X-43A Hits Mach 7
quiggy writes "As previously reported, NASA tested the X-43A yesterday. The results are in, and the scramjet hit Mach 7, setting a new speed record. CNN is also reporting the story, with a note that a similar jet could be tested by the end of the year, hopefully reaching Mach 10."
1 mach = 334 m/s , , ,
:)
10 mach = 3340 m/s = 3.3 km/s
speed of light c = 300 000 km/s
(3 km/s)/(300 000 km/s) = 1/100 000 of c
this engine travelled at aprox 0.00001c !
good work scientists
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#\ @ ? Colonize Mars
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And just how do you keep something going that fast from burning up in the atmosphere?
Life is not for the lazy.
CNN in a poor programming decision IMHO, did not carry any news of this while it was happening. OTOH FoxNews did!! Which supprised the hell out of me. They did ask some expert a few times how this would mean that missiles (in the future) could hit Osama in 15-30 minutes instead of the 4+hours it takes today. But at least they did have someone talking about the technolodgy/science behind this, and actually showed the takeoff, and launch of the plane. Quite nice of them.
Kudos to Fox, to CNN: do a better job, or you will fall further behind FoxNews.
later,
epic
"Im drowning here, and you're describing the water!"
Did anyone notice that the length of flight was 10 seconds? If it carried enough fuel for a sustained flight, it would be more impressive for a mach 7 flight. I realize this is a proof of concept flight.
the trip to london is to short to benefit from a scramjet..
I am the Alpha and the Omega-3
There's an old Airforce saying:
A new plane doesn't make a new engine possible: A new engine makes a new plane possible.
That's why when NASA went for the moon a critical development was the F-1 first stage rocket engine. Capable of 1.5M lbs. of thrust it allowed the Saturn V first stage to be built with only 5 engines. Compare this with the Russian failed manned lunar rocket the N-1 which had 20 engines. They never were able to work all together (vibrational problems) and abandoned it after several launch disasters.
So why is NASA stopping development? (The successor the X-43C will not be flown). Why are we freezing this enabling technology? Are we (under Bush's program) sacrificing everything to plant a flag on Mars and not making space flight practical? It might be worth it if we ever got to Mars but it looks highly doubtful that his proposal is a serious attempt at anything but votes!
Sorry for the (mostly) repost but I really wish we would move "faster" towards developing the technologies towards practical* spaceflight.
*As noted in previous posts, by not carrying the oxygen on board you save a LOT of weight. Remember the reaction is H2 + O = H2O (and energy) and since the atomic weight of oxygen is 16 compared to hydrogen for every kilo of hydrogen you carry you carry EIGHT of oxygen. The weight savings (could be in the millions of pounds) makes up for the turbo-fans/rocket engines you must carry for the takeoff/orbital transition parts of the flight.
- First stage, accelerate vehicle on a long maglev runway. 100% reusable, no fuel carried, speed of about Mach 1 reached.
- Second stage, SCRAM Jet. Reaches about Mach 10. Then detaches and glides back to Earth on automatic. No oxygen carried, only fuel. Efficient and (apart from the fuel) reusable.
- Third stage, rocket. Takes the plane the rest of the way into orbit.
- Fourth stage, ion drive, takes the payload to a different planet (Mars anyone?). This would probably carry the payloads of several launches of a space plane.
Of course, you'll need to build a launcher on the destination planet, if you want to get back. And the SCRAM Jet is not going to be very useful on a planet with a thin atmosphere (but fortunately most such planets have low gravity, so it's less of an issue).I am TheRaven on Soylent News
The artilce that you linked to said
"Paul said although signs so far are positive, it still is too early to say the scramjet experiment succeeded. The scramjet experiment took place during the final few seconds of the flight, which lasted almost 10 minutes."
A quick search with google also did not turn up any reports of confirmed success. Do you have any?
Check this article for details, but apparently they used a 2 stage solid fuel rocket to accelerate the engine to Mach 7.6. Then they did a 6 second test of the scramjet.
Besides, where would they put the bigger tanks? The thing is tiny; and hydrogen is seriously not dense; meaning very little fits into the vehicle.
-WolfWithoutAClause
"Gravity is only a theory, not a fact!"Unfortunately, the drawbacks of airbreathing appear to outweigh the advantages, at least for vehicles intended to put objects into orbit.
The problem is that a scramjet trades a dense propellant (LOX) for more of a low density propellant (LH2). As a result, the propellant tanks on a scramjet vehicle would end up being larger (and heavier) than those on an SSTO rocket with similar payload. LH2 is also much more expensive than LOX, so your propellant costs go up (not that propellant cost is currently important, but your vehicle is also in a more aggressive thermal environment so it to will be more expensive.)
Worse, the effective Isp of a scramjet (after you take into account drag and gravity losses due to its lower acceleration) ends up being little better than the rocket. See Henry Spencer's comment on this.
About the only place scramjets may make sense is in hypersonic cruise missiles. The US military has a scheme for using hydrocarbon fuels, converting these fuels into hydrogen + CO in flight by partial combustion with a portion of the incoming air (that portion is slowed to a stop by a conventional ramjet inlet, with the fuel being used to keep the air relatively cool and the inlet from melting.) The H2 + CO + nitrogen is then injected into a scramjet for complete combustion.
The simulations are probably more precise than getting your hands on the aircraft after flight. In fact, the simulations would not take into account other non-flight stress like hitting the water from that altitude ;)
Nitrogen is far more difficult to dissciate (i.e. seperate the atoms), remember it's a triple bond, while oxygen is only a double bond. You need approximately twice as much energy to seperate a N2 molecule compared to O2.