. Re:Darwin Award winner by axis-techno-geek · · Score: 1
      ...but then you could say:

      "Why don't you make like a jet, and scram." ;)

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    4. Re:Darwin Award winner by Democracy_0001-Alpha · · Score: 0

      I believe this is the thoughts that come across that person's mind. - "Why not make a BatMobile and testrun it myself." He make exactly 2 mistake in that "expierment." First, testing a theorically fast car near mountain. (You suppose to test in on open field) Secondly, you never test an experimentally cars youself. If anyone ever seen an air craft engineer actully sit in the expiermentally air craft and test it him/her self please reply, and please cite the site.

  2. Dupe.. by hookedup · · Score: 5, Informative
    1. Re:Dupe.. by hookedup · · Score: 0, Redundant

      what in the hell is with the mods? this is seriously getting out of hand.. the article was posted yesterday people..

    2. Re:Dupe.. by perly-king-69 · · Score: 3, Funny

      You're new here, right? ;-)

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      This sig is inoffensive.

    3. Re:Dupe.. by hookedup · · Score: 1

      heh not too new.. but now i realize why so many people turn to trolling..

    4. Re:Dupe.. by stoolpigeon · · Score: 4, Funny

      what's worse is michael posted both

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      It's hard to believe that's how Micronians are made. Why don't we see it right now by having you both kiss one another?
    5. Re:Dupe.. by Anonymous Coward · · Score: 0

      yep

    6. Re:Dupe.. by IWorkForMorons · · Score: 1, Funny

      Dude...don't turn to trolling. Sure, it's fun at first. Especially back when I was a teenager discovering IRC. Man, you've never felt anything like successfully baiting Christian into telling you off. You wouldn't believe the things Christians will type but not say. Ahhhhh....I miss those days. But anyways, don't start trolling. Not here anyways. Geeks are your friend.

    7. Re:Dupe.. by Anonymous Coward · · Score: 0

      In Soviet Russia, the mods are asking...
      what the hell is up with YOU!?!!

    8. Re:Dupe.. by Anonymous Coward · · Score: 0

      No, I'm not new, I just didn't look to see if I already had an account before I created a second one.

    9. Re:Dupe.. by Anonymous Coward · · Score: 0

      Uh...I was replying to the guy who said he understood why people turned to trolling. I replied to his post with advice regarding trolling, and trying to be funny at the same time. Why the hell would this be marked off-topic? Christ...Mods: take the stick out or your arse and relax. ____ IWorkForMorons

    10. Re:Dupe.. by Anonymous Coward · · Score: 0

      Gee... wonder if he gets paid by the story?

    11. Re:Dupe.. by Anonymous Coward · · Score: 0

      Only if it's a dupe.

  3. still need ... by pvt_medic · · Score: 4, Interesting

    the b-52 to launch the plane. Will they be able to develop on of there that can take off on its own? or will we always be launching them from the underbellies of a big plane.

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    1. Re:still need ... by Anonymous Coward · · Score: 5, Informative

      Um, this is primarily a test of an engine, not an aircraft.

      The X1 was also launched from a plane and was the first aircraft to break the sound barrier. Planes such as the SR-71 have far surpassed this speed and takeoff in the conventional fashion.

      I'm not sure what you're referring to when you state "always be launching them from the underbellies of a big plane".

    2. Re:still need ... by Profane+MuthaFucka · · Score: 2, Informative

      Yes, they will be able to do that. For subsonic flight, it would use regular engines. Once it got fast enough, the SCRAMJET would take over. This one gets around all that by using a rocket to accelerate it to the right speed before engine ignition.

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    3. Re:still need ... by n0mad6 · · Score: 5, Informative

      Obviously if this method of propulsion is used in aircraft that are anything but proof-of-concept, they'll have to take off on their own power. However most of these experimental aircraft are dropped from the belly of an aircraft already at altitude, even manned aircraft like the X-1 and X-15 (both rocket-powered, dropped from a B-29 and B-52 respectively). For the most part, getting the aircraft to the needed altiude on its own would require too much fuel (making the need to design a much bigger aircraft, etc.).

    4. Re:still need ... by J.+Jacques · · Score: 5, Informative

      It's a test flight, not a full-fledged production vehicle we're talking about here. The plan is that eventually aircraft will take off under normal jet propulsion, use scramjets to accelerate to escape velocity, and use chemical-powered propusion once they have left the atmosphere.

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    5. Re:still need ... by Anonymous Coward · · Score: 0

      RTFA...

      "That kind of craft would probably employ multiple propulsion systems including a turbo-jet to reach supersonic speeds, scramjets to take the vessel to the edge of the atmosphere and then chemical rockets to enter the void of space."

      Regards, AC.

    6. Re:still need ... by intertwingled · · Score: 1

      What about the Messerschmitt Me 163B Komet? The first and only operational rocket fighter aircraft? It wasn't very effective, but man, it must have been a helluva ride!

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    7. Re:still need ... by Waffle+Iron · · Score: 4, Interesting
      The B-52 isn't the big deal. Instead, it's multimillion dollar conventional Pegasus rocket booster that gets the test vehicle up to speed. The Pegasus has been in use for a long time to launch small payloads into orbit; it's always dropped from an airplane.

      What I don't quite understand is why they need a rocket capable of reaching orbit just to get the X-43 up to ~mach 5 so it can start it's engines. It seems like overkill to me. I would suppose they only use the Pegasus's first stage; maybe they had some cheap spares laying around.

    8. Re:still need ... by alecks · · Score: 2, Interesting

      How do they catch it afterwards? Or do they let it fall in the ocean?

    9. Re:still need ... by trs998 · · Score: 5, Interesting

      Wouldnt it have a problem with wing size?

      flying at 5,000 mph, you'd basically have all the body lift yo'd need... the SR-71 (aka Habu or Blackbird) uses small wings and is very specialized.

      The SR-71 has tiny wings, and consists of 2 huge engines.. it also leaks fuel onto the runway until the body heats up to running temperature.

      The point being that the SR-71 has a very high take off and landing speed due to the small lift per mile figure. It will fly straight up and over a thousand mph until the engines run out of oxygen at nigh on 100,000 feet.

      A aircraft using the scramjet capable of 5,000 mph would have to have very small wings for low air resistance and wouldnt need large lift per mile.
      The ScramJet wouldnt work at low speeds, therefore the runway would have to be very long to take off using a conventional JATO (Jet Assisted Take Off) unit to get the ScramJet working. Getting a scramjet off the runway is going to be interesting!

      BTW, what engine does the proposed (Active?) Aurora reconissance/spy plane use? It's supposed to have a very high speed (~3000-4000 mph?)

    10. Re:still need ... by Anonymous Coward · · Score: 1, Interesting

      Actually, there is a second, less publicized part of the X-43 program. The X-43A-LS is a low-speed version of the Hyper-X, and it is designed to take off and land from a conventional runway. There are some differences in the two aircraft, though: the -LS has slightly larger wings and tails than the Hyper-X, due to the speeds that it flies at, and the propulsion system that it uses: the -LS uses a model aircraft turbine engine. More info on the X-43A-LS: www.accurate-automation.com.

    11. Re:still need ... by Anonymous Coward · · Score: 0

      The Komet had a flight range of only 62 miles.

    12. Re:still need ... by Anonymous Coward · · Score: 0



      Did anyone else notice this was submitted by pinkUZI? pinkUZI is a fucking dumbass - don't read stories submitted by that user.


    13. Re:still need ... by Anonymous Coward · · Score: 0

      Well, isn't this interesting?

    14. Re:still need ... by skinny.net · · Score: 5, Funny

      They don't need the B-52! Because of the power of the X-43a, it is taking off with a B-52 on its back just to show off!

      Please don't mod this informative.

    15. Re:still need ... by essreenim · · Score: 1

      ..and then fly to the moon!
      Come fly with me, lets fly, lets fly away....oo

      I hope the windows will be circular and the detination - anywhere, so long as its via Saturn and Jupiter..

    16. Re:still need ... by HokieJP · · Score: 5, Insightful

      I think they're using it because its cheaper than designing a whole new rocket just for three flights.

      Plus, the plane is the subject of the experiment, so you want to minimize the number of possible failure points in all the other systems. Using a booster thats already proven is a great way to do this. Of course, in flight one it was the booster that failed...

    17. Re:still need ... by MrCocktail · · Score: 3, Interesting
      An article describing some sc/ramjet technology. For the impatient:


      The scramjet propulsion system uses different kind of technology than traditional rockets. Instead of carrying both fuel and oxygen to ignite, the scramjet uses oxygen in the atmosphere. To get the oxygen to ignite the fuel, it needs to take the oxygen into its combustion chamber at extremely high speeds.
    18. Re:still need ... by MrCocktail · · Score: 1

      Whoops, didn't complete my thought. Therefore, the Pegasus booster is used to get the X-43A to a sufficient speed where the scramjet will actually work. Other people have also said that using the Pegasus booster first means they don't have to pile on a whole lot of other crap onto the X-43A just to test the scramjet aspect.

    19. Re:still need ... by Anonymous Coward · · Score: 4, Informative

      the SR-71 (aka Habu or Blackbird) uses small wings and is very specialized.

      The SR-71 has tiny wings,


      Small wings? Have you ever looked at an SR-71? With a wing span of 55 and a half feet, and a wing area of 1795 square feet, its wings are far short of "small". A 737 only has a wing area of 1344 square feet.

      Low lift wings maybe, making for less wind resistance and friction, but small, not hardly.

    20. Re:still need ... by Anonymous Coward · · Score: 1, Informative

      If by "conventional" you mean "needs exotic accelerant to burn fuel and immediate refueling after take-off", then yeah, sure, ok.

    21. Re:still need ... by Anonymous Coward · · Score: 0

      No, conventional takeoff as in "takes off from the ground" rather than being dropped from another aircraft.

    22. Re:still need ... by EvvL · · Score: 1

      Suposedly "Aurora" uses a Pulse Detonation Engine from what I've heard.

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    23. Re:still need ... by Steepe · · Score: 2, Informative

      The SR71 needed that stuff because it flew over mach 3 at almost 100k feet. the friction and heat buildup from going that fast that high was beyond the metals used back in the days the SR-71 were designed. New spy planes (aurora) can do the same without the loosly put together skin. (which is why the SR-71 leaked like a siv on the ground.

      A more useful comparison would be with an F15-e or F16, more than capable of traveling at mach 2ish, no refueling right after takeoff, regular old jet fuel.

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    24. Re:still need ... by MachineShedFred · · Score: 1

      Please don't mod this informative.

      You didn't expect moderators to actually READ the post; much less THINK did you?

      You must be new here...

      Oh, and dollars to donuts says that the same moderators I just talked about are now going to bomb my karma into oblivion.

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    25. Re:still need ... by DerekLyons · · Score: 1
      It's a test flight, not a full-fledged production vehicle we're talking about here. The plan is that eventually aircraft will take off under normal jet propulsion, use scramjets to accelerate to escape velocity, and use chemical-powered propusion once they have left the atmosphere.
      And it will be more complex, heavier, lower performing, and have more potential failure modes than the conventional rocket it replaces.

      Such a bargain.

    26. Re:still need ... by Anonymous Coward · · Score: 0

      that's not entirely true. even old biplanes broke the speed of sound for short periods in dives and survived.

    27. Re:still need ... by Anonymous Coward · · Score: 0

      They are going to use some buildings in Haiti. They were going to use some in Iraq, but they had to blow it up before it hit the target^H^H^H^H^H^Hlanding pad.

    28. Re:still need ... by Phurd+Phlegm · · Score: 1
      New spy planes (aurora) can do the same without the loosly put together skin. (which is why the SR-71 leaked like a siv on the ground.
      You forgot to say "mythical aurora." There is no real evidence of its existance. The A-12/SR-71 didn't stay secret for nearly as long as people have been claiming Aurora has been operational. I'm sorry (since it sounded cool), but I don't think it exists.
      A more useful comparison would be with an F15-e or F16, more than capable of traveling at mach 2ish, no refueling right after takeoff, regular old jet fuel.
      The actual range at mach 2 in something like an F-15 is much less than you might think--I recall something in the low hundreds of miles. The range of an SR-71 at mach 3 is something like three thousand miles, according to this link from the Air Force Museum. Punch line: if you're planning a fast trip in an F-15, you're going to be doing aerial refueling.
    29. Re:still need ... by Dyolf+Knip · · Score: 1
      And it will be more complex, heavier, lower performing, and have more potential failure modes than the conventional rocket it replaces.

      Interesting claim, especially given that scramjets have no moving parts, no theoretical upper speed limit, and are expected to be around 3 times more fuel efficient that today's best liquid chemical rockets (which are very near the maximum allowed by physics), to say nothing of being able to ditch a great deal of fuel and oxidizer (the shuttle, IIRC, takes along a few million pounds of LO2).

      Scramjets certainly will have difficulties. Chief among these is the fact that it can't ignite at anything less than mach 5, thus necessitating other propulsion systems which would, as you point out, be so much dead weight at scramjet & orbital speeds. There is also the materials problems of surface heating of a plane approaching orbtal velocity of mach 26.

      So, nobody is suggesting that scramjets are as simple as legos. But if you're going to argue against even _trying_ to use them, at least pick some limitations that really exist. You might also notice that while advanced rocket technology is over 50 years old, it was the nevertheless the rocket boost that caused of the failure of the last test, not the scramjet.

      --
      Dyolf Knip
    30. Re:still need ... by Steepe · · Score: 1

      Your absolutely right about the f15 and mach 2, I was just letting the original poster know that just because an 1950's high altitude spy plane is refueled in the air right after takeoff, (actually at 40k', when its skin seals up real good) doesn't mean we are incapable of building one. He was insinuating that because the SR-71 leaks we can't build a bird that can do the job.

      I also find it hard to believe we (the US.. greatest country in the universe) would retire the SR-71 without a replacement.

      --
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    31. Re:still need ... by DerekLyons · · Score: 1
      So, nobody is suggesting that scramjets are as simple as legos.
      You are right, nobody is doing so. But what they *are* doing is arguing that airbreathers are inherently superior to rockets, and they aren't when you look at the real numbers.
      But if you're going to argue against even _trying_ to use them, at least pick some limitations that really exist.
      Which is exactly what I did. As you point out, you need other systems to get the scramjets up to ignition speed (which makes the airbreather more complex than the rocket stages it replaces). Scramjets might be more fuel efficient, but you still need great gobs of fuel for the systems that get them up to ignition speed, which is a huge performance hit. There's also the TPS, which along with the acceleration systems introduce more failure modes than the rocket stage they replace. As you point out, the scramjet itself has no moving parts, but all the supporting systems have them in abundance, and the price you pay for this abundance is a stage that peforms half as well as the simpler rocket stage it replaces. (And 'moving parts' are only a subset of 'failure modes'.)

      The simple fact is that while the theory of airbreathing stages is powerfully seductive, the reality is that they simply don't work out in practice once you look at the real numbers. They only way to make airbreathers come out on top is with wildly optimistic and utterly unfounded claims of what they might do at some point in the future.
    32. Re:still need ... by Dyolf+Knip · · Score: 1
      Indeed it is. But the application thereof is barely in its infancy. Rockets have been shown for 50 years to be usable for LEO launches, but just barely. They are too fuel hungry, too heavy, too inefficient, requiring systems that are too large and too unwieldy to be reliable and cheap. So much of the thing is given over to the fuel and the rockets that payload capacity is practically a minor side bonus. At best, rocket launches have never been less than one or two thousand dollars per pound to LEO. With expenses like that, the entirety of space, the universe as a whole, is basically a pork project for various congress-criters.

      Honestly, I have no particular affinity for scramjets. What I want, what we all _need_, is a decent means of LEO entry. Rockets don't quite cut it. Scramjets might. As might laser launches, or beanstalks, or whatever. Considering the rewards the human race could reap from opening up space, it's worth trying the more promising avenues.

      Remember, the US has spent hundreds of billions of dollars (inflation adjusted) on projects which, though they may have been nifty, even awe inspriring, did not really let anyone _do_ anything in space (Apollo & ISS come to mind). IIRC, NASA has put 3 orders of magnitude less than that into this particular approach; less than the cost of a single Shuttle launch.

      You may be right. Scramjets may not work at all, or function but be even less economical than rockets. But so far They've spent (relatively speaking) chump change on finding out, and what we stand to gain from cheap LEO access is worth it.

      --
      Dyolf Knip
    33. Re:still need ... by Democracy_0001-Alpha · · Score: 0

      The air on sea level is way too dense compare to air like 10,000 m above sea level. If its going to boost that fast near sea level, I personally believe the air craft frame will melt. Secondly, the fuel mention earlier is important. With super, and hyper, sonic jets, to keep the engine warm is crucial. Take the famous Concords Super Sonic Jet for example; it use 6 time more fuel when its on the ground then when it is in air. The take off and gaining the required height parts of an air craft is the most fuel consuming time during the whole flight. Secondly, I don't believe there is actully an X-series air craft that take off from sea level. Finally, X, like F stand for Fighter and B stand for Bomber, it stand for eXperiment. It is a mean of testing the air craft frame and engine. It was never mean to be "tradictional."

    34. Re:still need ... by DerekLyons · · Score: 1
      Indeed it is. But the application thereof is barely in its infancy. Rockets have been shown for 50 years to be usable for LEO launches, but just barely. They are too fuel hungry, too heavy, too inefficient, requiring systems that are too large and too unwieldy to be reliable and cheap.
      Fuel hungry? So what? Oxidiser and fuel are cheap. Rocket engineers would love to get their systems down in cost to where fuel costs are important. Too heavy? Compared to what? No airbreather, current or proposed, weighs in at less than twice what it's rocket equivalent would. Large and unwieldy? No airbreather, current or proposed, is even as small as twice the size as the rocket stages it replaces. No airbreather, current or proposed, is anywhere nearly as cheap as the rocket stages it replaces.

      The bone simple fact is that the numbers don't favor the airbreather.

      So much of the thing is given over to the fuel and the rockets that payload capacity is practically a minor side bonus. At best, rocket launches have never been less than one or two thousand dollars per pound to LEO. With expenses like that, the entirety of space, the universe as a whole, is basically a pork project for various congress-criters.
      An airbreather won't be much better as far as mass fractions go, airbreathing engines are pound for pound less fuel efficient than rockets. Rockets not being reliable or cheap is an artifact of their development history and politics, not an inherent property. (And their expense is coming *down*, as the X-Prize vehicles are demonstrating.)

      The remainder of your comments hinge on your basic misunderstanding that the current situation is the way it ever will be.
    35. Re:still need ... by Anonymous Coward · · Score: 0

      Please don't mod this informative.

      Did you add that to guarantee the "+5 Funny"?

    36. Re:still need ... by pfdietz · · Score: 1

      A scramjet that flies at a single speed doesn't need moving parts. A scramjet that is intended to operate over a large range of speeds -- as it would have to do in a launcher -- probably needs a variable geometry inlet.

      The cooling system for that hypersonic leading edge also probaby has lots of moving parts (as well as miles of channels for all the coolant.)

    37. Re:still need ... by pfdietz · · Score: 1

      Scramjets aren't more fuel efficient for launch to orbit. They are potentially more propellant efficient -- but they achieve that by using more fuel and less (onboard) oxidizer. Unfortunately, LOX is really cheap and dense, while LH2 is more expensive, and much less dense.

  4. The parent post should be modded as REDUNDANT by Anonymous Coward · · Score: 0, Informative

    Why are you posting AGAIN ??? and on the same subject?

  5. scramjet? by SoTuA · · Score: 5, Funny
    I thought it was an HP printer...

    Da-dum-ching!

    1. Re:scramjet? by qc_dk · · Score: 2, Funny

      no no, you're thinking of the HP ScrambleJet

    2. Re:scramjet? by The_Mr_Flibble · · Score: 5, Funny

      However Hp are seeking legal representation regarding trademark infringment. A spokesman for hp said "We wouldn't want our customers getting the two technologies confused and trying to fly on one of our printers".

    3. Re:scramjet? by callipygian-showsyst · · Score: 3, Funny

      You're thinking of HP's low cost laser, the "ValueJet".

    4. Re:scramjet? by Anonymous Coward · · Score: 0

      I thought it was an HP printer...

      No. you're thinking of ScamJet, and they've been bought out by Lexmark

    5. Re:scramjet? by Anonymous Coward · · Score: 0

      or was he thinking of HP's joint venture with IBM, JetBlue

    6. Re:scramjet? by Anonymous Coward · · Score: 0

      The HP consumables are still 2 times as expensive as the Scramjet. ;)

    7. Re:scramjet? by Kiryat+Malachi · · Score: 1

      You mean ValuJet, right?

      Bringing a new meaning to the term "system crash".

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    8. Re:scramjet? by Anonymous Coward · · Score: 0

      is that the one that only prints pictures of the flordia everglades?

  6. Favorite Quote on Hypersonic Travel by ansible · · Score: 5, Insightful

    Gordon D. Pusch wrote in sci.space.tech: "Hypersonic travel combines all the disadvantages of airplanes with all the disadvantages of rocket flight and all the disadvantages of re-entry --- continuously."

    1. Re:Favorite Quote on Hypersonic Travel by LBArrettAnderson · · Score: 0

      as well as all the advantages of airplanes with all the advantages of rocket flight and all the advantages of re-entry continuously.

    2. Re:Favorite Quote on Hypersonic Travel by SmackCrackandPot · · Score: 2, Funny

      Remaining on the ground combines all the disadvantages living on the surface of a planet with all the disadvantages of orbiting a star and all the disadvantages of being inside the orbit of an asteroid belt - continuously.

    3. Re:Favorite Quote on Hypersonic Travel by Anonymous Coward · · Score: 1, Insightful

      Leaving the surface of a planet combines all the disadvantages of being inconceivably distant from an energy source, with all the disadvantages of being inconceivably distant from a food source, with all the disadvantages of being exposed to continual hard radiation, with all the disadvantages of having your body waste away from lack of gravity - continuously.

    4. Re:Favorite Quote on Hypersonic Travel by SmackCrackandPot · · Score: 1

      But at least you don't get woken up by your neighbors at 4am.

    5. Re:Favorite Quote on Hypersonic Travel by Anonymous Coward · · Score: 0

      I like the cut of your jib young man!

  7. Space flight? by spellraiser · · Score: 4, Interesting

    The article starts off with this:

    The space agency's dogged pursuit of extreme speed, officials hope, will ultimately make space flight easier to accomplish.

    OK, so exactly how is this supposed to aid space flight efforts? There is no mention made of that in the article at all.

    I would have thought that the ability to reach incredible speeds in horizontal flight inside the atmosphere is unrelated to both:

    1) Entering orbit (horizontal flight).

    2) Flying in vaccum (different conditions than in atmosphere).

    I'm confused ... any thoughts?

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    1. Re:Space flight? by Profane+MuthaFucka · · Score: 0

      Even launching a rocket from a moving jet at 35000 feet saves a trememdous amount of fuel vs. launching from the ground. If you could piggyback a rocket on a plane above 100,000 feet travelling at Mach 8, the cost to get into space would drop dramatically. Perhaps by a factor of 5, because of the smaller booster required.

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    2. Re:Space flight? by pe1rxq · · Score: 4, Interesting

      It is important as it might enable more efficient ways to bring stuff into orbit.
      At the moment the only viable way to get stuff in orbit is by strapping a shitload of explosives under it.
      Remember, it is horizontal speed that results in the air pushing a winged body upward towards that vaccum so it is not totally unrelated to space flight.

      Jeroen

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    3. Re:Space flight? by Anonymous Coward · · Score: 0

      1) Entering orbit (horizontal flight).

      You mean vertical, right? :P

    4. Re:Space flight? by Analogy+Man · · Score: 3, Informative

      The trajectory of a conventional rocket accomplishes 2 things...getting up...and getting to orbital speed. This approach really replaces the first nearly vertical portion with a more conventional lifting air breathing propulsion vehicle.

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    5. Re:Space flight? by Skyfire · · Score: 5, Informative

      well, if you get your rocket to reach really high speeds at a fairly high altitude inside the atmosphere, you have less altitude for the rocket to fly and less energy that needs to be expended merely to accelerate the rocket. overall this means less rocket fuel needed to reach orbit. also, because you are starting your rocket at a higher altitude you can optimise your rocket motor for a higher altitude which would increase its effiecieny. overall, a Good Thing

      Disclaimer, IANARSBIAITTBO (I am not a rocket scientist, but i am in training to become one)

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    6. Re:Space flight? by Walrus99 · · Score: 2, Informative

      As anyone who has taken high school physics should know, to get into orbit does not just require "going up." It requires reaching orbital velocity about 25,000 mph.
      physlink.com

      A scram jet could be used for part of an orbital flight from about 7 to 10 times the speed of sound. A rocket would probably be used before and after the scram jet, but there would be considerable fuel savings. Of coure once you are outside the atmosphere, a jet is useless and a rocket engine would have to be use.

      Well this is "news for nurds."

    7. Re:Space flight? by PhuCknuT · · Score: 2, Informative

      No, orbits are horizontal. When you watch a rocket launch vertically, it's only the first couple miles up that are vertical, after that they start to curve towards the orbit they are aiming for, and they start accelerating horizontally and decelerating vertically.

    8. Re:Space flight? by mikerich · · Score: 4, Interesting
      OK, so exactly how is this supposed to aid space flight efforts?
      There is no mention made of that in the article at all.

      Would this be completely unconnected with the Hypersonic Cruise Vehicle (Falcon) concept? DARPA's idea for a global hypersonic bomber that could pre-emptively bomb a country back to stone age before Letterman.

      Still, the Germans beat DARPA to this idea by about 60 years - meet the Sanger Amerika bomber... an aircraft that would fly right around the planet skipping off the atmosphere like a stone thrown across a pond.

      Best wishes,
      Mike.

    9. Re:Space flight? by AllUsernamesAreGone · · Score: 1

      But wouldn't you be using as much, perhaps more, energy overall to get something into orbit that way? Instead of just expending energy getting a rocket and its fuel into orbit, you're putting a plane and its fuel AND a rocket with fuel (even if it is less) into high altitude flight and then firing up the rocket. The energy to move the extra mass of the plane and its fuel has to be taken into account.

      Or have I missed something?

    10. Re:Space flight? by laertes · · Score: 2, Informative
      You're both wrong. Getting to orbit requires attaining the requisite altitude (maybe 100 miles) in addition to the requisite tangental (horizontal) speed. If you don't have the altitude, you'll drag on the atmosphere, and your orbit will decay. If you don't have the tangental speed, you come back down.

      BTW, this is why the X-prize will need to have a follow-up contest (Y-prize?) to really open up space: the X-prize teams are trying for altitude, and then falling right back down. They aren't achieving orbit, because they aren't adding the tangental speed.

      --

      Yes, I'm still a junky. Are you still a bitch?
    11. Re:Space flight? by Anonymous Coward · · Score: 0

      Reaction Mass.

    12. Re:Space flight? by peragrin · · Score: 1

      Well the Scram jet and regular jet should be using the same fuel source. At least I think they are?

      If you can take a DC-10 style plane, remove the rear engine and replace it with a rocket, tack on a pair of scramjets next to the regular turbo props. It would look a bit ugly, but it would cost considerbly less than the Shuttle to launch, and carry as much.

      Only little probelms like re-entry heat on the wings would need to be solved, but those are easier to deal with than getting up there to begin with.

      --
      i thought once I was found, but it was only a dream.
    13. Re:Space flight? by Gunfighter · · Score: 3, Insightful

      I have a friend who works on this project for NASA and I asked the same question. His answer was quite simple: it's not supposed to aid space flight efforts. Keep in mind the first 'A' in NASA: Aeronautics.

      I'm sure we'll eventually be able to deploy scramjet technology to boost space-bound vessels into the upper atmosphere and release them from there to continue under their own power. Given that the scramjet itself currently needs a boost, I think it will be a while before we see such a feat.

      --
      -- Stu

      /. ID under 2,000. I feel old now.
    14. Re:Space flight? by Somegeek · · Score: 1

      A rocket uses pure thrust to lift stuff and takes a LOT of energy. An airplane can mostly use its wings to support its mass and only needs a fraction of the enery, and its reusable.

      Think about the energy a wingless rocket would use to keep a 747 sized mass of cargo in the air for 5 hours, versus what a 747 manages to do it with.

      --
      And as you tread the halls of sanity, You feel so glad to be, Unable to go beyond. I have a message, From another time..
    15. Re:Space flight? by Pauli · · Score: 1

      The majority of the fuel weight in a rocket is the oxidizer, which in a jet you get for free (from the air).

    16. Re:Space flight? by AKAImBatman · · Score: 3, Informative

      Speaking of Hypersonic bombers blowing shit back to the Stone-age, you might want to look up Project Pluto. These military guys can be some real heartless bastards at times. Still, they make the target go boom, so who can complain?

    17. Re:Space flight? by Anonymous Coward · · Score: 0

      I had read a revisionist history with that tool being used. Hell of a concept. I thought a multiple-warhead ICBM was an impressive concept. This thing is just mean.

    18. Re:Space flight? by Galvatron · · Score: 1

      Of course, the Japanese realized that sometimes you don't even need airplanes to bomb your enemies. (Okay, so the only documented casualties were from a curious family that found an undetonated bomb on the ground, but it's still kind of interesting)

      --
      "The question of whether a computer can think is no more interesting than that of whether a submarine can swim" -EWD
    19. Re:Space flight? by mikerich · · Score: 1
      Dear god, the American military of the 1950s really was determined not to get to through to the 1960s.

      Thanks for that scary link, all of a sudden Dubya's NMD plan seems almost rational... ALMOST.

      Best wishes,
      Mike.

    20. Re:Space flight? by AKAImBatman · · Score: 1

      The bright side of the Pluto Project was that it and NERVA made good proof of concept projects for nuclear propulsion. Given some of the more advanced reactor designs being worked on, it's quite probable that we'll see Nuclear Thermal Rockets for space travel in the near future. As our understanding of these propulsion methods increases, we may even be able to use them to power safe atmospheric flight. :-)

    21. Re:Space flight? by DerekLyons · · Score: 1
      At the moment the only viable way to get stuff in orbit is by strapping a shitload of explosives under it.
      And after developing this complex and expensive booster, you reduce your requirements to .9 of a shitload.
    22. Re:Space flight? by WindBourne · · Score: 1

      The expensive part is getting to speed. The shuttle has 2 external solid fuel boosters and one huge tank that is used for nothing but getting a large mass up to speed. Once you are at speed, it is easy. If we can use a very large jet aircraft to provide a lift to say 30-50K with cheap jet fuel, and then use scram jets to increase speed to 5K and altitude to say 70K, once again using cheap jet fuel, then we can seperate with much small h2/o2 rockets that can take the load to space. BTW, that rocket would be fairly small in comparison to what is required today (altitude and speed is much higher).

      --
      I prefer the "u" in honour as it seems to be missing these days.
    23. Re:Space flight? by DerekLyons · · Score: 1
      well, if you get your rocket to reach really high speeds at a fairly high altitude inside the atmosphere, you have less altitude for the rocket to fly and less energy that needs to be expended merely to accelerate the rocket. overall this means less rocket fuel needed to reach orbit. also, because you are starting your rocket at a higher altitude you can optimise your rocket motor for a higher altitude which would increase its effiecieny. overall, a Good Thing
      Well, that's the theory. In practice it works somewhat less well.

      To carry less 'rocket fuel' (actually less oxidiser Mr. wannabe rocket scientist as you still need fuel for the jet stage, typically far more than the rocket it replaces), you end up carrying more fuel, more structure, more systems, etc... You replace one low altitude engine (TSTO) or one compromise engine (SSTO) with *three* different engines. Because of the lengthy heating during the supersonic phase, you increase your cooling and TPS requirements. This goes on, but these are the biggies.

      The theory is powerfully seductive, but for the forseeable future the disadvantages are massive, and barring major breakthroughs in aerodynamics and thermodynamics, the numbers simply don't work out.

    24. Re:Space flight? by visgoth · · Score: 1
      I heard a nice, simple way to describe achieving orbit in the anime movie Wings of Honneamise.
      Its been a while, but here it goes:

      You take a rock and throw it. It follows a ballistic trajectory, arcing upward, and then falling back to earth. Throw it harder, and it goes higher and farther. If you throw it hard enough, the rock's "impact point" is out beyond the curvature of the earth, and it ends up "falling" forever.

      --
      My patience is infinite, my time is not.
    25. Re:Space flight? by mikerich · · Score: 1
      Have you read 'Project Orion: The Atomic Spaceship 1957-1965' by George Dyson? (ISBN 0140277323 Penguin Press Science) It's a complete history of Project Orion and why it ultimately failed.

      There is also an excellent BBC4 documentary called 'By Atom Bomb to the Stars' which has an enormous amount of colour footage of the Orion tests - well worth watching out for.

      Best wishes,
      Mike.

    26. Re:Space flight? by mcflaherty · · Score: 1

      True, but that is for a low impulse projectile launch. We don't do it that way. The rock analogy describes what is needed to catapult an object into orbit. We use force over time to launch a rocket into orbit, since the engine is firing for the duration of the ascent into orbit.

      Just picking nits.

      --
      -- I am become sig, destroyer of posts.
    27. Re:Space flight? by AKAImBatman · · Score: 1

      I haven't read the book, but I am well aware of the concept. The Orion is interesting because it gets *more* efficient as it gets larger. This is in direct opposition to all other forms of propulsion. Unfortunately, the very concept is a bit scary to most people. Thus you can expect that NERVA, Gas Core Nuclear Rockets, and Nuclear Salt Water Rockets will be developed long before we start seeing 8 million ton Orions carting cities around the Solar System.

    28. Re:Space flight? by Dyolf+Knip · · Score: 1
      A scram jet could be used for part of an orbital flight from about 7 to 10 times the speed of sound

      Why only to mach 10? Scramjets have no theoretical upper limit on speed, only lack of air would force the switch to a vacuum-capable system. Orbital velocity is in the mach 20-25 range.

      --
      Dyolf Knip
    29. Re:Space flight? by sootman · · Score: 1

      The "Sanger Amerika bomber," eh? Hmm, I wonder what the Germans designed it for. I guess I'd better click that link and find out. :-)

      Seriously, thanks for the link... but that's just the funniest (in its way) name for a plane I've ever heard.

      --
      Dear Slashdot: next time you want to mess with the site, add a rich-text editor for comments.
    30. Re:Space flight? by Anonymous Coward · · Score: 0

      "could pre-emptively bomb a country back to stone age before Letterman"

      Since when has Letterman bombed...oh, wait, never mind.

  8. Re:Military - yuck by bpowell423 · · Score: 5, Informative

    They're not (directly) working on cruise missiles, although the tech could be used for that. They're trying to invent a cheaper way to get to orbit. This is just a test bed to figure out the scram jet. The plan is for a standard jet engine to get you to supersonic speeds, the scram jet to get you to hypersonic speeds and the edge of the atmosphere. Once you're going, say, Mach 7 and most of the atmosphere is below you, you fire the rocket engine to get you the rest of the way to orbit. This approach wouldn't require the rocket to carry as much oxydizer, thus less weight, less cost.

  9. Re:Sonic-boom? by youlogee · · Score: 2, Insightful

    Aren't there laws governing mach speeds over populated areas?

  10. Re:Sonic-boom? by PhuCknuT · · Score: 2, Informative

    They're testing it over the pacific ocean.

  11. Re:Sonic-boom? by sploxx · · Score: 4, Informative

    Yes, you would hear the sonic boom of the test flight. (If you are close enough to hear it at all, of course).
    At supersonic speeds, the edge of the soundwaves that are produced by an object is a cone in the object's inertial frame. Regardless of the speed. The speed only changes the angle of this cone..

  12. ROCKET MAN by Space_Soldier · · Score: 2, Funny

    Let us strap a human to it and sing "The Rocket Man"!

    1. Re:ROCKET MAN by Patrik_AKA_RedX · · Score: 1

      Do we get to vote about who gets picked as a volunteer?

    2. Re:ROCKET MAN by Anonymous Coward · · Score: 0

      Poll: Who should ride the first hypersonic engine?

      ( ) Darl McBride
      ( ) Bill Gates
      ( ) George Bush

      Choose wisely :)

    3. Re:ROCKET MAN by Anonymous Coward · · Score: 0

      Linus Torvalds, just to make sure the thing can run LINUX.

  13. What are the advantages of continual reentry? by glrotate · · Score: 1

    Just curious?

    1. Re:What are the advantages of continual reentry? by AllUsernamesAreGone · · Score: 2, Funny

      Depends what you're reentering I suppose...

    2. Re:What are the advantages of continual reentry? by pe1rxq · · Score: 3, Funny

      You don't have to bring your own heater?

      Jeroen

      --
      Secure messaging: http://quickmsg.vreeken.net/
  14. Why? by Wind_Walker · · Score: 4, Insightful
    Forgive me for being so stupid, but what's the point of making a craft that can go Mach 7? The article claims travel benefits, going from New York to London in 2 hours. But honestly, travelling that fast, if anything went wrong you're toast. Turn a little bit to the wrong side, and suddenly you've lost a wing from the shock. No commercial airliner would stand for that.

    The only possible use I can think of is hyper-range weapons. Ground-controlled planes armed with lethal cargo (nuclear or not) could be flown around the globe faster than any ICBM, and guided with better accuracy.

    I'm all for "Science for Science's sake" but I think this is worthless for any practical purposes.

    1. Re:Why? by russler · · Score: 0

      I hear what you are saying. I had your same type of reaction to the previous story about robotic cars racing through the desert. I mean, come on! How obvious is it that we would like to be able to send unmanned recon/payload delivery vehicles through the desert in Iraq or wherever in future wars? What other common practical uses would such vehicles have? I'm sure there are some, but I bet they are ancillary to the main objective stated above.

      Didn't we all learn our lesson from the movie Real Genius? Please don't tell me that Val Kilmer's message fell on deaf ears!

    2. Re:Why? by random_rabbit · · Score: 1
      So you could control these "hyper-range" weapons from the ground, and with better accuracy than "any" ICBM. But you say this is not good enough for a commercial airliner?

      In a modern aerospace engine the fan blades are operating at *above* their melting temperature. If something goes wrong there, you are almost certainly toast, yet you wouldn't think twice about crossing the Atlantic at 30,000ft pushed along by several million moving metal parts.

      I'd probably take my chances with the scramjet (but I'd let you go first)

    3. Re:Why? by Hektor_Troy · · Score: 5, Insightful

      You know, if anything goes wrong with a regular transatlantic airliner while it's over the North Atlantic, I think it's fairly safe to say you're toast as well.

      Granted, the nice stewardesses tell you that you can use your seat cushion as a floatation device, but two things strike me in that scenario:

      1) What are the chances of surviving initial impact into the ocean when the plane is in a 600 mile an hour vertical dive
      2) Do I really want to float around in the North Atlantic for several days, clinging to a pillow full of beer farts

      And yet, we still do this on a regular basis because guess what - it's actually fairly safe. As will hypersonic travel be, once we get around to getting better materials etc.

      In the 1700's people really believed that if you traveld faster than a horse, you'd die from the shock and that it would be impossible to build a heavier than air flying machine. Guess what - they were wrong, and you will be as well. Some day (if we don't manage to blow up ourselves first).

      --
      We do not live in the 21st century. We live in the 20 second century.
    4. Re:Why? by meringuoid · · Score: 4, Insightful
      The article claims travel benefits, going from New York to London in 2 hours.

      This is the most tragic thing I've ever read on Slashdot. We USED TO be able to go from New York to London in two hours. It was sixties technology, hacked together by two dying empires looking for some prestige. Now we're looking at a little dart fired off a B-52 and dreaming of flying that fast again someday... What the hell went wrong?

      --
      Real Daleks don't climb stairs - they level the building.
    5. Re:Why? by lfourrier · · Score: 3, Interesting

      We USED TO be able to go from New York to London in two hours. What the hell went wrong?

      1) US refusing Concorde at supersonic speed over US territory.
      2) Price of petrol
      3) 2 hours of transatlantic flight, 2 hours to go to the initial airport, 2 hours to go from the final airport...
      4) Looking back at this, it was somewhat an ecological catastrophe

      How will all those factors be taken into account by the sdcramjet developers?

    6. Re:Why? by Anonymous Coward · · Score: 1, Insightful

      what's the point of making a SUV that can go over 80MPH or have an engine bigger than a 4 CYL?

      what's the point of making a supersonic passenger jet?

      what's the point of driving around in a circle for 200 laps?

      what's the point of the olympics?

      we do things as humans because we can... it's insane to send people underwater into deep waters... but we go there to look at the wierd creatures...

    7. Re:Why? by meringuoid · · Score: 2, Interesting
      Mmm... Maybe I can forgive the US banning Concorde overland, given the noise it made; I was in Reading last summer, shortly before Concorde was grounded, and heard one _hell_ of a roar filling the whole place. Looked up and there it was, coming up out of Heathrow. There must have been a hundred rock bands there and nothing came close for sheer decibels. Bloody beautiful, though. Just the shape of it stinks of speed.

      The other killer was probably that it couldn't quite carry the fuel to cross the Pacific. That cut it off from LA - Tokyo, which cut it off from a big moneyspinner...

      --
      Real Daleks don't climb stairs - they level the building.
    8. Re:Why? by gowen · · Score: 1
      What are the chances of surviving initial impact into the ocean when the plane is in a 600 mile an hour vertical dive
      Planes rarely hit the sea in 600mph vertical dives, at least not intact. If the planes still in one piece on impact, its probably because the pilot is ditching, and your chance of getting out isn't bad.
      If there's catastrophic failure at altitude, you're screwed.Do I really want to float around in the North Atlantic for several days, clinging to a pillow full of beer farts
      It beats drowning.
      --
      Athletic Scholarships to universities make as much sense as academic scholarships to sports teams.
    9. Re:Why? by thedillybar · · Score: 1
      But honestly, travelling that fast, if anything went wrong you're toast. Turn a little bit to the wrong side, and suddenly you've lost a wing from the shock.

      You can bet someone said the same thing when the Wright Brothers put a plane in the air. They're testing this; they're not putting it into production. We still have a lot to learn, and this is a big step in the right direction.

      Good luck to the fine men and women at NASA. We'll be watching.

    10. Re:Why? by Anonymous Coward · · Score: 0

      Apparently, no one really wanted to go from New York to London in two hours.

    11. Re:Why? by notbob · · Score: 0

      How does freezing to death and suffering for days beat drowning in under 3 minutes?

      It'd be pure torture to be stuck out there.

      A rescue team... maybe if you're not too far out, but anything past hellicopter range and you're waiting on a friggin clipper to get there.

      So you'd be SOL.

      Or maybe they'd land a neat sea plane for you... just remember to duck ;)

    12. Re:Why? by the+eric+conspiracy · · Score: 1

      But honestly, travelling that fast, if anything went wrong you're toast.

      Isn't that pretty much true in any tin can moving at supersonic speeds powered by exploding fuel? The Concorde cruises just fine at Mach 2, the SR-71 at Mach 3.3+.

    13. Re:Why? by Anonymous Coward · · Score: 0

      What? An ICBM takes 30 minutes to get from the USA to Russia with GPS-guided accuracy. Do you really think somebody's going to bother using a scramjet to deliver nukes?

      Of course, since the military can afford high R&D expenses and higher failure rates, the technology will likely find its way to military uses before civilian ones. But that just tends to be the way it is with most technologies.

      aQazaQa

    14. Re:Why? by gowen · · Score: 1
      How does freezing to death and suffering for days beat drowning in under 3 minutes?
      Because, if the worst comes to the worst you can do the DiCaprio, and choose to let go.
      --
      Athletic Scholarships to universities make as much sense as academic scholarships to sports teams.
    15. Re:Why? by Anonymous Coward · · Score: 0

      Not quite true. Granted a major structural failure (like having a wing rip off) at 35,000 feet is the kiss of death, for sure. However, there are many, many minor structural failures that can be survived at subsonic speeds.

      Here is a good example, ever see what a bird strike looks like on an aircraft? You probably have, since they mostly make it back to earth in one piece to be photographed. How much bigger was the hole made on the shuttle wing? Not much, from what the NASA test showed, of course there isn't enough of the shuttle left to actually check. The instant the shuttle started to yaw, it was toast. At the hyper velocities that are being travelled, the structures can not take the load shift, and they tear themselves apart. Same case here. Little damage at 600 mph is bad, the same damage at 5000 mph is a fireball.

    16. Re:Why? by arabung · · Score: 1

      When you're going 5000 mph, the likelihood for something going wrong shoots up. The likelihood for something going wrong killing everybody stays the same: really damn high.

    17. Re:Why? by Anonymous Coward · · Score: 0

      Dude, good post, but really, you should acknowledge where you ripped the quotes: to wit, George Carlin's performance on ``Airport Announcements''

    18. Re:Why? by Beryllium+Sphere(tm) · · Score: 1

      One metric ton of fuel per passenger, for one thing.

      Lack of military spinoff technology may be part of the reason we're not flying at Mach 7. By the time of the XB-70, the military was already seeing the end of the higher-faster approach and concentrating more on treetop-level flight and stealth.

    19. Re:Why? by mccrew · · Score: 1
      What the hell went wrong?

      Simple economics. In order to travel at Mach 2, the airplane is significantly heavier, mechanically more complicated, less fuel efficient, and overall more expensive to operate. A supersonic aircraft will always be more expensive to operate with respect to a subsonic aircraft. I couldn't believe that Boeing was even seriously considering their "Sonic Cruiser" aircraft for as long as they did before finally acknowledging the obvious. Given these realities, there just isn't the demand for it. Only rich fat-cats and celebrities could afford the $10,000 fare. Regular folks are willing to pay $500 and put up with an 8 hour flight.

      Aerospaciale (sp?), the maker of the Concorde, never made a dime on the 16 or so Concordes it built.

      --
      Hey, Windows users, there is no such thing as "forward" slash, there is only slash and backslash.
    20. Re:Why? by mnemonic_ · · Score: 1

      God damn you have as stupid an attitude on scientific research as Bush.

    21. Re:Why? by robbymet · · Score: 1

      If you can make a plane go Mach 7, you can use it as a first stage in a two-stage-to-orbit reusable launch vehicle. Remember that a plane traveling at Mach 7 has a ridiculous amount of kinetic energy, which can be converted to potential energy (altitude) by performing a pull-up maneuver. This allows the rocket (second stage) to be released at an altitude and velocity high enough that only one rocket stage is required to lift a satellite into orbit. Because the rocket can be a single-stage now, it can be designed to return to Earth and be reused, drastically reducing launch costs and making launch from a range unnecessary (sufficient redundancy can be built into the plane to make it safe, plus you don't have to worry about multiple rocket stages re-entering the atmosphere. Traveling at this speed creates immense levels of heat (temperature increases with the square of the mach number, i.e 4x higher temp at Mach 4 than Mach 2 [16/4], 25x higher temp at Mach 7 than Mach 2 [49/4]!). Luckily, this is only true in the atmosphere, when air molecules are being decelarated from Mach 7 to 0 on the plane's surface. If a plane can go fast enough to leave the atmosphere, it can significantly reduce its heat load. It can then periodically trade its potential energy for kinetic energy and rapidly transverse the globe exo-atmospherically (this is the concept the Germans came up referred to elsewhere). The plane heats up again as it re-enters, but unless it continues to accelerate in space, it will re-enter at a velocity slower than it's exit velocity, so the worst heating case is on exit, which it already survived! The costs of the initial build for such planes is high because the materials that can withstand these speeds are so expensive (Inconel, etc) but the ability to reuse the entire vehicle significantly reduces launch costs. Sadly, the space industry is government subsidized and competition averse, so there is little motivation to change the status quo. In government contracts, the less expensive your product, the less money you make.

  15. Second Post of X-43A Article Today by gravelpup · · Score: 2, Funny
    --

    Things are more like they are now than they ever were before.

    1. Re:Second Post of X-43A Article Today by Anonymous Coward · · Score: 0

      Come on! This at least deserves +5 Informative at the top of the thread. People should know that they are reading the same thing they read 23 hours ago! To let them do it and not tell them is a crime! Mod parent up as Informative, mod this up as funny.

    2. Re:Second Post of X-43A Article Today by Anonymous Coward · · Score: 0
    3. Re:Second Post of X-43A Article Today by Anonymous Coward · · Score: 0
      from the dupes-of-dupes dept.

      didn't somebody just say that? :^)

  16. Ok, so Jet Propulsion Lab. does space.... by Zaiff+Urgulbunger · · Score: 5, Funny

    Slight off-topic, but why do I have to go to Jet Propulsion Laboratory to find out about the Mars rovers, and then I have to go to National Aeronautics and Space Administration to find out about fancy new jet engines?!

    Is it a cunning plan to out-fox those secret stealing ruskies?

    1. Re:Ok, so Jet Propulsion Lab. does space.... by MajorDick · · Score: 1

      I dono, but back in 94 maybe early 95 or so , I was surfing around WPAFB for info on pulsejet engine, which are a hobby of mine. I also saw something interesting done in html and though hmm howd they do that ? Well of course I wiewd the source and found a couple of URL's commented out. Interesting I thought , what behind those... The answer The Advanced Power Directorate, after about 10 minutes of surfing I realized I was in a very classified extranet for the big engine manufacturers , really kinda scared me , I was for weeks just waiting for a knock on the door.

    2. Re:Ok, so Jet Propulsion Lab. does space.... by demachina · · Score: 3, Interesting


      http://www.jpl.nasa.gov/about_JPL/jpl101.pdf

      The way this reads is there was a race after sputnik to launch the first U.S. satellite. The JPL/Army Orbiter lost out to the Navy's Vangaurd. Vangaurd exploded on the pad and JPL revived Orbiter but they focused on the satellite more than the rocket. They turned their focus to payloads from them on, and NASA came in to being in 1958 and assumed hegemony over rocket R&D elsewhere. As for not changing the name I assume it was:

      A. Sentimental, since the early JPL had a rich history
      B. To cheap to print new stationary and change signs
      C. Geeks busy doing geek stuff and didn't get around to it

      The original founders are a colorful group. Theodore Von Karman was the leader and guding force.

      Jack Parsons, leading chemist, who was part of an "esoteric order" rumored to be fond of drugs and orgies.

      Tsien Hsue-shen is considered to be the father of the Chinese missile and space program. He was held hostage in the U.S. for a number of years during the red scare when he wanted to return home to China. He was released by Eisenhower as part of prisoner exchanges in Korea.

      --
      @de_machina
    3. Re:Ok, so Jet Propulsion Lab. does space.... by Anonymous Coward · · Score: 0

      B. To cheap to print new stationary and change signs

      It's been half a century. Talk about procrastination!

  17. Inertia? by baudilus · · Score: 1

    I hope they took the time to invent inertial dampeners like they have on Star Trek. I'd hate to see what mach-7 does to the pilot...

    1. Re:Inertia? by Marbleless · · Score: 1

      It's not speed that kills, it's acceleration. Mach 7 is perfectly safe, assuming your craft stays together. Compare it to jumping off a building, the stop at the bottom is the nasty moment.

      --
      --I thought I was wrong once, but I was mistaken.
    2. Re:Inertia? by Patrik_AKA_RedX · · Score: 3, Informative

      Mach 7 is velocity. The only thing you could feel is the acceleration. But flying at mach 7 would feel the same as flying at mach 0. (Excluding external influences). You would only need inertial dampeners when the acceleration would be high.

      Inertial damperners aren't exactly that hard to build. Consider that the inertial force is proportional to both mass and acceleration, the only thing you would need to acomplish is reducing mass to near zero. I'll leave that as an exercice for the reader.

    3. Re:Inertia? by Anonymous Coward · · Score: 0

      Acceleration is the issue, not speed. The space shuttle gets up to mach 25 to leave earth (BBC article).

    4. Re:Inertia? by MenTaLguY · · Score: 1

      You would only need inertial dampeners when the acceleration would be high.

      Like when turning.

      Actually if you don't mind making reeeeeeealllly slow turns it's not too bad, but you do have to be very careful at those speeds.

      --

      DNA just wants to be free...
    5. Re:Inertia? by StarfishOne · · Score: 0

      [quote]
      Inertial damperners aren't exactly that hard to build. Consider that the inertial force is proportional to both mass and acceleration, the only thing you would need to acomplish is reducing mass to near zero. I'll leave that as an exercice for the reader.[/quote]

      My attempt to find a solution:

      You say it's important to reduce mass to near zero. Soo.. what about ditching the pilot?

      ;)

    6. Re:Inertia? by Patrik_AKA_RedX · · Score: 1

      I don't think that's much of a problem. At least not for transatlantic flights. The pilot could take of at a slow speed, get to the right altitude and heading and then fly full speed, until he crossed the ocean. Slow down and land.

      But I doubt such a plane could handle even slow turns at mach 7. Turning would make the plane slightly less aerodynamic. At such high speed this could cause severe stress on the plane.
      but I'm not an aircraft engineer.

    7. Re:Inertia? by Anonymous Coward · · Score: 0

      Mach 7 is speed (a 1-dimensional quantity). Velocity implied a multidimensional *vector* (direction & magnitude). Mach is a measure of speed of sound, which is dumb. Use m/s, mph, km/h, km/s... something that is a real unit of measurement. Btw, NASA was mandated to go *all Metric (IU)*. HEHHE... Metric rules (and I live in the US, too). pints/quarts/gallons... i can never figure that shit out. Litres (Liters) makes sense. m/km make sense.

    8. Re:Inertia? by Anonymous Coward · · Score: 0

      "I'll leave that as an exercice for the reader."

      Well, the gravetic deck plates I use already compensate for acceleration. What are these "inertial dampers" you speak of?

  18. Did you forget a non? by Anonymous Coward · · Score: 0

    in your sig?

    1. Re:Did you forget a non? by AllUsernamesAreGone · · Score: 1

      Nope, the lack of non makes it far more accurate than the original.

  19. Re:Sonic-boom? by T'hain+Esh+Kelch · · Score: 1

    I am more curious as to how loud it'll sound... 7 times the normal boom? Havent read much about mach-speeds...

  20. Complexity not always a good thing by Analogy+Man · · Score: 4, Interesting
    That kind of craft would probably employ multiple propulsion systems including a turbo-jet to reach supersonic speeds, scramjets to take the vessel to the edge of the atmosphere and then chemical rockets to enter the void of space.

    The danger here is that the darn thing will carry all of these systems and have no capacity left over for payload. I recall the Boeing SST back in the late 60's early 70's was based on a swing wing concept. The scale of the mechanical systems to swing the large wing faced them with a difficult choice of a swing wing or passengers...but not both.

    In the physics world one has a sense that they are on to something when the math becomes elegant and simple...I think in the "no moving parts" nature of the scram jet are appealing...a turbofan/scram/rocket combination is not

    --
    When the people fear their government, there is tyranny; when the government fears the people, there is liberty.
    1. Re:Complexity not always a good thing by Keick · · Score: 1

      Possibly, but work is underway to create a dual-mode, and even tri-mode hypersonic engine. The dual-mode will be a scramjet/solid-fuel engine already under development by the air-force. The during scramjet operation the cowl flaps are open to mix oxygen with cracked JP7, then ignited. Once your far enough out, the cowl flap will close and the engine, or engine bypass, will be used as a solid fuel booster.

      The weight of a scramjet engine is much greater than the weight of the oxygen that would normally have to be caried.

      The tri-mode engine, still under "consideration", would be to take a standard jet turbine, and surround it on the outside (bypass) with the scramjet.

    2. Re:Complexity not always a good thing by Veles · · Score: 1

      Actually, in the Deutschen Museum there is a concept demonstration of such an engine. (By Daimler-Chrysler)

      Basically, the same chambers are used for the three stages, and blockers are used to block the air entry and the turbojet when required. (The motor changes shape)

      Of course, its heavier than a single engine design, but not that much heavier than the heaviest single design would be. So not that much heavier than Turbo-Jet ...

      --
      I will find later.
    3. Re:Complexity not always a good thing by gargleblast · · Score: 1

      The danger here is that the darn thing will carry all of these systems and have no capacity left over for payload.

      Most rocket-only launch systems are multi-stage, most notably the Saturn V but also the Shuttle.

      Part of the reason is that bell nozzle rocket engines are most efficient only within a limited altitude range. One viable SSTO (Single Stage To Orbit) engine is the aerospike, however NASA canceled Lockheed Martin's aerospike project, the X-33, a few years ago. There are other such projects.

      But back to scramjets - a launch system including jet stages might still require multiple engines, but would likely carry less oxidant and fuel.

  21. Physics Question by Pirogoeth · · Score: 2, Interesting

    I've mostly forgotten almost all my physics, so could someone please answer a question for me?

    Why do you need to be going 25,000 mph to get away from the Earth?

    I can jump into the air and get away from the Earth, for a couple seconds anyway, and I'm not going nearly that fast.

    I thought as you got farther away from a body, the gravitational pull decreases using some inverse-square rule.

    As long as you can get airborne and are able to keep moving upwards, why doesn't it become easier to keep going the higher your altitude?

    --
    Happiness is like peeing yourself. Everybody can see it but only you can feel its warmth.
    1. Re:Physics Question by kidgenius · · Score: 1

      You're right, gravity is very weak, but it requires enormousamounts of energy to keep movin upwards as you said. Notice, when you jump, you are able to get only aout 6-12 inches off the ground. Now consider that you need to get about 100 miles off the ground to get into orbit, andyou run into the problem of getting enough energy to do so. You also run into problems about a propulsion system that doesn't use air the entire flight, b/c once you get into space, you wont have any air.

    2. Re:Physics Question by ch-chuck · · Score: 1

      yeahbut, I also wondered about the 'escape velocity' thing: say you had enough energy onboard and no need for external oxygen, couldn't a vehicle just fly up at, say, a steady 1000mph and get away from the earth's gravity well? Or does 'escape velocity' have to do with orbital mechanics?

      --
      try { do() || do_not(); } catch (JediException err) { yoda(err); }
    3. Re:Physics Question by ianfs · · Score: 1

      It has an awful lot to do with the fact the Earth is an incredibly large body with a very large gravitational field. You can escape but only for a second.

      Also you way an incredibly small fraction of what a space craft ways.

      --
      "Terminate?"
      "Terminate... with extreme prejudice"
    4. Re:Physics Question by Anonymous Coward · · Score: 0

      The problem is staying up once you're there. If you jump up, you don't manage to do this. One way to stay up is to acheive orbital velocity. That way, you are actually continually falling back down to Earth, but you manage to keep going sideways fast enough so that the Earth's pull is just strong enough to drag your path into a loop around the Earth. Orbital velocity for interesting heights is about 25,000mph.

    5. Re:Physics Question by GuyFawkes · · Score: 4, Informative


      In real layman's terms......

      weigh yourself at sea level
      then weigh yourself again at the top of mount everest

      unless you are using *really* accurate scales the two readings will be the same.

      now go back to both locations where you weighed yourself and measure the atmospheric pressure in both places.

      unlike your weight you'll find the pressure is about a third of what it was at sea level.

      pressure in a known and unchanged mixture of gases is another way of counting how many molecules of gas there are in any given cubic meter, or to put it another way, the mass of a given cubic metre.

      so your aerofoil (wing) at the top of everest has about one third of the mass of gas to ride on as it does at sea level.... if your aerofoil is a fixed wing then you can always travel three times as fast (hence needing a scramjet) whereas if your aerofoil is a rotary wing (helicopter) you come up against a hard limit when the out edges of the rotors approach the speed of sound, hence the much lower maximum altitude ever recorded in a helicopter as opposed to a swing wing.

      NB all of the above is really really simplified and therefore full of errors to a physicist / aerodynamics / bernoulli / etc etc etc

      HTH etc

      --
      http://slashdot.org/~GuyFawkes/journal
    6. Re:Physics Question by kidgenius · · Score: 1

      Absolutely, keep a constant velocity and you will do it. But you ever notice what happens when you throw a ball in the air? It acelerates downwards, slows its ascent, and comes back down to earth. So to retain this constant velocity requires a constant force downwards. To keep a constant force is very difficult. Just as gravity decreases with the inverse square, your energy output will be climbing by a squared value of some kind. (no time to do the math right now)

    7. Re:Physics Question by Anonymous Coward · · Score: 0

      Perhaps what you need is a way to throw yourself at the ground and miss.

    8. Re:Physics Question by GuyFawkes · · Score: 1


      you could IN THEORY get into space by climbing at one centimetre a week, but you'd need reaction motors capable of exhausting reaction mass at an appreciable proportion of the speed of light, and I for one would not like you lighting up such a motor in the atmosphere of any planet I was on.

      escape velocity is easy enough, think small weight tied to piece of string, swing weight around on piece of string so string is always taut.

      if breaking strain of piece of string equates to gravity and therefore escape velocity then when the string breaks (when the weight is travelling fast enough) the weight will fly off

      note that firing something at escape velocity at sea level on earth isn't enough, air resistance will slow it down VERY fast, think of bullets from high velocity rifles.

      --
      http://slashdot.org/~GuyFawkes/journal
    9. Re:Physics Question by eutychus_awakes · · Score: 3, Interesting

      Indeed, all you would need to do to lift a 5-pound object above the Earth's atmosphere would be to supply an engine which can provide 5.1-pounds of thrust for a VERY long time. Trouble is, when you shut the engine off (or ran out of fuel) you would just fall back to Earth unless you somehow managed to achieve orbital trajectory and velocity. You do the math on how much fuel that would take (a lot - more than you could ever possibly carry). Without escape velocity, the Earth has you - forever! It doesn't matter if you travel as far as the Sun - unless you have escape velocity with respect to the Earth, you're going home. Gaining escape velocity with respect to the Sun is another problem. . .

      For the more technically-mided folks out there, the idea is to achieve higher kinetic energy than you currently posess in gravitational potential energy with respect to the Earth. The farther away you go from Earth, the higher your potential energy is (the longer you "fall" to get back to our planet) - so you have to integrate from the surface of the Earth to infinity altitude to determine the total energy you would need to escape the Earth's gravity. The masses cancel each other out - and you're left with approximately 25,000 mph for your escape velocity.

      Be nice to me - I haven't had my coffee yet today.

      --
      This sig is a test. If this had been an actual sig, you would be reading something quite a bit wittier than this now.
    10. Re:Physics Question by kidgenius · · Score: 1

      Also, you need to apply a force greater than your mass. If you wegih a couple hundred tons, you have to supply a constant force of a couple hundred tons. The energy expelled to do this is an insane amount, and that's why you have these huge rockets with massive amounts of propellant.

    11. Re:Physics Question by Glock27 · · Score: 3, Interesting
      Without escape velocity, the Earth has you - forever! It doesn't matter if you travel as far as the Sun - unless you have escape velocity with respect to the Earth, you're going home. Gaining escape velocity with respect to the Sun is another problem. . .

      Your post was mostly right except for this part. IF (yes that's a big if;) you had sufficient fuel, as you pointed out above, you could fly at 1 MPH to the Moon. And, once you reach the crossover point (where the Moon's gravitational field is stronger than the Earth's), you have escaped in the sense of escape velocity. You won't be going back home.

      Escape velocity is only relevant for ballistic (unpowered) objects.

      Given our current propulsion systems, all of our spacecraft are essentially ballistic except for the new ion powered ones - and those are very low thrust. Practical antimatter propulsion would make things a lot more interesting! :-)

      --
      Galileo: "The Earth revolves around the Sun!"
      Score: -1 100% Flamebait
    12. Re:Physics Question by Anonymous Coward · · Score: 0

      "exhausting reaction mass at an appreciable proportion of the speed of light"

      At one centimetre a week, which is essentially hovering? Did you mean using the "standard" amount of reaction mass?

    13. Re:Physics Question by SamSim · · Score: 1

      The phrase "able to keep moving upwards" is the most important in that sentence. Aircraft are able to fly because they move through air. The higher you go, the less air there is, and the harder it is for a conventional aircraft to remain airborne. At that point you start to need a more traditional wingless rocket booster a la NASA. So far nobody has successfully combined the two technologies but I daresay a lot of people are working on it since it could prove staggeringly useful for cheaply boosting stuff into orbit.

    14. Re:Physics Question by GuyFawkes · · Score: 1

      yes, 1 ton of reaction mass is plenty for 10 tons of payload, IF you can eject the reaction mass at say 0.99 c

      (where c = 186,000 miles per second)

      --
      http://slashdot.org/~GuyFawkes/journal
    15. Re:Physics Question by eutychus_awakes · · Score: 1

      True about the Moon and all, but the easiest way to explain a term like escape velocity is to keep things simple - the classic 2-body problem. (Incidently, I only used the Sun as a distance reference.) Once you shut your engines off in a 2-body framespace, you are a ballistic object. Your possible trajectories are then either parabolic (moving away from the Earth, and falling back to the surface), elliptical (orbiting, counting a circle as a "perfect" ellipse), or hyperbolic (having achieved escape velocity, curving for awhile, but then proceeding on a straight, unimpeded line away from the Earth).

      It just so happens that ballistic trajectories are the most efficient way to move from point A to point B in terms of fuel / mass. Currently, that is.

      --
      This sig is a test. If this had been an actual sig, you would be reading something quite a bit wittier than this now.
    16. Re:Physics Question by Have+Blue · · Score: 1

      You are technically correct about gravity, but what you should be comparing distances to is the radius of the Earth- 6000km. Going from sea level to Everest is miniscule compared to this. Even going up to the edge of the atmosphere (a few hundred km at most) is not much proportional change. You're have to go out several thousand km before the decrease became noticable, and *way* farther than that before Earth's gravity can be ignored.

    17. Re:Physics Question by Anonymous Coward · · Score: 0

      Your under the mistaken belief that things in space are weightless. They are not. They seem weightless since they are in a constant state of freefall circling the earth. Rockets may launch upward initially but most of the distance they cover is horizontal. If you were to launch a rocket perfectly vertically you may be able to escape the atmosphere but you would just fall back to earth once your fuel runs out. Think of it this way. You hold a ball 1m off the ground and it falls. You hold a ball 1km off the ground and it falls. you hold a ball 1000km off the ground and it will still fall. What keeps objects in orbit is thier velocity. They fall down to earth at a rate equal to the rate at which the earth curves away from them so they remain at a constant distance from the ground. The distance off the gorund does not matter (ie this could be acomplished just 1m off the ground if the earth were perfectly round and had no atmosphere.)

    18. Re:Physics Question by eingram · · Score: 1

      weigh yourself at sea level
      then weigh yourself again at the top of mount everest

      unless you are using *really* accurate scales the two readings will be the same.

      now go back to both locations where you weighed yourself and measure the atmospheric pressure in both places.

      No, no, no! Weigh yourself at sealevel then take the atmospheric pressure at sealevel. Then go to the mountains, weigh yourself, and take the atmospheric pressure while you're up there. Too much work/travel the other way. ;)
    19. Re:Physics Question by mccrew · · Score: 2, Informative
      so your aerofoil (wing) at the top of everest has about one third of the mass of gas to ride on as it does at sea level.... if your aerofoil is a fixed wing then you can always travel three times as fast (hence needing a scramjet)

      Assuming the same coffficient of lift, Cl, in order to generate the same amount of lift you would have to have the same "dynamic pressure" (to borrow a Boeing term), then (from Bernoulli equation)

      • 0.5 * densitySL * velocitySL**2 = 0.5 * densityEverest * velocityEverest**2

      If the ratio of densitySL/densityEverest is 1/3, then solving for velocityEverest:
      • velocityEverest = sqrt(3) * velocitySL

      or approximately 1.73 times the speed at sea level.

      --
      Hey, Windows users, there is no such thing as "forward" slash, there is only slash and backslash.
    20. Re:Physics Question by Anonymous Coward · · Score: 0

      i wonder what an anti matter explosion would look like

  22. Circumference by rwiedower · · Score: 4, Interesting

    But if the earth's circumference is around 25,000 miles, and this jet can go 5,000 miles an hour, that would mean it would take only 2.5 hours to get from any location to any other.

    Okay, if it only takes 2.5 hours at top speed to go anywhere on the planet, how much time is spent accelerating and decelerating versus actually flying at Mach 10? And how much fuel are you burning in the process? I remember working at LaRC when they were just starting to test scramjets and I still think the science is good for orbit, but bad for commercial applications.

    1. Re:Circumference by Anonymous Coward · · Score: 2, Insightful
      rwiedower: But if the earth's circumference is around 25,000 miles, and this jet can go 5,000 miles an hour, that would mean it would take only 2.5 hours to get from any location to any other...
      BZZTT Wrong: Earth circumference is 25K miles at GROUND LEVEL. Are you trying to skim the surface? If you just go up 1 mile then you will find the circumference is ~31K etc. etc.
    2. Re:Circumference by EulerX07 · · Score: 1

      Actually, if the circumference is 25 000 miles you can reach any point of the globe in 12 500 miles assuming you use a straight line to get to it.

    3. Re:Circumference by tiled_rainbows · · Score: 1

      Uh, yeah, that's why he said it would take two and a half hours. The distance covered in two and a half hours at 5,000 mph is left as an excercise for the reader.

    4. Re:Circumference by lommer · · Score: 3, Informative

      um no, some very simple math indicates that if you go up 1 mile, the circumference is only about 6 miles longer. You have a point, but it's not nearly as big an effect (especially considering thinner air -> efficiency at high altitudes).

    5. Re:Circumference by tiled_rainbows · · Score: 4, Informative

      31,000 miles?

      How do you work that out? a circumference of 25,000 miles gives us a radius of 3,978 miles. Go a mile up, and the effective radius is 3,979 miles, which gives us a circumference of...

      25,006 miles. Not much of a difference.

    6. Re:Circumference by Anonymous Coward · · Score: 0

      circum. = r*pi*2

    7. Re:Circumference by Spamalope · · Score: 2, Funny

      Okay, if it only takes 2.5 hours at top speed to go anywhere on the planet...

      If the security check ins take any longer we'll need speeds like this to get anywhere. Besides, just think how fast all of your luggage can be lost and sent to Burma!

    8. Re:Circumference by Anonymous Coward · · Score: 0

      That would be nice, as I'm travelling to Burma. I think with all the unrest there, it's the only place that one can remain under the authorities' radar.

    9. Re:Circumference by stud9920 · · Score: 1

      Your multiplications by and division by 2 pi were sooo necessary. As for me I am glad I can use units especially crafted to measure the earth, instead of some stupid tyrant's left toe.

    10. Re:Circumference by Anonymous Coward · · Score: 0

      As for me I am glad I can use units especially crafted to measure the earth

      Congratulations--Would you like a doggie biscuit?

    11. Re:Circumference by Blethrow · · Score: 1

      I was there in January. You'll love it. It can be a bit of work (negotiations, schedules) but it's worth it.

  23. B-52 Monthership almost as interesting by Bravo_Two_Zero · · Score: 4, Interesting

    Almost as interesting as the X programs is the B-52 mothership that launches them. There was an Air & Space article years ago (no online version at airspacemag.com) about it.

    It's an aging early-model B-52B, evidenced by the non-pointy nose and is 49 years old. There are virtually no spare parts remaining for it, and most of the current inventory (Gs, Hs) don't have any parts commonality.

    Plus, we never sold any of them to other countries, so it's not like there's a stockpile somplace else on the globe. The cost to replace it is prohibitive, given the structural reinforcements needed to carry the craft aloft. Also, the airframe is very young from an hours perspective. In fact, it's the lowest hour B-52 in the inventory.

    The USAF has loaned an H-model to NASA to become the next generation launch platform, but I haven't heard much about it since the 2001 announcement.

    It's a supremely important beast in the research arsenal. And, given our penchant for resurrecting C-64s as web servers and using mame to emulate decades-old cabinet games, it seems like the sort of thing that would interest the average computer geek.

    Like so many things, it's the logistical details of maintaining an archaic aircraft against all odds (and lack of funding) that really become the story rather than the whizz-bang doodad that always gets the front page pictures.

    --


    Amateurs discuss tactics. Professionals discuss logistics.

    1. Re:B-52 Monthership almost as interesting by Mudcathi · · Score: 1
      given our penchant for resurrecting C-64s as web servers

      New clueless guy sez: "So that's why all of those sites keep getting slashdotted! Jeez, ya think they'd use better computers for webservers."

      --

      "He who throws mud, loses ground." - proverb

    2. Re:B-52 Monthership almost as interesting by ferralis · · Score: 1
      Hrm.. sounds like my company's server room...

      My favorite thing about the B-52 is that they just plain work. Damned fine (and lucky) engineering there. Unlike computers, once you've got a stable airframe there's really not much need to change it. Perhaps some smaller company will aquire licenses to build this thing... it would be wonderful if places like NASA and collections of major universities, etc. could obtain one.

      Probably unfeasible, though... and the durned things are certainly not sexy enough for marketting...

      --
      Any generalization is a stupid one.
    3. Re:B-52 Monthership almost as interesting by aldoman · · Score: 1

      What? Are you insane!?

      Do you know the amount of matience that is required for a B-52 or even a commercial 747?! Sure, you can refuel it in an hour or so, but if you want to service it it takes months.

      Also, I'd like to know how you know that B52's 'plain just work'. I'm sure some of them have had server faults that you never will here about.

    4. Re:B-52 Monthership almost as interesting by Dun+Malg · · Score: 1
      Almost as interesting as the X programs is the B-52 mothership that launches them. There was an Air & Space article years ago (no online version at airspacemag.com) about it. It's an aging early-model B-52B, evidenced by the non-pointy nose and is 49 years old.

      Here's a picture of the old B-52B (foreground) and their new B-52H (background) from the "50th Anniversary of the B-52" event a couple years ago. I personally like the old-fashioned 1950's "Right Stuff" look of the older one more than the hospital-white new one.

      Wow. Lot's more NASA B-52 pics

      --
      If a job's not worth doing, it's not worth doing right.
  24. What is a scramjet? by Jim+Hall · · Score: 5, Informative

    For those who want to know what a scramjet is, and how it works, check this page.

    A ramjet has no moving parts and achieves compression of intake air by the forward speed of the air vehicle. Air entering the intake of a supersonic aircraft is slowed by aerodynamic diffusion created by the inlet and diffuser to velocities comparable to those in a turbojet augmentor. The expansion of hot gases after fuel injection and combustion accelerates the exhaust air to a velocity higher than that at the inlet and creates positive push.

    Scramjet is an acronym for Supersonic Combustion Ramjet. The scramjet differs from the ramjet in that combustion takes place at supersonic air velocities through the engine. It is mechanically simple, but vastly more complex aerodynamically than a jet engine. Hydrogen is normally the fuel used.

    This is all very different from conventional airliner engines, which are a gas turbine/fan nacelle called a "turbofan". (A "turboprop" is a gas turbine driving a propeller instead of a fan, BTW.)

    1. Re:What is a scramjet? by Anonymous Coward · · Score: 0

      A former professor of mine has been working on something much cooler... though a long way off:
      http://caius.utias.utoronto.ca/shcramjet.htm l

      It's got a cool name too: Shcramjet

      Also, check out the RamRocket, a combined-cycle rocket engine. Very cool, but again, very advanced:
      http://caius.utias.utoronto.ca/rbcc.htm l

  25. A hypothetical assumption. by c.emmertfoster · · Score: 4, Funny

    Let's assume for a moment here that I'm not Buckaroo Banzai and I'm a little bit vague on what the upper limit has been for manned flight (or travel in any medium, salt-plain automobiles or whatever). "Mach seven" really doesn't sound all that impressive. THIS IS 2004! We should be on mach ten-hundred by now.

    For Christ's-sake, in that episode of ST:TNG where Riker had salt-and-peper hair and he didn't play trombone, I clearly heard him say: "WARP THIRTEEN! ENGAGE!" What the hell mach was Tom Cruise going before he entered into coitus with that blonde? What is the top theoretical speed of the current US fighter/and or/stealth aircraft?

    What are the records here, that my tax-dollars are allegedly breaking?

    Don't mod this retarded shit up, this is the uninformed wanting to become informed.

    --
    We can neither love nor pity nor forgive. If you make a slip in handling us you die!
    1. Re:A hypothetical assumption. by Magada · · Score: 0

      It must have been an in-joke on the part of the episode's writer. In Star-Trek mock physics, warp >10 is simply unattainable.

      --
      Something bad is coming when people are suddenly anxious to tell the truth.
    2. Re:A hypothetical assumption. by c.emmertfoster · · Score: 1

      Last episode of ST:TNG, the one where picard was alternately prescient/bizarre/senile. I believe it was called "All Good Things." I'm sure there is an after-the-fact explanation ala "the Kessel run," but it was said, never-the-less. ...

      --
      We can neither love nor pity nor forgive. If you make a slip in handling us you die!
    3. Re:A hypothetical assumption. by Glock27 · · Score: 2, Informative
      What is the top theoretical speed of the current US fighter/and or/stealth aircraft?

      Current fighters top out at somewhat over Mach 2, perhaps Mach 2.5 for the F-15.

      The upcoming F-22's top speed is classified, but it might be as high as Mach 3 (this is purely a guess on my part). It is quite a bit higher performance than the F-15, and can cruise at supersonic speed (somewhere over Mach 1, again classified) without afterburner. It's the first aircraft ever to have this capability, dubbed "supercruise" (not after Tom...I think).

      The SR-71 is the current air-breathing airplane speed record holder, with a top speed of around Mach 3.5, though the actual top speed is still classified as far as I can tell.

      The X-15 had a speed record of Mach 6.72 (in 1968!) but was a rocket, not an air-breathing aircaft.

      Hope that helped! :-)

      --
      Galileo: "The Earth revolves around the Sun!"
      Score: -1 100% Flamebait
    4. Re:A hypothetical assumption. by Hittite+Creosote · · Score: 2, Informative
      Fastest winged vessel the US has ever produced? 28,000km/h!

      Well, that was the orbiting velocity of the Space Shuttle. That's over Mach 20. It's rather easier to go fast in space - there isn't all that air you have to shove out of the way.

      The fastest combat jet is the MiG-25, which has been radar tracked at 3,395km/h.

    5. Re:A hypothetical assumption. by Anonymous Coward · · Score: 0

      The unofficial manned air speed record is Mach 6.7 which was attained by the X-15 according to this X-15 fact sheet.

    6. Re:A hypothetical assumption. by lommer · · Score: 1

      Well, as other posters have pointed out, it's quite simple to achieve ludicrous speeds in space, and the space shuttle regularly goes WAY faster than mach 7. However, for atmospheric flight the current record is held by the NASA/AF X-15 program in the 60's. In 1967 it hit a top speed of mach 6.7 and had two flights to over 100 km altitude (that's high enough to win the X-prize). The program was a great success, but had two failures, one of which totaled on of the planes and killed its pilot. Humans haven't returned to hypersonic (>mach 5) atmospheric flight since the program was cancelled (unless it's classified).

      It might not seem that this scramjet test is that impressive given that it is only going 0.3 mach faster, and that it isn't even manned, but it does reflect the direction of the last 40 years of aviation innovation - efficiency. Whereas the X-15 was powered by a rocket, this will have a full airbreathing engine. However, I'll agree that if you look at the fact that Yeager broke mach 1 in 1947, and the X-15 hit mach 6.7 in 1967, it's pretty sad that we have no craft capable of even taking a human faster than mach 5 in 2004.

    7. Re:A hypothetical assumption. by egomaniac · · Score: 3, Informative

      "Mach seven" really doesn't sound all that impressive.

      The SR-71 Blackbird has an official top speed of around Mach 3.5, and unofficially several pilots have reported taking the plane to substantially higher speeds. The plane's airspeed indicator goes up to Mach 5, if that means anything.

      At Mach 3.5, air resistance raises the plane's temperature to nearly a thousand degrees fahrenheit. Conventional aircraft aluminum would soften and lose its structural integrity at that temperature. For that reason, the SR-71's skin is made out of titanium. Thermal expansion causes the plane to be around six inches bigger while it's flying versus on the ground, which naturally caused nightmares for the plane's designers. The plane has a special cooling system which uses its jet fuel as a coolant liquid, circulated under the skin. After landing, ground crew must wait for a while before they can safely touch it, because the surface is so hot.

      And that's only Mach 3.5. Does Mach 7 still not sound impressive to you?

      --
      ZFS: because love is never having to say fsck
    8. Re:A hypothetical assumption. by Dun+Malg · · Score: 1
      It's the first aircraft ever to have this capability, dubbed "supercruise"

      Before some wiseguy points out that the Concorde cruised above mach 1 without afterburners, the difference is that the Concorde needed afterburners to GET above mach 1. The F-22 does not.

      --
      If a job's not worth doing, it's not worth doing right.
    9. Re:A hypothetical assumption. by Anonymous Coward · · Score: 0

      THIS IS 2004! We should be on mach ten-hundred by now.

      I know some people who have technology that can approach those speeds - they just need some test pilots. You should volunteer. :-)

    10. Re:A hypothetical assumption. by mnemonic_ · · Score: 1

      The F-22's top speed has been commonly quoted as 1.9M, mostly due to skin friction. It has demonstrated supercruise of Mach 1.53 and a requirement for the ATF program was supercruise of at least 1.5M. There are strong reports that both the British Electric Lightning and American F-14D were capable of supercruise, albeit at a much lesser magnitude (~1.1M with no external stores).

      The SR-71 is not completely "air-breathing." It used a turbo-ramjet hybrid design created by engineer Ben Rich. It only was airbreathing when functioning as a ramjet.

      Top speeds are only "top" until they're broken. The highest speed I've seen quoted for the SR-71 is around 3.2M, and as that was significantly above its typical cruising speed I doubt that it could go higher. I've never heard of it being "classified."

    11. Re:A hypothetical assumption. by mnemonic_ · · Score: 1

      "What is the top theoretical speed of the current US fighter/and or/stealth aircraft?"

      There's not a formula (or formulae) currently with which one can just plug in some values and come up with a theoretical terminal speed for an aircraft. Even disregarding differences in aircraft configuration (additional stores, fuel etc.) and flight path (level flight, dive, low altitude, high altitude?) top speed is the combination of a million different mechanical, aerodynamic features, impossible to calculate with significant precision.

      Of course, one can easily make reasonable estimates based on past demonstrated performance. The fastest U.S. fighter is the F-15 with a top speed of Mach 2.5 (achieved with a minimal fuel load and clean configuration).

      Top speed doesn't matter so much in a fighter though as sustained speed and acceleration to a lesser degree. The quoted top speed (i.e. used to advertise the aircraft to potential buyers) can only be maintained for a few minutes at most before too much fuel is consumed. Practically speaking, a high top speed for a fighter is only significant because it implies a high acceleration, which is essential in tactical air engagements (i.e. dogfights) in which complex maneuvers rely on rapid positive and negative acceleration (among many other things).

      Hope this helps.

    12. Re:A hypothetical assumption. by thebigmacd · · Score: 1

      "The SR-71 is not completely "air-breathing." It used a turbo-ramjet hybrid design created by engineer Ben Rich. It only was airbreathing when functioning as a ramjet."

      You just contradicted yourself. A turbo-ramjet consists of a turbojet and a ramjet. If it had a rocket it would be called "rocket-ramjet".

      It is always air-breathing.

    13. Re:A hypothetical assumption. by catfry · · Score: 1

      Regarding the f-22, I seem to remember having read somewhere, that due to the fact that the plane has no variable geometry intakes, the possibility of it both being effective at low speed, and at over mach 2, is quite low, the conclusion being as far as i remember, that the f-22 probably cannot go significantly faster than mach 2

    14. Re:A hypothetical assumption. by hyc · · Score: 1

      Yep, all true.

      PS, I've flown in one.

      http://www.highlandsun.com/hyc/blakbird.jpg

      --
      -- *My* journal is more interesting than *yours*...
  26. Obligatory Spaceballs comment by MalaclypseTheYounger · · Score: 5, Funny
    "Prepare ship for Ludicrous Speed! Fasten all seatbelts, seal all entrances and exits, close all shops in the mall, cancel the three ring circus, secure all animals in the zoo!"

    What have I DONE!?!?! MY BRAINS ARE GOING INTO MY FEEEET!!!

    --
    Check out the best P2P sharing website: MEDIACHEST.COM
  27. It will be... by Anonymous Coward · · Score: 0

    It will be a spectacular failure :-(

  28. Re:Is this not just about the same as yesterday? by Ctrl-Z · · Score: 0, Troll

    Yes, same story, same "editor". Welcome to Slashdot. Please pick up a gift bag from the table on the right.

    --
    www.timcoleman.com is a total waste of your time. Never go there.
  29. Re:Use of technology by Machine9 · · Score: 0, Offtopic

    We don't need anything beyond a stick. Of course, there will be treacherous governments that equip their armies with the much more advanced board-with-nail-in-it. Violating all sorts of treaties with their sophisticated military might.

  30. Re:Use of technology by Anonymous Coward · · Score: 0

    And, of course thise technology will be used for war. There's never been a technology that hasn't been used for war. Even the simple wheel enabled some nasty engines of destruction. Does this mean that we should not have technology?


    Just ask Ted Kazinski.

  31. ScramJet rocks for overseas trips by the_thunderbird · · Score: 1

    Thank god, finally a tech that won't leave me in a plane for 12 hours while travelling overseas without a cigarette! Yippy!

    1. Re:ScramJet rocks for overseas trips by LoveMuscle · · Score: 1

      There's a cheaper/healthier (but not necessarily easier) solution to that problem. Quit your vile tobacco habit...

    2. Re:ScramJet rocks for overseas trips by the_thunderbird · · Score: 1

      true dat!

  32. Dive? by bluGill · · Score: 4, Insightful

    Mostly I agree, but your first question starts with an incorrect assumption: a 600mph vertical dive. Pilots are trained at ditching an airplane at sea, and planes do float for a short time after this happens. In fact (though I don't know of any specific cases off hand) it has happened before, and many passangers have survived ditching at sea. Vertical dives do not happen in a significant amount of emergency situations, wings are simple devices and don't break all that often, and a wing is all you need to prevent a vertical dive.

    Airplanes have backup batteries, and backup radios. You can be sure that before the plane hits the water emergency people know that it is going down, and about where. They might not be able to get to you in time to save you, but they at least know where to look just in case.

    I'd prefer to float around the North Atlantic than die. Though I think it is safe to assume that if it really is several days before rescure workers find you they will find a dead body. However depending on where the crash happens, rescure workers may find you sooner.

    1. Re:Dive? by Hektor_Troy · · Score: 1

      Well, to be completely honest, the two points I made were taken from George Carlin's skit about airplane announcements, but imagine if you will, a catastrophic loss of cabin pressure (roof flies off) and it just HAPPENS to take the cockpit with it, just how are the pilots supposed to steer it? Sure, it doesn't happen all that often, but hey - we were talking about unlikely events anyway (like maneauvering (how the devil do you spell that?) a hypersonic aircraft outside of it's safety envelope).

      --
      We do not live in the 21st century. We live in the 20 second century.
    2. Re:Dive? by molarmass192 · · Score: 2, Informative

      Even if you survive the crash, you'd die of hypothermia in a few hours. I don't know if you've ever swam in the North Atlantic but I spent a few days at the beach in Nova Scotia in the middle of August and let me assure you that the water was not much over 60F. You die when your body core temp reaches 80F. In 60F water, you've got about 3 hours of survival time immersed. So, in an ideal scenario, unless the rescuers get to you in under 3 hours, you're gonna die anyhow.

      --

      Good people do not need laws to tell them to act responsibly, while bad people will find a way around the laws-Plato
    3. Re:Dive? by Hittite+Creosote · · Score: 1

      Well, you're dead. Just as you are if that really huge truck on the opposite carriageway has a major blowout and suddenly veers right across you and you have an articulated trailer hit you in the face at over 100mph while you were on your way to the airport.

    4. Re:Dive? by Anonymous Coward · · Score: 0
      Just so you know your original comment was appreciated

    5. Re:Dive? by ValentineMSmith · · Score: 2, Interesting

      While this wasn't actually a "successful" ditching attempt, IIRC, over half the passengers lived through it. The video link on the site doesn't actually lead to a video of the crash, but I can remember seeing the video on one of those "Real-People-In-Real-Pain" TV shows for which the Fox network is so famous. The Aircraft came to rest roughly 500 metres or so from the beach, and the water was relatively shallow. Several people on the beach waded out and helped the passengers to shore.

      --
      Karma: Chameleon - mostly influenced by bad '80s New Wave music
    6. Re:Dive? by StevenMaurer · · Score: 1

      Actually, this example is the exception that proves the rule that the original poster made.

      This is the absolute best scenario under which a plane could ever be expected to ditch - warm water, immediate help, shallow "landing" type incline, etc. - and still about half the passengers died.

      Heaven help you if something actually goes wrong on an airplane over cold ocean that can't be immediately fixed - because you're dead. Period. All the FAA "safety" rules amount to is window dressing trying to disguise this fact.

  33. How fast is Mach 7? by StateOfTheUnion · · Score: 1
    How fast is Mach 7? In fact how fact is a Mach?

    Mach = Speed of Sound, but speed of sound changes depending on air density/pressure (altitude), temperature, and absolute humidity.

    When someone says Mach 7, is that at sea level and STP (standard temperature and pressure {1 atm, 25C)) or is that at the altitude and conditions of the air through which the craft is flying (e.g. 30,000 ft, -25C)?

    1. Re:How fast is Mach 7? by Anonymous Coward · · Score: 0

      STP = 1 atm @ 0C, Standard State = 1 atm @ 25C

  34. Re:Is this not just about the same as yesterday? by Anonymous Coward · · Score: 0

    yep

  35. Well, if anything goes wrong in any plane by purduephotog · · Score: 1

    "You're toast", as you've aptly pointed out.

    There's not alot that can be done when your tail section blows out due to improper riveting. You can't do anything but pray and land when the top of the aircraft peels open like a sardine can due to a bad joint that allows a crack to propogate the length of the plane.

    And you know what? People still die falling down a flight of stairs.

    It doesn't matter how fast you go, how close to the ground you are.

    Now you do have good points about wing shock, but, those speeds are air that is no longer as dense, thus the forces exerted are much less and probably very close to equivelant as what's seen now adays.

    I think I'd like to be able to go from NYC to London in 2 hrs. Especially if it works out to be cheaper.... I could go get my warm beer and be back before the night is out :)

  36. 5,000 mph by ubeans · · Score: 1

    Seven times the speed of sound? How does that compare to the Millenium Falcon going at hyperspeed?

  37. My sister did the logo! by TheXerox · · Score: 3, Interesting

    My sister Caity died of cancer at 11 years old a couple years ago..

    Caity was out in California for proton radiation treatment, Joel (uncle in law / NASA engineer) held a party for his Engineering Section at his house and Caity drew a picture of the X43 plane's logo on the sidewalk in chalk.

    After Caity passed Joel took the picture of her sidewalk drawing and went to Nasa to have the plane named in Caity's honor and have her picture on the side of the plane.

    I hope this one does a lot better than the last time, it has a lot of sentimental value!

    --
    Mountain Dew and doughnuts, because breakfast is the most important meal of the day!
    1. Re:My sister did the logo! by Jesrad · · Score: 1

      I hope this one does a lot better than the last time, it has a lot of sentimental value!

      You can be proud, it did.

      --
      Maybe we deserve this world ?
  38. X-43C is cancelled, unfortunately by Maimun · · Score: 2, Informative

    I already posted this in another discussion here, but probably it is worth mentioning again. The bigger cousin of X-43A, X-43C, is being cancelled because it does not fit in the new space plans.

  39. Deja Vu ? by AftanGustur · · Score: 2, Insightful


    The article claims travel benefits, going from New York to London in 2 hours. But honestly, travelling that fast, if anything went wrong you're toast.

    I imagine this is almost exactly what was claimed when the combustion engine was being developed..

    Just think about it:
    The inventors claim travel benefits, going from New York to Bostin in 3 hours. But honestly, travelling that fast, if anything went wrong you're toast.

    --
    echo '[q]sa[ln0=aln80~Psnlbx]16isb572CCB9AE9DB03273snlbxq' |dc
  40. Is it just me... by Jexx+Dragon · · Score: 2, Insightful
    or are prototype names getting stupider? Really Hyper-X? Sounds like the name for a fighter in a cheap sci-fi. Even Star Trek uses a letter(s) followed by numbers.

    Maybe since Sci-fi authors started using the normal system NASA felt they needed to distence themselves from the logical way of doing things so as to gain/keep credibility?

    --
    I don't have time to comment my code, the program is late already.
    1. Re:Is it just me... by Anonymous Coward · · Score: 0

      makes sense to me... X is always used for experimental planes, and it's hypersonic... so hyper-x.

  41. It's a shame... by Anonymous Coward · · Score: 0

    they keep putting this on OSC's Pegasus XL vehicles. The first Pegasus rockets were painted black, but they had to change them to white because it was too hard to recover the black ones from the ocean floor.

  42. Further research issues? by jollygreengiantlikes · · Score: 1

    Does anyone have direct experience with the Hyper-X project? An undergraduate physics cohort of mine spent some time at Langley doing research with the project team and at that point (~5 years ago) there were significant problems with the engine itself (such as the airspeed differential at the intake of the engine). The article doesn't comment on what steps have been taken to correct these issues and to warrant a test of the engine?

    JGG

  43. Blows up faster than the Concorde by Anonymous Coward · · Score: 0

    So searching for wreckage and humans after a crash will cover many hundreds of miles? Brought to you by the lowest common bidder, your tax dollars at work. What idiot made price over quality a government mandate?

    Sure NASA will build the test models right at some point, who will make the commercial jets properly with all of the price wars going on? Where will they be allowed to fly? The Concode wasn't even allowed to fly at full speed in many areas, nonless even take-off or land.

    I'd rather take my chances on the Paris railline...

  44. Why is the X43 a big deal..what about Aurora? by Reik · · Score: 1

    Hasn't Aurora been going faster than this for almost fifteen years now?
    Nevermind that no one officially knows about it or has even gotten a decent picture...

    1. Re:Why is the X43 a big deal..what about Aurora? by Anonymous Coward · · Score: 0

      B2 Spirit is the Aurora. Ever wondered why there are no toilets in this plane which is supposed to do 15-hours-long missions ?

  45. ahhhh, the eligance of simplicity... by LifesABeach · · Score: 0

    my mind wonders to the Actual math/engineering that it would take to evaluate this solution to beyond just the 'X-Prize'.

    instead of a bomb, think of some type of manufacturing process that uses micro gravity, and vaccum. or the retrieval process of space objects.

    were the hell is McGiver when we need him?

  46. Rather US Centric statement by mcbevin · · Score: 0, Troll

    I like this quote from the Mission Information - 'No vehicle has ever flown at hypersonic speeds powered by an air-breathing scramjet engine.'

    Aren't they forgetting a few other countries here - India .... Russia? Didn't even Australia get something flying?

    Maybe they haven't technically flown a _vehicle_, and maybe I'm slightly mistaken here, but I find it almost typical of NASA to so completely ignore these other countries who in this case actually got there first and are possibly (?) more advanced than NASA in this area.

    Of course if your world view is limited to America and the occassional country it chooses to bomb, then the statement is in its way correct :).

    1. Re:Rather US Centric statement by Anonymous Coward · · Score: 2, Informative
      Maybe they haven't technically flown a _vehicle_,

      No, they didn't. It was a rocket test.

      and maybe I'm slightly mistaken here

      Yes, you are.

      but I find it almost typical of NASA to so completely ignore these other countries who in this case actually got there first and are possibly (?) more advanced than NASA in this area.

      No, NASA's statement, as it was worded, was correct. It is you who are in error.

      Of course if your world view is limited to America and the occassional country it chooses to bomb

      Would you please fuck off and die, you ideological bigot? Can't we keep the worst of the international politics out of the sciences, or has ideology fucked over your brain that much?

    2. Re:Rather US Centric statement by 110010001000 · · Score: 1

      Maybe you should worry less about what we are doing and more about what your country is doing. Those countries did not fly a vehicle, but a rocket. You are stupid, and mistaken.

    3. Re:Rather US Centric statement by HokieJP · · Score: 1

      India has announced a program that will test a similar plane in a few years. Australia tested a scramjet mounted on the front of a rocket, and it was falling straight down towards earth at the time the jet achieved combustion. I couldn't tell you about Russia. Fortinately, I don't really have to, since you just tossed some names out without even attempting to make a case. Maybe you should try to get some facts before you go making unfounded accusations?

    4. Re:Rather US Centric statement by Anonymous Coward · · Score: 0

      India hasn't even run ground tests on their scramjet engines yet, they will begin ground tests ni 2005.

      Russia (I'm not 100% sure of this) has flown a scramjet engine strapped to a missle, and it did generate thrust, but it was not the power source for the missle, it was just along for the ride. I haven't heard of them flying anything powered by a scramjet.

      Australia strapped a scramjet engine to a rocket, fired it 300km up, let it freefall back into the atmosphere, and turned on the scramjet for about 6 seconds right before it hit the ground. I'd hardly call that a scramjet powered vehicle.

    5. Re:Rather US Centric statement by mcbevin · · Score: 1

      I was thinking more about the Indian/Russian scramjet missile which afaik already works and is faster than anything else in the world. Heres a few links I was able to quickly google:

      http://www.nti.org/e_research/profiles/India/Mis si le/
      http://www.newsmax.com/archives/articles/2001 /12/1 2/140853.shtml

      As I said in my message, I'm aware these aren't _vehicles_, however I've always thought of them as the state of the art in this area rather than what NASA is doing. Perhaps someone can explain how what NASA is doing is more difficult/advanced.

      In any case, I just thought these things warranted mention (especially given the fact that nuclear armed missiles in the hands of a not-too-stable-state flying faster than anything the US has - and thus presumably rendering the planned missile system helpless - imho warrent attention).

    6. Re:Rather US Centric statement by HokieJP · · Score: 1

      So, in your first link, the words "proposed hyperplane" suggest to me that their plane, unlike NASA's, doesn't exist yet. The rest of the article, as far as I could tell, is about ballistic missles powered by rockets and 'regular' jets.

      The second link is from NewsMax. Since I assume you're not from the U.S., you may not know that this is not a reputable news site. They are actually ultra-right scandal-mongers. I didn't see a single source cited in that entire article, but it appears they took the news from a Washington Times article (the Times is another right-leaning paper, not to be confused with the reputable Washington Post). The Russians denied the report as can be seen here. So if you want to believe that the Russians have scramjet-powered BM warheads, you go ahead. I won't say that they don't, but to ignore such rumors when discussing real hypersonic research doesn't make one "US centric"

  47. Re:Physics Question - orbital velocity by CyBlue · · Score: 1

    Spacecraft and satellites don't *escape* the earth's gravity. They just reach high enough speeds such that for every meter they fall toward the earth, they've gained a meter in altitude by traveling forward along the curve of the earth. If you're going faster than orbital velocity, you'll leave the Earth, if you're going slower, you'll spiral inward until you crash.

  48. Re:Physics Question - orbital velocity - part deux by CyBlue · · Score: 1

    To further clarify, when you're on the ISS or Space Shuttle, you're not exactly in zero gravity. You're constantly free-falling towards Earth. Anything that's not traveling fast enough along the curve of the earth outside of the atmosphere will fall back down rather fast.

  49. Project cancelled by Anonymous Coward · · Score: 0

    Seems they at least have funding left for a test flight, which is good.

  50. Here's your answer by soldeed · · Score: 1

    This is only the first test of the technology. The scramjet concept has been around a long time, and they have tested them in wind tunnels before, but no one has ever actually flown one yet. Future models WILL go mach 10, but this one wont. Baby technologies take baby steps.

  51. Good post, but... by bjdevil · · Score: 1
    2) Do I really want to float around in the North Atlantic for several days, clinging to a pillow full of beer farts

    ...don't forget to give George Carlin credit when using his material (one of the best shows he ever did, BTW).

    --
    Some are born to move the world, to live their fantasies... Neil Peart
  52. Scramjets = Mach 10 cruise missile by citanon · · Score: 1
    A Mach 10 aircraft would not be able to fly around the world faster than an ICBM, which travels at ~Mach 25 through orbit and can reach any target in the world 30 minutes after launch from the continental US.

    On the other hand, while a rocket needs to carry its own propellant, the scramjet uses atmospheric air. It is therefore much more efficient, and for a given size and weight constraint, one could build a scramjet powered vehicle that could have some combination of greater speed and range over conventional rocket propelled vehicles.

    For the military, this means that you could probably pack a Mach 10, six hundred mile range missile into a SM-II launcher. Then every destroyer and cruiser in the Navy would be able to carry dozens of missiles that can hit targets six hundred miles away within six minutes of launch. Once it gets there, its warhead, traveling at Mach 10, will have several times the destructive power of a warhead on a cruise missile, which travels at just below Mach 1.

    The characteristics of a scramjet powered missile would allow the military to attack deeply burried bunkers and highly mobile targets with cruise missiles launched from hundreds of miles away. It's a military wet dream.

    Globalsecurity.org, as always, has a nice write-up.

  53. Spoiler Alert by Dr.+Evil · · Score: 1

    Because, if the worst comes to the worst you can do the DiCaprio, and choose to let go.

    Hey, I didn't see that movie!

    1. Re:Spoiler Alert by Anonymous Coward · · Score: 0

      YM "you insensitive clod". HTH.

  54. Ahh, a Tom Lehrer tribute! by Buran · · Score: 1

    from the once-the-rockets-go-up-who-cares-where-they-come-d own dept.

    "That's not my department," said Wernher von Braun.

  55. Bullocks!! Anglo-Saxons are the superior race !!! by Anonymous Coward · · Score: 0, Troll

    You have Einstein, we have Newton
    You have Neumann, we have Turing
    You have Salk, we have Fleming

    Good books you say? You have Shatner, we have Shakespeare ...

  56. Re:Why? its a bomb of course... by Diclophis · · Score: 2, Insightful

    Like everything else the govt pays for... its an offensive weapon. take a look at the calculations

    ((1 / 2) * (1 000 kg)) * ((7 000 mph)^2) = 4.89619666 x 10^09 Joules

    a 20 kiloton bomb is ~10^13 joules...

    What these means is... if they can put these engines on largers chunks of mass (i.e. increase the mass of the object flying at 7 times the speed of sound). They could have a bomb, with the explosive power of an atomic weapon... without using atomic methods. There is no need to strap a atomic warhead to this missle.... the missile is the warhead. And the best thing is... you would never hear it coming (radar wouldnt give you enough time to react (bleep bleep boom)).

  57. "Balls Eight" Retired. by ericlp · · Score: 1

    I'm curious about that stock photo. "Balls Eight" B-52B #008 is supposed to be retired now with the B-52H you mention ( it is painted white, with the NASA logo - looks weird ) Taking over the job. There was some overlap time for both jets, but the tall tail B model should be gone now.

  58. From the by g0bshiTe · · Score: 1

    We posted a similar article yesterday department.

    I what department this story actually comes from.

    *INSERT FLAME HERE*

    --
    I am Bennett Haselton! I am Bennett Haselton!
  59. Hypersonic Cruise Vehicle (bomber) ? by spruce · · Score: 1

    Maybe it's related to these plans?

    Choice quotes...

    "The US will be able, using aircraft based on its own territory, to strike at individual targets without warning and without the need for foreign bases"

    "The current and future international political environment severely constrains this country's ability to conduct long-range strike missions"

  60. Hmmm by Anonymous Coward · · Score: 0

    I saw one a few months ago at Castle Air Museum (near Modesto, CA...http://www.elite.net/castle-air/) and the wingspan sure didn't seem like 55 feet....and I was walking around underneath it. The plane seemed very slender and thin....more like a steerable horizontal rocket. I guess it's in the perception of the shape though. On the other hand, the B-36 they have seemed gigantic...no wait, it is gigantic.

    1. Re:Hmmm by trs998 · · Score: 1

      I find it difficult to believe its got a WINGSPAN of 55 feet.

      basically it consists of a fuselage and two vast engine nacelles. The 'wing' is the 4-6 feet wide strip between the engines and body, plus a tab on the outside of the engines.

      I imagine wherever you got the data from counted every horizonal surface (aka the entire plane bar tail) as 'wing' - it all generates lift, but wing is traditionally the bits that arnt in the main fuselage or engine nacelles.

      anyway, who needs wings when you can just vector the thrust down a bit?

  61. Re:Why? its a bomb of course... by bindo · · Score: 1

    RIIIiiight...

    so DOING the calculations you would be just 10^4 off a 20 kiloton bomb.
    That is the equivalent of a 2 ton bomb (tnt equivalent).

    I think Most militaries have these at least since WWII ....

    so what ?

    Bind0

  62. SR-71? by rice_burners_suck · · Score: 1
    Why not use the good ol' SR-71? It goes at least that fast, and is already known to work.

    Yes, I know Buick stopped making the SR-71 a few months ago, but they should restart their high-quantity production.

    1. Re:SR-71? by richmaine · · Score: 1

      The SR certainly does *NOT* go that fast.

      And one of the main reasons that the SR can't go that fast (well, beside the fact that it wouldn't be able to take the heat) is *DIRECTLY* related to the whole point of scramjets.

      The SR is a ramjet (well, it is a multi-mode engine, but we'll skip over that part). The extra sc in scramjet is for supersonic combustion, which is the whole tricky point. If you have to slow the intake air down to subsonic speeds for the combustion, you are fighting a loosing battle as the vehicle speeds go up. Ramjets like the SR are not practical at hypersonic speeds.

    2. Re:SR-71? by rice_burners_suck · · Score: 1
      You mentioned heat, which is interesting. The SR-71 can, in fact, take a LOT of heat. The plane's components are quite a bit smaller than they need to be in order to fit together. In fact, when it is fueled on the ground, gasoline actually spills out from the cracks. It is extremely dangerous to start the aircraft because the entire thing could explode. Once in the air, the plane begins to heat up, and the parts therefore expand and fit together properly. The plane then must be refueled (in the air), after which it can go to its destination. Also, it is able to go much faster than "they" will care to tell you.

      Of course, you didn't hear it from me. (I saw it all on a documentary on the Discovery Channel or something like that.)

    3. Re:SR-71? by Anonymous Coward · · Score: 0

      Actually, all that fuel (which is certainly NOT gasoline) leaking out on the ground is not dangerous at all. The amount of heat that is require to ignite it is immense, so that the plane doesn't explode as it's flying along (the fuel is used as a coolant for the rest of the craft). This also made the fuel a commodity, and expensive to produce, which is one reason why the program got shut down.

    4. Re:SR-71? by richmaine · · Score: 1

      It will take a lot of heat, but not that much. Not Mach 7... or even 4. In fact, what I hear from people who would know (and who are a lot better sources than anything on Discovery channel - some of them have flown it) is that the speed is heat-limited instead of thrust-limited.

      Yes, it eventually would run out of thrust (and long before Mach 7), but it would have heat problems first. If I recall correctly (but I'm not as sure of that part), it is the engines that first run into overheating problems.

      P.S. Don't believe every rumor you here just because it sounds good to put down what "they" tell you. "They" don't always tell you the truth, but then neither do the people who tell you that "they" are lying.

  63. Re:Military - yuck by trybywrench · · Score: 1

    if they could use this to build a mach 7 cruise missile that has the accuracy of todays cruise missiles it would be an incredibly formidable weopen. Imagine a spy sat. finding a target and then being able to deliver ordnance on that target within a few hours regardless of whether or not there are any deployments in the region.

    --
    I came to the datacenter drunk with a fake ID, don't you want to be just like me?
  64. Bleh - 1950s technology... by HermanZA · · Score: 1

    These things have been experimented with decades ago. What is different about it now?

  65. Re:Why? its a bomb of course... by Diclophis · · Score: 1

    What...?

    the point is hat this bomb could be delivered to any point on the surface of this planet, without the target knowing, and or having enough time to react. e.g. launch rocket... 1 hour later USA to (uncooperating nation) "You have 1 hour to comply to our demands or your building (capitol, army facility, stock pile of tnt) will explode.". There is know way they could evacuate a army facility or remove the sensitive materials from the target before the bomb got there... if they comply to our demands... the bomb flys over there heads, into the ocean somewhere. And of course if we anticipated that they werent going to comply... every 30 minutes we launch another one.

    This is what most people dont understand about atomic weapons. A. Everyone is afraid of them being used... look at the facts, USA is the only nation to use atomic weapons to harm humans on purpose. B. When we bombed hiroshima, the japanese did not comply, 1 week later we bombed another nagasaki they got the point that time... if the japanese had not complied then... the USA would have built even more bombs, quicker faster and bigger (its the american way you know)... Little Boy (the first atomic weapon dropped on hiroshima) weighed ~10,000 lbs... the b-29 bomber that carried the bomb has a max load of 20,000... so thats 2 bombs / b-29... according to the wikipedia site in 1940 the govt contracted for 1200 b-29s... thats 2400 hiroshimas... a day... USA has had the ability to bomb this planet into non-existance ever since we built the first damn device ('I am death destroyer of worlds'). And now, not only do we have the technology to nuke earth to hell and back... we can send bombs to mars, jupiter, the moon... any point in our solar system. "HELLO WORLD" if you think your going to be somewhere, where you cannot be nuked to hell by the united states of fucking america, you are sadly mistaken. And to think that every redwhiteblue blood is running around afraid of towelheads hijacking aircraft... the only terrorists we should be afraid of are ourselves (and fucking idiots driving with cellphones).

  66. 5,000 mph = ? KPH by Pejorian · · Score: 1

    I hope NASA has all the units right on this one, and they don't get all excited when it hits 5000 KPH.

    Wouldn't be the first time they'd gotten confused between metric and that kludgy old British system that the rest of the US uses.

    I always find it funny that the US made such a stink about getting out from under British rule, but they continue to use their measurement system long after everyone else has moved on...

    --
    - Murphy's Corollary: - It is impossible to make things foolproof because fools are so ingenious.
  67. This is not the first scramjet by Clod9 · · Score: 1
    In the Mission News item labeled "03.24.04 - Latest Update: X-43A Flight", NASA's site says:
    "No vehicle has ever flown at hypersonic speeds powered by an air-breathing scramjet engine."

    How does this relate to the run of HyShot back in August? The X-43A won't be the first successful scramjet-powered flight....and HyShot was designed to go Mach 7.6, which I think is hypersonic. Is NASA implying that HyShot didn't really work?

    1. Re:This is not the first scramjet by xeosdd · · Score: 2, Informative

      No, they just don't like it when a project that cost a fraction (arround AU$1.5 million) of what theirs did suceeded before theirs did, by a bunch of mechanical engineers at a university that nobody knows about. More details about the project are available at the Center for Hypersonics and UQ news.

      We had some lectures from the head of the engineering faculty in first year, and he went into a fair bit of detail on how the system worked. Last I heard was that the project has received further funding, but that was shortly after their mostly sucessful trial run (they couldn't find their rocket for a few weeks in the Australian desert). I've heard nothing else about it since, though. But that's probably because all anybody talks about now is mice in space.

    2. Re:This is not the first scramjet by Acrimonious+Coward · · Score: 1

      HyShot did not achieve scramjet-powered flight. It was a scramjet attached to the front of a missle and was merely a test of the combustion characteristics at hypersonic speeds, it never flew by itself.

    3. Re:This is not the first scramjet by Anonymous Coward · · Score: 0

      The australian engine did turn on succesfully, and worked for a few seconds before it crashed into the ground. But, it did not fly under it's own power since it was attached to a rocket at the time. Also, it did not achieve its top speed.

      It was the first successful test of a scramjet engine but not a successful test of scramjet powered flight.

  68. Aerospaciale? by mnemonic_ · · Score: 1

    What the fuck? There is not and never has been any aircraft manufacturer with a name close to "Aerospaciale." The Concorde was jointly developed by a consortium of British and French companies, none of which have the name which you conjured.

    1. Re:Aerospaciale? by mccrew · · Score: 1
      Mr. mnemonic, meet Mr. Clue.

      If you are too lazy to click the link, I quote, "Airframe development and production of the Concorde were undertaken jointly by Aerospatiale and BAe, with two final assembly lines, at Toulouse and Filton respectively."

      Here's some advice: next time do a quick search to save yourself the shame of your profane public display of ignorance. Hah!

      --
      Hey, Windows users, there is no such thing as "forward" slash, there is only slash and backslash.
  69. Re:Physics Question - correction by mccrew · · Score: 1
    ...must proofread posts better...
    ...must proofread posts better...
    That should be:
    • If the ratio of densitySL/densityEverest is
    • 3, then solving for velocityEverest
    --
    Hey, Windows users, there is no such thing as "forward" slash, there is only slash and backslash.
  70. no by mnemonic_ · · Score: 2, Informative
    1) US refusing Concorde at supersonic speed over US territory.
    Done for the same reason that most western European countries cited when limiting Concorde flights, i.e. noise. I'd expect less noise to be generated by scramjets because of the lack of fans (reducing aerodynamic and mechanical noise) and more compact combustion of the vapor-fuel mixture.

    2) Price of petrol
    SCRAMJETs will not use kerosene-derived propellant. They will combust hydrogen with oxygen from the atmosphere (maybe you should have done 2 seconds of research).

    3) 2 hours of transatlantic flight, 2 hours to go to the initial airport, 2 hours to go from the final airport...
    A flight on a Mach 5 aircraft will be shorter than the same flight on a Mach .9 aircraft.

    4) Looking back at this, it was somewhat an ecological catastrophe
    If what you mean by "somewhat" is "not really." I can't see the 20 Concordes built adding significantly the net pollution of thousands of supersonic military aircraft in service around the world.

    How will all those factors be taken into account by the sdcramjet developers?
    They don't need to.
  71. Re:still need ...Yes by dnoyeb · · Score: 1

    RTFA, but that could be applied more to those who responded that you.

    TFA implies it will always need assistance.

    This engine works by taking in compressed air at supersonic speeds. It necessarily must be launched to supersonic speeds by some other means.

    NASA's current design is, from TFA, launch craft from earth with Jet engines, mid-earth flight with scramjet, into outers-space with rockets.

    So this is a more accurate test than one might imagine without **** :-)

  72. one more thing about the SR71 by tacokill · · Score: 1

    Don't forget that, while sitting on the ground before takeoff, there is SUBSTANTIAL fuel leakage out of the plane. It consistently drips a significant amount of fuel while on the ground and not "heated". Once the plane is in the air and heated up, the expansion causes all of the joints and fittings to tighten up thus eliminating fuel leakage.

    Kind of a weird "feature" but I thought I'd throw that in as well.

    1. Re:one more thing about the SR71 by egomaniac · · Score: 1

      This also happens during flight, actually -- when the SR-71 refuels from a fuel tanker, it has to fly subsonic so that the tanker can keep up with it. This causes it to cool off enough that it starts to leak again, and it only tightens back up once it reaccelerates.

      --
      ZFS: because love is never having to say fsck
  73. It's tiny! by Anonymous Coward · · Score: 0

    Just look at it! The actual plane is the black thing at the front of the booster.

    http://www.dfrc.nasa.gov/Gallery/Photo/X-43A/Med iu m/EC01-0019-18.jpg

    More pictures here
    http://www.dfrc.nasa.gov/Gallery/Photo/X-43A /index .html

    1. Re:It's tiny! by Anonymous Coward · · Score: 0

      Stupid comment box put spaces in the urls. There shouldn't be a space in "Medium" on the first url and there shouldn't be a space in "index.html" in the second url.

  74. That's not a troll, it's the truth by Anonymous Coward · · Score: 0

    I think it's unfair to mod it as a troll because he is absolutely right.

  75. Re:Why? its a bomb of course... by jafac · · Score: 1

    The engine will not function at relatively low altitudes. The thicker air will likely poison the reaction, or at the very least, the characteristics of the shock wave will cause it to not be directed into the nozzle properly. It will likely slow significantly due to air-drag, without thrust, at low altitude.

    But I think it might make a nifty interceptor warhead for NMD. . .

    --

    These are my friends, See how they glisten. See this one shine, how he smiles in the light.
  76. Re:Use of technology by Call+Me+Black+Cloud · · Score: 1

    Why do people keep saying we were there to get someone else's oil? We're seeing record prices at the pump. Hell, I wish we had taken oil...we could use it about now.

  77. Re:Use of technology by Call+Me+Black+Cloud · · Score: 1

    The flamebait part came from, "Rather than say, bombing civilians into the ground just to get our hands on somebody else's oil." If there was basis in fact it wouldn't be flamebait.

  78. NASA slashdotted? by Anonymous Coward · · Score: 0

    I can't get to any nasa.gov sites. www.nasa.gov resolves to canonical www.nasa.gov.speedera.net. I don't think it's possible to /. NASA, so is anyone else unable to reach NASA sites?

  79. Re:Why? its a bomb of course... by Wyatt+Earp · · Score: 1

    The B-29s were not all capable of delivering A-bombs in 1945.

    There was a special model B-29 called the "Silverplate" that was the only B-29 that could drop nukes.

    http://www.nasm.si.edu/research/aero/aircraft/bo ei ng_b29.htm

    "Late in 1944, AAF leaders selected the Martin assembly line to produce a batch of Superfortress atomic bombers codenamed "Silverplate" aircraft. Martin modified these special B-29s by deleting all gun turrets except for the tail position, removing armor plate, installing Curtiss electric propellers, and configuring the bomb bay to accommodate either the "Fat Man" or "Little Boy" versions of the atomic bomb."

  80. Re:Use of technology by Anonymous Coward · · Score: 0
    Why do people keep saying we were there to get someone else's oil? We're seeing record prices at the pump. Hell, I wish we had taken oil...we could use it about now.

    Why do you think the object of controlling oil production and shipping is to lower the price? Gas wasn't exactly cheap (in constant dollars) back in the 50s, when mid-east oil was vertically integrated from well to pump. The lowest gas prices were under Clinton, IIRC.

    Your logic is specious.
  81. Re:Use of technology by good+soldier+svejk · · Score: 1
    First, it's not offtopic. Meta moderators, please fix this.

    Done. Or at least I meta-modded the offtopic mod "unfair." I wish I could fix it.
    --
    It is cowardly, and a betrayal of whatever it means to be a Jew, to act as a white man

    -James Baldwin