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Transportation The Military Technology

How We Might Have Scramjets Sooner than Expected 674

loralai writes "Recent breakthroughs in scramjet engines could mean two-hour flights from New York to Tokyo. This technology, decades in the making, could redefine our understanding of air travel and military encounters. 'To put things in context, the world's fastest jet, the Air Force's SR-71 Blackbird spy plane, set a speed record of Mach 3.3 in 1990 when it flew from Los Angeles to Washington, D.C., in just over an hour. That's about the limit for jet engines; the fastest fighter planes barely crack Mach 1.6. Scramjets, on the other hand, can theoretically fly as fast as Mach 15--nearly 10,000 mph.'"
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How We Might Have Scramjets Sooner than Expected

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  • 10000mph! (Score:1, Interesting)

    by Dogers ( 446369 ) on Thursday December 13, 2007 @06:56PM (#21690074)
    But until we get forcefields to protect against bird strikes at 10000mph, don't expect to see it in passenger jets any time soon.
  • by Anonymous Coward on Thursday December 13, 2007 @06:59PM (#21690122)
    F-16 top speed at altitude: Mach 2+
    F-22 top speed at altitude: Mach 2.42 (officially...it's reported it can exceed Mach 4)
    F-18 top speed at altitude: Mach 1.8+

    I actually couldn't find a modern jet fighter that COULDN'T exceed 1.6 (at least within my aforementioned 2 seconds of research)

    Of course, that doesn't diminish the insanity of Mach-15, but still.

    Oh yeah, if you turn, your heart will forcibly exit your body via your anus before exploding. Have fun.
  • Re:SR-71 Blackbird (Score:5, Interesting)

    by Miltazar ( 1100457 ) on Thursday December 13, 2007 @07:01PM (#21690164) Homepage
    Yes, infact I knew someone who use to fly those things and they weren't allowed to fully throttle up. He also said that during normal missions the plane would damage itself when going the faster speeds. Now of course this is all at someones word, so I have no written proof. Also there would be a slight correction, the SR-71 didn't have "normal" jet engines. SR-71 used ramjet engines, scramjets employ similar but much more advanced technology.
  • Re:SR-71 Blackbird (Score:4, Interesting)

    by Fry-kun ( 619632 ) on Thursday December 13, 2007 @07:12PM (#21690340)
    Agreed.
    I've heard stories that imply that the true top speed of SR-71 is somewhere closer to M5 or M8 - as tested "unofficially" by the military sector.
    Most likely such speeds are attainable but not sustainable (fuel runs out, plane breaks in mid-air, ..?).
    Maybe they used some experimental (or nonstandard) fuel -- then again, it may be a bunch of bullshit.

  • Cost? (Score:3, Interesting)

    by Hacksaw ( 3678 ) on Thursday December 13, 2007 @07:12PM (#21690342) Homepage Journal
    Sure, that's cool and stuff, and I'm sure we'll eventually overcome the other technological problems, but the energy is a gigantic factor in this. How much would the fuel cost jump to have a two hour flight from NYC to Tokyo? Would it be worth it? Remember that ten times faster might mean 1000 times more costly!
  • Re:SR-71 Blackbird (Score:5, Interesting)

    by DaedalusHKX ( 660194 ) on Thursday December 13, 2007 @07:14PM (#21690370) Journal
    Of course materials will have to advance further, and not just structural components (which might well strip off the plane or warp at speeds too far past a few Mach) but new fuel mixtures will have to be worked out. This was similar to the requirement to add Cesium to current fighter plane fuel along with a few other rare elements to raise its flash point. Experimental planes blowing up because the fuel overheated or certain electronics received more heat than they could tolerate is nothing new, but the production models will obviously have to have gotten past that point when they roll out :)

    I wager this technology has been near perfected sometime ago, but as with all things, it was probably kept back to be used in case of sagging sales due to rights abuses at airports (Atlas has Shrugged, and it is visible in that people are avoiding airports now because of the downright abusive behaviors of the TSA and federal shock troops there to protect us from incompetent unshaven twits with box cutters and toothpaste.

    Seriously, this will be the carrot on a stick to dissuade people from using other less regulated means of transportation. Obviously L.O.S.T. was ratified recently in Congress to restrict private sea travel... now only warships and those with "permission papers" will be "allowed" to travel, and who knows what else is coming. Free travel is becoming far less so.
  • by Baddas ( 243852 ) on Thursday December 13, 2007 @07:15PM (#21690382) Homepage
    Horses and humans can run 20 miles a day...

    Trains changed it to 400-600 miles a day...

    Cars made it routine to drive 100 miles a day...

    Planes made it routine to fly 3000 miles for a vacation...

    I really can't wait until it's routine to nip out to Luna for a weekend.
  • 2 hours, eh? (Score:3, Interesting)

    by pizzach ( 1011925 ) <pizzachNO@SPAMgmail.com> on Thursday December 13, 2007 @07:16PM (#21690394) Homepage
    Does that 2 hour flight time from New York to Japan include the time to accelerate and slow down from the 10,000 miles an hour speed? Somehow I am skeptical. Speaking of which, I wonder what the ideal acceleration speed is for plane so that it gets to max speed relatively quickly without endangering the health of it's passengers.
  • by EmbeddedJanitor ( 597831 ) on Thursday December 13, 2007 @07:26PM (#21690540)
    Designing a commercial airframe that will survive these speeds and be commercially viable (ie. cheap enough to build and maintain) is a far greater challenge. That definitely won't take "a couple of years".
  • Re:SR-71 Blackbird (Score:5, Interesting)

    by Miltazar ( 1100457 ) on Thursday December 13, 2007 @07:27PM (#21690560) Homepage
    Actually that brings up a good point. I can't believe they're wanting to go faster then the SR-71, or even as fast. It had the problem about its fuel tank sealing up at high speeds, but on the ground it leaked badly. Problem was that they didn't have a material that could seal the tank and still be flexible while not melting off at those high temperatures. Have they solved this problem?

    If not then maybe they want the scramjet because its quiet(er) then the ramjets of old? I know tons about the SR-71, but I haven't really researched much on scramjets beyond the mythological Aurora(fabled successor to SR-71). Does a scramjet produce a less significant sonic boom then a ramjet?
  • by Un pobre guey ( 593801 ) on Thursday December 13, 2007 @07:28PM (#21690566) Homepage
    This article is a member of that old time /. favorite, taking basic physical phenomena and speculating about completely outlandish commercial products or services that they might in principle make possible. Assuming, of course, that all other laws of physics, biology, economics, etc. are suitably suspended.

    Usually they are based on some person's preliminary doctoral research. This time it was based on that perennial nerd baby boomer childhood favorite with a cool name, scramjets.

    Ho hum.

  • Re:SR-71 Blackbird (Score:2, Interesting)

    by Anonymous Coward on Thursday December 13, 2007 @07:30PM (#21690588)
    I met one of the pilots in the early 1990's and he was a scary dude. He was was a complete and total religious fanatic who could not shut up about how the Apocalypse was coming and Jesus would come back to kill all the gays, liberals, and Communists. I half expected him to mention purity of essence! The idea that our government trusted him with one of its most expensive and advanced pieces of hardware really scared me. He did mention though that some parts of the plane actually got stronger when it was flown because it got superheated and fused together. Could of been BS since I'm not a materials expert, but it sounded really cool. He wouldn't say how fast the thing could really go but hinted strongly that it was significantly faster than what people thought.
  • by eagl ( 86459 ) on Thursday December 13, 2007 @07:33PM (#21690636) Journal
    Nothing wrong with turning at those speeds, as long as you remain within basic (and generally well defined) load limits. The speed doesn't really matter very much except in very specific situations (such as uneven transsonic shock wave formation). In general, a 9 G turn at 400 knots is pretty much the same as it is at mach 2.0. Dynamic loads caused by airflow may change, but the ability to maneuver is not necessarily directly tied to speed.

    There are many hazards in high speed flying, but having the plane explode around you from simply turning at high speed is not one of them. There will be restrictions but turning a plane at high speeds is not some mysterious capability we have yet to sort out.

    I know this because I've done it.
  • by Angelwrath ( 125723 ) on Thursday December 13, 2007 @07:33PM (#21690638)
    Gotta love the flight from City A to far-away City B comparisons. Except you need to be going Mach 3+ before Scramjets get past minimal stall speed, and the only way to get to Mach 3 right now is with a rocket-assisted takeoff. The neighbors around airports are going to love that, I'm sure.

    I wonder if Scramjets would increase or decrease condensation trails, which are known to have a dimming and cooling effect on everything below them. Decreasing would mean more sunlight hitting the ground, but also more heat, which would only heat up the Earth at ground level that much more. If it increases, it means more cooling, but also more dimming.

    Interesting times.
  • Re:Amazingly . . . (Score:3, Interesting)

    by Zebra_X ( 13249 ) on Thursday December 13, 2007 @07:38PM (#21690706)
    The operating cost per hour of the SR-71 was about $86,000/hr. Lol
  • by AHumbleOpinion ( 546848 ) on Thursday December 13, 2007 @07:40PM (#21690746) Homepage
    Just too late as we trip over the peak of oil production...

    We are not going to run out of oil. The price of oil will increase and make alternatives feasible. As this occurs the demand for oil will decrease. The rate of consumption will also peak, it just lags production. The question is really when the transition to alternatives will occur and how much pain do we have to feel to get the process started. In short, as we use less oil to go to work and the supermarket, to get food from the farms to the supermarket, ... the more we will have for lubrication, plastics, and exotic high speed transportation. Oil prices skyrocket as demand out paces supply, we switch to alternatives, oil prices crash as supply now out paces demand.
  • Re:SR-71 Blackbird (Score:3, Interesting)

    by protolith ( 619345 ) on Thursday December 13, 2007 @08:17PM (#21691252)
    My old man saw an SR-71 at Reese AFB in Texas in the '70s while he was an Airforce Instructor pilot. He always used to tell me that the pilot was wearing a misson patch that said "SR-71 Mach 5+"

    Growing up I heard that line every time I pointed out that the books all say Mach 3.
  • Re:SR-71 Blackbird (Score:3, Interesting)

    by Sanat ( 702 ) on Thursday December 13, 2007 @09:08PM (#21691776)
    My team saw a YF-12 land at a non regular air base in 1965 or so. The next day we saw it take off and once it cleared the runway then it went straight up until it was out of sight. I was a systems analyst for the minuteman missile system and as so was not an expert on aircraft even though there was a fighter wing and heavy bomber wing stationed at the base. I knew i saw something special that day.

    It was very impressive to watch that aircraft disappear from sight in mere seconds.
  • Re:SR-71 Blackbird (Score:3, Interesting)

    by ILongForDarkness ( 1134931 ) on Thursday December 13, 2007 @09:26PM (#21691976)
    Heat, exactly, at 5+ mach you are at approximately the re-entry speed of the space shuttle (once it has hit the "real atmosphere) so you need to be built like one to survive the heat.

    Also, no doubt time will be saved for long flights, but turning a 2hr hop into a 10 min hop really wouldn't be that useful. You still have to slow down on both sides (which should take considerably longer with a faster plane) wait in turn for a position to take off and land, and have all the normal flight overhead of getting there early and getting your luggage and stuff. That is what did the Concord in, it just simply wasn't worth halfing your flight time which translates into about a 20% savings for short flights, at a price several times that of a normal plane.

    Assuming it could be made affordable, it could cause problems too. If there was less time involved in flying the amount of travel being done (especially for business) could drastically increase. Our airports can barely handle the load they currently have, so if the airplane was available in large numbers, it could still be years before the infrastructure would be available to support it.

  • by cojsl ( 694820 ) on Thursday December 13, 2007 @09:27PM (#21691980) Homepage
    In "Skunk Works" about Lockheed's black projects program- U2, SR-71, F-111, etc (a GREAT read btw) Ben Rich said they found scorched specks on some SR-71 canopies that turned out to be bugs that they figured were lofted to 100,000ft in nuclear tests.
  • Re:SR-71 Blackbird (Score:3, Interesting)

    by FuturePastNow ( 836765 ) on Thursday December 13, 2007 @09:42PM (#21692128)
    Here's an idea (and not a new one): a single-stage-to-orbit vehicle equipped with both scramjets and a rocket engine. If you can get up to 100,000 feet and Mach 6 on scramjet power, wouldn't that dramatically reduce the rocket's fuel requirements for going the rest of the way?
  • Re:SR-71 Blackbird (Score:1, Interesting)

    by Anonymous Coward on Thursday December 13, 2007 @09:57PM (#21692314)
    Mach 6.3 would not be possible. The airframe would not be able to contend with frictional heating at this speed. This isn't merely a materials problem as the aircraft needs a heat sink somewhere. The X-15 handled this with an ablative coating that was burned off during its Mach 6+ flights.

  • Re:SR-71 Blackbird (Score:3, Interesting)

    by tjstork ( 137384 ) <todd.bandrowsky@ ... UGARom minus cat> on Thursday December 13, 2007 @10:04PM (#21692380) Homepage Journal
    a) You met a total nutjob who claimed to be a SR-71 pilot, and you believed him?

    Actually, you want fanatics to be your warriors. Let's call it for what it is, and say, you want people in your military that have the ability to make a game out of hunting other people. This is particularly true in the Air Force, where the whole culture is about a solo hunter out there, going out and bagging his or her prey - either other enemy aircraft, or ground targets.

    Quite often, this will attract those who might also tend to be religious fanatics.
  • Re:SR-71 Blackbird (Score:5, Interesting)

    by Heembo ( 916647 ) on Thursday December 13, 2007 @10:21PM (#21692552) Journal
    I fly all the time. From Hawaii, all over the country for work. I have a scraggly beard and I usually fly in sweat pants and a t-shirt. I look ruffled at best, and often also wear tie died shirt. I have never been hassled by TSA. Never. In fact, TSA is usually really polite and helpful. The trick is, I try to be polite and refrain from asshole behavior. If you are going to start shit with the TSA, then you will have a bad experience. If you act polite, even minimally so, it's a non issue to get through security. And I carry my iPhone with me, which is based off of BSD while not quite linux is still an OSS *nix variant. So I'm cool. ;-)
  • Re:SR-71 Blackbird (Score:3, Interesting)

    by vought ( 160908 ) on Thursday December 13, 2007 @10:43PM (#21692738)

    Have they solved this problem?
    No. When the Air Force re-commissioned some Blackbirds at Edwards briefly a few years ago, they had to go looking to DuPont for the original sealant recipe.
  • Re:SR-71 Blackbird (Score:4, Interesting)

    by ckd ( 72611 ) on Thursday December 13, 2007 @10:43PM (#21692742) Homepage
    This is why Ben Bova wrote a story postulating a supersonic zeppelin that used the Busemann Biplane to avoid sonic booms (reviewed here [tangentonline.com]).
  • Re:Sonic Boom - Bust (Score:3, Interesting)

    by hoofie ( 201045 ) <mickey@MOSCOWmouse.com minus city> on Thursday December 13, 2007 @10:48PM (#21692782)
    One of my wife's relatives was a wind tunnel engineer on Concorde. I also remember seeing an interview with one the senior engineers on Concorde. He pointed out that Concorde was the FIRST in a projected series of supersonic transport aircraft. They had got over all the hard questions [propulsion issues, airframe heating etc. to name many] with Concorde and it would have been possible to scale up the design to larger sizes, assuming the propulsion improvements and efficiences could be developed as well. Concorde B [concordesst.com] was already being considered early on. Note the 10db reduction in takeoff noise.

    After all, if you look at normal transport aircraft [Boeing & Airbus] they have got progressively larger and larger with more powerful but also more fuel efficient engines.

    . That is what has brought the cost of air travel so low. As time passes and Concorde recedes more into the distance, I think it will be seen more and more as a missed opportunity.
  • Re:Sonic Boom - Bust (Score:4, Interesting)

    by Maniakes ( 216039 ) on Thursday December 13, 2007 @10:53PM (#21692824) Journal
    If it had been a Boeing supersonic jet, I'm sure all Americans would have come out of their houses to listen proudly and patriotically to their sonic booms.

    Maybe, but not in Oklahoma City in 1964 [wikipedia.org].
  • by vought ( 160908 ) on Thursday December 13, 2007 @11:11PM (#21692962)

    What happens when you launch ordinance off a missile rail at supersonic speeds?
    Missiles use rocket motors, so they're faster than the airplane. They come off the rails at Mach 2+ and accelerate.

    Air-launched cruise missiles (which use turbine engines) must be launched at subsonic speed, or the turbine won't start.

    I can't say definitively, but I'm pretty sure that all bombs (whether free-fall, precision, guided, or retarded version of either) must be released at subsonic speeds if you want anything resembling accuracy.

    The Hound Dog missile, an early form of cruise missile carried by B-52s, had its own turbine, and there are anecdotal stories of B-52 pilots using the Hound Dogs for supplemental thrust during heavy takeoffs - but I find that hard to believe. The B-52, of course, was high-subsonic in any flight regime. Cross the sound barrier in a dive, and the wings had a nasty habit of coming off.
  • Re:SR-71 Blackbird (Score:5, Interesting)

    by Nefarious Wheel ( 628136 ) * on Friday December 14, 2007 @12:01AM (#21693400) Journal
    Problem was that they didn't have a material that could seal the tank and still be flexible while not melting off at those high temperatures. Have they solved this problem?

    One of the problems they had was dissimilar metals in the airstream, mostly for sensors and plugs -- they had different rates of thermal expansion than the skin. Things that leaked and didn't fit on the ground were designed to fit together quite well at rated speed.

    Heat was definitely a problem. There was at least one reported case where a pilot inadvertently got his helmet welded to the canopy in flight. And while sitting in the spa at the Jokewood in Mountain View a few years back I heard a story of a KC135Q refueling officer having to wait while the SR71 made slow S-turns to keep from stalling, while the skin of the aircraft changed from strawberry red to black. Too hot to refuel until he did.

    "Turn your ECM off please, I can't see you". "ECM is off. You will acquire visual prior to radar".

    Dang what an aircraft. Remember we had this before LBJ outed it in front of Congress. And word had it that one pilot said if they ever needed to break the record again, all they needed was to move the throttle up another notch.

  • Re:SR-71 Blackbird (Score:3, Interesting)

    by Palpitations ( 1092597 ) * on Friday December 14, 2007 @12:32AM (#21693612)
    Given the forces experiences at takeoff on a 747 (roughly .25 g from the reference I found), it would only require about 12 minutes to of constant acceleration to reach mach 5. I think most people could handle 12 minutes of .25 g for getting up to speed and slowing down. Doing some back of the napkin quality math, that means flying to anywhere in the world in less than 4 hours it seems.

    There's a lot to overcome to get to that point. That said, if it's within reach, and if it can be done without major sacrifices when it comes to fuel economy, then it's certainly worthy of the time and effort. Unfortunately you're spot on when it comes to the capacity of airports, and that would be one area that would need drastic improvements if this became commercially viable.

    Disclaimer: I've been drinking, and my numbers could very well be wrong. What I came up with was .25 g = 2.4525 m/s^2. 12 minutes later, that leads to a velocity of around 3,950 mph (a little over mach 5). Using the Google Maps "drill through the earth" thing, I came up with a distance of around 12,250 miles to go from one point to the furthest point possible. Anyway, take this with a grain of salt - mod down if my numbers seem wrong, but please hesitate and make sure this is at least somewhere near correct before you mod up (there's enough blatantly wrong information sitting at +3 to +5 as it is).
  • by spineboy ( 22918 ) on Friday December 14, 2007 @01:50AM (#21694156) Journal
    I work at a major university medical center, and we often take care of pilots (current and retired) with diseases/problems not handled by the base doctors.
    All of them are calm like a brick, not even a flinch when told they had cancer.
    "OK Doc, what do I do next?"

    One of my senior partners who was a flight surgeon told me that that's what all the fighter pilots are like - almost unemotional, even when being shot down. All that stuff on TV, with the pilots screaming "WE'VE BEEN SHOT!!!! MAYDAY MAYDAY!!!" is not at all what these guys are like.

    Yes, I guess the guy could calmly express that he wanted all the gays/commies/people who don't sweep their sidewalk killed, but I don't think that that type of thinking usually lends itself to calmly expressing those thoughts - they usually come at you like a shotgun.
  • by Tired and Emotional ( 750842 ) on Friday December 14, 2007 @07:49AM (#21695902)
    That's amazing. As well as fast it appears to be VTOL. On current planes you have to fly into Narida and then take an almost hour long ride on a fast train to get into Tokyo. So its going to take around 2 hours on a good day to get from landing at the Airport to stepping off the train in the bowels of Tokyo Station.

    Of course, there's a trade-off here. In order to go real fast you have to get real high, and to do that you have to go real fast (or follow a ballistic trajectory, which would require you to drink your Chateau Lafitte through a straw). So perhaps there is an economically feasible envelope up at around Mach 5 and 100,000+ feet - Concorde pretty much demonstrated there was not one at Mach 2 and 60,000 feet and presumably this one will be even more capital intensive.

    What it does for global warming is another question - you might have to only fly them during the day.

  • Re:SR-71 Blackbird (Score:5, Interesting)

    by AndersOSU ( 873247 ) on Friday December 14, 2007 @09:53AM (#21696612)
    I'd like to add that while the SR-71's top speed may technically be classified, but anyone with a photo, a protractor, and a scientific calculator can figure out at least the top design speed.

    When an object like the black bird travels at supersonic speeds, an oblique shock [wikipedia.org] is formed starting at the tip of the plane. The angle that the shock wave forms is proportional to the mach number, and they are related in a relatively simple equation. The faster you go, the tighter the shock.

    It is wise to keep the wingtips inside of the shock, lest they be ripped off. It is logical to assume that the designers would put the wingtips as close to the shock as possible to maximize the wing's area. Therefore, by drawing a triangle from the tip of the plane to the tip of the wings, and measuring the angle, you should have a pretty good first order approximation of the maximum speed of the blackbird. I don't recall the number off the top of my head, but if someone wants to figure it out, the math is pretty simple.
  • Re:SR-71 Blackbird (Score:2, Interesting)

    by DBA Overlord ( 1159947 ) on Friday December 14, 2007 @10:05AM (#21696700)
    Considering the pilot & RSO would warm up their lunch by holding it against the glass of the cockpit windows, I doubt their helmets would stick. The skin of the aircraft did not turn strawberry red and have to do "S" turns waiting to refuel. By the time the aircraft came down from altitude to refuel, it would have cooled down anyway. Or do you thing the tanker flies at 85,ooo feet? LBJ did not "out it". He just named it wrong. It was supposed to be the RS-71. But you are correct about the speed records. My shop would get flight data, and mach 3.3 was not the fastest I personally saw. The greats thing about them was being out on the middle taxi way as they took off. The nose wheel cam up at that point, and you felt like the bones would shake out of your body. Still gives me goose bumps thinking about it.
  • Re:SR-71 Blackbird (Score:3, Interesting)

    by monomania ( 595068 ) on Friday December 14, 2007 @10:12AM (#21696774)

    The last commercial Concorde flight was on 23 October 2003 (source). Therefore it was flying more than two years AFTER 9/1


    Concorde was taken out of service after the crash in France due to a strip of metal on the runway blowing out a tire, the shards of which tire hit the fuselage and punctured the fuel tank, which started a fire, resulting in the horrific crash we've all seen. The components involved (fuel tank lining, tires, etc.) were redesigned and tested, and the initial public flight of the restored service took place on 9/11 (same day as the WTC attack) with a planeload of Concorde executives and employees; the flight went (as planned) halfway across the Atlantic and returned. The following day, as you all know, all comercial flights in the US were grounded. When commercial flights were finally restored weeks, the initial flight to New York was greated by no less an eminence than (Don Juan) Guliani himself, who exhorted the passengers to do one thing while in NYC -- spend a lot of money.

    Reasons for its eventual demise were economic, relating mostly to inefficiencies in the aging technology and marketing model itself (small number of passengers, high expense per passenger, etc.). The airlines had already begun to switch to a strategy of marketing luxury charters (as opposed to depending upon regular commuter traffic) but even this model could not defeat the built in inefficiencies.

    It is easily arguable that the huge economic downturn in the airline industry post-9/11 was a contributing factor to this, but what hobbled supersonic commercial flight to begin with (what made the Concorde a losing economic model, and the Boeing SST a no-go) was the worldwide Luddite reaction to the supersonic boom controversy, which limited the avenue for commercial SST traffic to the route between NY and London/Paris exclusively.

  • Re:SR-71 Blackbird (Score:3, Interesting)

    by prock307 ( 513323 ) <rock.sr71@net> on Friday December 14, 2007 @12:09PM (#21698088) Homepage Journal
    The engine inlet is about Mach 5 if I calculated things correctly and use the assumption that the shock cones will be able to move all the way back out when the shock has been captured on the mouth of the engine inlet.

    This can also be somewhat confirmed by the pilot reports that noted a reduction in fuel burn when they accelerated past Mach 3.2 to evade missiles.

    Now as far as the airframe, that depends on if you want the bow shock to remain clear of the entire airframe, or if you allow it to touch the outer edge of the mouth of the engine inlet. The 3-views I found seem to indicate somewhere just over Mach 4 with 5 a possibility if you let the bow shock reach the edge of the engine inlet.

    I haven't had to make this calculation in about 8 years and I don't have a protractor handy, so I could be off a bit.
  • Re:SR-71 Blackbird (Score:1, Interesting)

    by Anonymous Coward on Friday December 14, 2007 @01:12PM (#21699042)
    The MiG 21bis had a similar moving shock cone in the nose-located inlet. (The cone also housed the radar antenna.) Beside modifying the shockwawe according to speed, the movability also had the important function of decreasing intake area to prevent the inlet from bursting from overpressure. It was a quite fast fighter too, exceeding Mach 2.

    (I served in the minuscule Finnish Air Force when we had 20 MiGs and 40 Saab Drakens before Hornets. The regular staff mechanics, very knowledged and well trained, told me that in test flights in Russia they had modified the cone to travel even further forward and had thus achieved Mach 2.4 consistently without any other modifications; and in one occasion even 2.7 but at that point the intake had popped half its rivets out and the aircraft had been lost. In Finland MiG 21bis was specified at Mach 2.05 to allow all pilots in the prestigious if unofficial international "Mach 2 club".)

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