X43-A on to Mach 10 459
Cat_Byte writes "On March 28 we read about the X43-A hitting Mach 7 with a successful scramjet test. Prior to that on June 2, 2001 the craft tore itself to pieces during a trial run. Well now they are preparing to hit Mach 10. The upcoming Mach 10 run of the X-43A appears to mark an end of the program. The seven-year, approximately $250 million Hyper-X program was created to provide unique "first time" data on hypersonic air-breathing engine technologies.
"At Mach 7, the front leading edge of the vehicle would see about 2,400 degrees Fahrenheit. At Mach 10, its probably twice that -- twice the heat load essentially," Sitz explained
FYI, Mach 10 is about 2 miles per second."
Mach 10? (Score:4, Funny)
Wait, maybe I'm thinking of something else...
Re:Mach 10? (Score:5, Funny)
Re:Mach 10? (Score:4, Funny)
Re:Mach 10? (Score:4, Funny)
No, it's actually the closest, most comfortable shave you can get.
Re:Mach 10? (Score:2)
No, it's actually the closest, most comfortable shave you can get.
Actually, I think its the 5th car Pops Racer built for his son Speed, complete with in trunk seatbelts for Sprittle and Chim Chim...
Re:Mach 10? (Score:2)
It's a razor, dumb ass.
Re:Mach 10? (Score:5, Informative)
FYI, he was referring to the episode of Star Trek Voyager, where they test out the new engine technology on the shuttle. It goes Warp 10 which apparently causes 2 of the characters to "evolve" into gecko-like creatures. another completely ridiculous plot that took place around the time of the episode where they found Amelia Earhart
Re:Mach 10? (Score:3, Funny)
Re:Mach 10? (Score:5, Funny)
Yeah, but they saved a lot of money on car insurance. That came in handy when they found the Chevy... floating in... space.
--
Evan
Re:Mach 10? (Score:5, Funny)
Yes, you're thinking of 88 miles per hour.
Now give me back the keys to my DeLorean, please.
Glad to see it (Score:4, Funny)
I'm impressed (Score:2, Interesting)
I could do my daily commute in 15 seconds. That would be fun.
Re:I'm impressed (Score:5, Funny)
Oh, you can have a commute like that right now. It's the stopping that's the problem.
Stupid Question? (Score:2)
Re:I'm impressed (Score:5, Insightful)
Re:I'm impressed (Score:2)
Imagine going to Neptune and back in 6 minutes.
Re:I'm impressed (Score:3, Informative)
Re:I'm impressed (Score:3, Funny)
Re:I'm impressed (Score:5, Funny)
Re:I'm impressed (Score:5, Funny)
I'm sorry, Fry, but astronomers renamed Uranus in 2620 to end that stupid joke once and for all ...
Re:I'm impressed (Score:5, Funny)
Urectum.
Re:I'm impressed (Score:3, Informative)
Re:I'm impressed (Score:2)
Re:I'm impressed (Score:3, Insightful)
Re:I'm impressed (Score:5, Funny)
Knowing English is not a requirement.
Re:I'm impressed (Score:4, Funny)
Re:I'm impressed (Score:2)
Not for commercial flight (Score:3, Informative)
Guys, commercial flight isn't really the goal. Instead, NASA's Hyper-X program, the six-year, $185 million research endeavor of which the X-43A is a part, is aimed at developing vehicles that can deliver payloads into space much more cheaply than traditional rockets. [edwardwillett.com]
GMD
Re:Not for commercial flight (Score:3, Interesting)
Re:Not for commercial flight (Score:3, Informative)
Uhh... 7 squared is 49 and 10 squared is 100. What's your problem?
Re:I'm impressed (Score:4, Funny)
I thought they killed off Data in the last movie. I guess not.
Re:I'm impressed (Score:4, Funny)
4,800 degrees farenheit.. (Score:2, Funny)
Re:4,800 degrees farenheit.. (Score:3, Interesting)
Re:4,800 degrees farenheit.. (Score:3, Funny)
Re:4,800 degrees farenheit.. (Score:4, Informative)
It would be somewhat more correct to possibly describe something as having twice as much internal energy (heat), because units of heat (joules or BTU's) are quantifiable units. Keep in mind that this still wouldn't lead to twice the temperature on an absolute scale, since the specific heat of virtually anything is variable with temperature - hence, you can't correctly surmise that just because there's twice as much heat then there must be twice as much temperature.
Re:4,800 degrees farenheit.. (Score:2)
Killer? You mean AC that doesn't work?
Anyone... (Score:3, Interesting)
Re:Anyone... (Score:2)
I don't know any reason why it would harm ones body but it sure doesn't sound like it would be good for it.
Re:Anyone... (Score:3, Interesting)
That's actually pretty well known. Rockets have been capable of giving a hellva lot more Gs, and experiments with Jet Pilots have pretty well established human's capacity for acceleration tolerance.
The thrust to weight ratios are interesting, however. A 15-20 to 1 ratio would provide one serious kick in the pants.
Re:Anyone... (Score:3, Insightful)
Re:Anyone... (Score:3, Insightful)
The final craft is supposed to be of a lifting body design. This is to provide as smooth of an airframe as possible. Even the slightest corner or dent could be a potential heat buildup hazard.
Re:Anyone... (Score:5, Informative)
Blinkx? (Score:3, Funny)
Fuel economy? (Score:5, Funny)
Re:Fuel economy? (Score:3, Funny)
And does it run Linux? Just imagine how fast Gentoo will compile on this sucker !
Re:Fuel economy? (Score:3, Informative)
Mach 10? (Score:3, Funny)
Holy crap, they're up to Mach 10 now? I guess I'm going to have to throw my old razors away. You'd think that a razor with 10 blades would be rather unweildy but I sure as hell am not going to let my neighbor Jones beat me in the male-gromming-department! Man, those old Mach 3 blades were already pretty expensive. I hate to see how much this new shit is gonna cost...
GMD
Re:Mach 10? (Score:2, Informative)
Knock yourself out:
Gillette M3Power -- a MACH3 innovation -- is a groundbreaking, powered wet shaving system for men that delivers a totally new shaving experience resulting in Gillette's best shave ever.
M3Power builds on the heritage of MACH3 and combines Gillette's latest and best razor and blade technologies. M3Power outperforms all other blades and razors in closeness, comfort and s
Shave wherever he prefers? (Score:3, Funny)
...features Micro-Power(TM), a gentle pulsing action powered by a Duracell AAA battery.
...allowing a man to shave wherever he prefers.
...and the Duracell AAA battery is easy to insert...
Ugh. Did anyone else get a little creeped out reading some of this shit? They really need to fire whoever came up with stuff like that. Unless they are trying to subliminally market it as something other than a razor.
GMD
Re:Shave wherever he prefers? (Score:3, Funny)
It's so your lady can pleasure herself while she prepared the landing strip...
Re:Mach 10? (Score:5, Funny)
Re:Mach 10? (Score:2)
It's for shaving your face and the rest of your body -- at the same time
Front leading edge.... (Score:4, Funny)
Re:Front leading edge.... (Score:2)
Re:Front leading edge.... (Score:3, Funny)
Let me guess: you shouldn't, because verbing weirds language?
Re:Front leading edge.... (Score:5, Informative)
There's the leading edge of the wings, the horizontal stabilizers, the vertical stabilizer, etc. A combat aicraft might have more leading edges for external hardpoints - really, the front-facing part of any protrusion from the fuselage. Whether the nose/front of the fuselage itself is 'technically' a leading edge or not.
Xentax
Crossing the atlantic (Score:2)
Big deal... (Score:5, Funny)
It's still going to take 4 hours just to get to the airport, check your baggage and get through security.
Re:Big deal... (Score:2)
Re:Big deal... (Score:5, Interesting)
Re:Big deal... (Score:5, Funny)
Hell, I could do this much easier.
Take an ICBM, put a stewardess inside.
Ta da' It's an airplane, not a missle.
Re:Big deal... (Score:4, Informative)
So is mine: There are not supporting facts in the Wired blurb because it's public record [house.gov]. The thing in Wired is a little easier to read.
Re:Big deal... (Score:2)
And that's why supersonic travel is still something of a white elephant. When you have to add two-to-four hours of "overhead" to each end of a trip, reducing your flight time by 75% doesn't really save you that much time.
If it costs five or ten times as much, no one except the stupidly-rich will pay for it. And, of course, if they can't market it to the masses, it will always cost that much.
mach 10 (Score:2, Insightful)
Most children are taught that you can count the seconds between a seeing a lightning strike and hearing a thunderclap and divide by five to determine how far the strike was in miles. This means that the speed of sound (Mach 1) is 5 seconds per mile, i.e., .2 miles per second (.5 km per second, I know...). It should therefore be well known to the same child that Mach 10 (10x the speed of sound) is 2 miles per second.
Re:mach 10 (Score:2, Informative)
So? (Score:2)
Re:mach 10 (Score:2, Insightful)
Hmph, children's games in old unit systems - you know, if the US switched completely to metric (never mind the impossibility of winning old people's hearts and minds), we'd save millions of dollars and avoid funny embarrassments like that Mars Pathfinder nonsense.
Re:mach 10 (Score:3, Funny)
And after all that work I realize that your method is indeed close enough for most people
How soon (Score:3, Funny)
How soon before someone overclocks it to get Mach 11?
Re:How soon (Score:3, Funny)
Just the thing (Score:2, Insightful)
A Third of the Way There... (Score:4, Interesting)
"At Mach 10 -- or 10 times the speed of sound -- the X-43A is traveling at about two miles per second. Thats in the range of 7,500 miles per hour."
Which sounds really impressive until you realize that escape velocity is 25,000 miles per hour and we are less than a third of the way to an air-breathing launch vehicle.
186,000 mi/sec... it's not just a good idea, it's the law!
Re:A Third of the Way There... (Score:3, Informative)
Re:A Third of the Way There... (Score:4, Interesting)
I don't believe air-breathing engines will ever make productive parts of the high-speed boost phase of a satellite launch. Now, something like Pegasus or SpaceShip 1 that uses a low speed air-breathing craft to get above lots of atmosphere, that's a pretty good idea.
Re:A Third of the Way There... (Score:5, Interesting)
This is a HUGE problem in some speed ranges, and it's _trivial_ in others. The neat thing about shock waves is, you get a rapid temperature rise during shock compression. One of the 'tricks' to the design of a scramjet, is to plan out the shock wave pattern in such a manner, the ambient temperature in the vicinity of your fuel injectors, is higher than the ignition point of your fuel. Then the only trick is, getting the system up to the velocities required for ignition to be spontaneous. Standard igniters just wont work in those velocity regimes.
As you suggested in the initial post, the problem of escaping atmosphere is huge for the orbital equation. Aerodynamic drag is 'inconsequential' whilst subsonic, but grows exponentially once you start playing with shock waves. 50% of the atmosphere (by mass) lives below 6,000 meters (18,000 feet) altitude. In the range of 80% lives below 13,000 meters (40,000 feet). The most efficient path out of the atmosphere is to utilize atmospheric lift at subsonic speed until well above these altitudes, to get past most of that sticky stuff called air. The messy problem of all that sticky air living below 40,000 feet really makes a single stage runway to orbit vehicle impractical. Efficient lift and reduced hypersonic drag are diametrically opposed concepts when designing the airframe. For the former, you want large smooth rounded surfaces, for the latter you want sharp edges and zero curves, as curves promote 'lotsa little shocks' and a 'shock fan', whereas an abrupt square corner still produces but a single shock wave.
If you look at modern heavy lift, long range airframes, they tend to all operate most efficiently between 32,000 and 40,000 feet. A 747 loaded to the max cannot climb above 32,000 till it's burned off a chunk of fuel (lower for older models), and then it MUST climb higer to be able to achieve it's maximum range, to take advantage of reduced fuel burns at 36 and 38 thousand. it's not really an accident that the transoceanic airways are 'busy' in the 32 to 38 thousand range, with virtually no traffic below or above those altitudes, except a few big ones in the early stages of step climbs as they burn off fuel. The combination of modern jet engines, and aerodymanic lifting bodies, this is the altitude range that is the 'sweet spot' for fuel efficiency. Aerodymanics prevent them from going higher (atmosphere gets to thin to generate the lift required), and engine efficiencies prevent them from operating lower. It's also not completely co-incidental that these are the tropopause altitudes, where you run into things like jet streams, which can give you a significant 'free ride' enroute. 80's and earlier vintage equipment operates 'at jet stream altitudes' eastbound, and 'just below them' westbound typically. Late 90's vintage equipment is slightly more efficient, so you operate above jet streams rather than below, when going westbound.
There have been many trillions of dollars spent on the engineering required for subsonic heavy lift above the majority of the atmosphere. We've got the point where it's efficient enough to be widely deployed. for a wide deployment of orbital transport, it doesn't make sense to NOT leverage this knowledge/technology base for the lower portion of the flight.
Scramjets are cool, but, they want to operate in the atmosphere, and at velocities that produce problems with the rest of the materials. In theory it's more efficient to not carry your oxidizer like a rocket does, but there's this little 'reality' problem with scramjets. We dont know how to build the tankage to carry the fuel for it, in a manner it wont melt from continued exposure to the hypersonic airstream that's presenting stagnation temperatures in the thousands of degrees (and at those high numbers, doesn't really matter if you are using C, K, or
Previous test aborted... (Score:4, Informative)
I was under the impression that the Pegasus boost missle went out of control so they self-destructed it...not that there was a problem with the X-43.
why is this public knowledge? (Score:4, Interesting)
Re:why is this public knowledge? (Score:5, Insightful)
Re:why is this public knowledge? (Score:3, Interesting)
But can it do... (Score:5, Funny)
Re:But can it do... (Score:4, Funny)
Re:But can it do... (Score:3, Informative)
Re:But can it do... (Score:5, Informative)
It is a true statement that a Parsec is a measure of distance. But that doesn't rule it out as a unit of time. Special Relativity tells us that time and distance units are interchangeable, because the speed of light is a constant value in all reference frames.
So, while I'm sure the original Star Wars quote wasn't meant to delve into the intricacies of modern physics, it certainly isn't technically wrong. Of course, since a Parsec is about 39 years, I certainly wouldn't want to be piloting for that amount of time...
Re:But can it do... (Score:4, Informative)
Oops ... that should have read "... since 12 Parsecs is about 39 years..." You must actually READ your post when you preview it :-)
Re:But can it do... (Score:3, Informative)
Read the Han Solo star wars books for it to make sense.
Mach 10 in the air.... (Score:2, Funny)
eeerh... i hate to say this (Score:5, Informative)
Mach number is the square root of the product of gamma, R, and T. Being:
gamma a propertie of the gas (1.33~1.44 aprox for air),
R the constant of the gas (universal R over Molecular Mass for every kilo
And T is the absolute temperature of the gas;
According to the International Atmosphere model, the temperature of air drops 6.5K every kilometer until you reach 11Km, beyond it remains constant until 22km, where it again rises.
So, if depending of the height (and particular condition of the day and the state of atmosphere) the Mach speed varies
As i haven't seen at what height they are flying, you can calculate yourself the Mach speed if you find the numbers.
So is very probable that they are flying at really great heights where the mach value greatly differs from sea level Mach, what is taught to children, as other poster suggested
Values of temperature of atmosphere can be found looking for ISA model (International Standard Atmosphere)
By the way, i am using SI; so, if you find a table with Farenhait (or whatever it is spelled) you can convert a farenheit degree to kelvin via:
(TF-32)/1.8+273 = kelvin
PD: Sorry for my bad english
Re:eeerh... i hate to say this (Score:5, Informative)
Actually, until you get very high in the atmosphere the speed of sound stays relatively constant compared to the speed of sound at sea level. Pressure and density decrease, but so does temperature.
You can plug in some number in a calculator at
http://www.grc.nasa.gov/WWW/K-12/airplane/sou
The actual ground speed number (assuming no head/tail wind) of travelling at mach 10 at 95,000 feet is 6,777MPH or 1.887 miles per second.
Up until now I, perhaps like most, though that since pressure decreases exponentially with altitude, that the speed of sound must also decrease at some constant, or at least predictable, rate with altitude. This was a real eye opener for me.
How long untill we go plaid? (Score:3, Funny)
Overheard at the press conference... (Score:5, Funny)
Reporter: Oh, I see. And most planes go up to ten?
General Tufnel: Exactly.
Reporter: Does that mean it's faster? Is it any faster?
General Tufnel: Well, it's one faster, isn't it? It's not ten. You see, most pilots, you know, will be flying at ten. You're on ten, all the way up, all the way up, all the way up, you're on ten on your airspeed. Where can you go from there? Where?
Reporter: I don't know.
General Tufnel: Nowhere. Exactly. What we do is, if we need that extra push over the cliff, you know what we do?
Reporter: Put it up to eleven.
General Tufnel: Eleven. Exactly. One faster.
Reporter: Why don't you just make ten faster and make ten be the top number and make that a little faster?
General Tufnel: [Pause] These go to eleven.
Oh jeeze (Score:5, Funny)
How in the world did the goatse.cx guy convince Taco to post that caption?
Correction (Score:4, Informative)
Actually, it's the rocket launcher that veered out of control.
A plane takes the rocket+X43 into a given altitude, the rocket launches bringing itself and the X43 to about Mach 3 and then the scram jet can take action, bringing the X43 up to Mach 7 after separation from the rocket.
It's the rocket that failed on the first attempt. Not the X43-A.
Mach Question.... (Score:3, Interesting)
Because if its at traveling altitude, your mach 6 35km altitude vehicle would be faster then your mach 7 15km vehicle (speed of sound is presure dependent).
But if it were otherwise, you could travel at mach 1.1 and still be subsonic if you are high enough, which doesnt make sense either.
So why dont they just give the speed in km/h (or mph)? Mach may be usefull if you are dodging around the speed of sound, but at mach 2,3 (or 10), who cares?
Re:Mach Question.... (Score:3, Informative)
This is useful because the way the medium flows changes significantly at the speed of sound - you have subsonic flow (what airliners fly in), transonic flow (what no one flies in because its ugly), and supersonic flow (what jet fighters fly in). There's also hypersonic flow, but its not as well defined a transition, and has a lot in common with supersonic flow.
Anyway. Mach numbers are useful because they're a similarity number; so much
Naively, it should be x16. (Score:3, Informative)
Re:At that speed.... (Score:2)
How do you figure?
Re:AWESOME! (Score:3, Funny)
Re:Speed for Escaping Earth's Gravity? (Score:3, Informative)
Re:Fahrenheit, some ancient term? (Score:3, Informative)
No, temperature is in degrees Celsius or in Kelvin. There's no such thing as a 'degree Kelvin'.