New Ion Engine Being Tested
Dr Cool writes "A new design of spacecraft ion engine has been tested by the European Space Agency which dramatically improves performance over present thrusters and marks a major step forward in space propulsion capability. Ion engines are a form of electric propulsion and work by accelerating a beam of positively charged particles (or ions) away from the spacecraft using an electric field. ESA is currently using electric propulsion on its Moon mission, SMART-1. The new engine is over ten times more fuel efficient than the one used on SMART-1."
Ion engines are high impulse, low torque, so they are appropriate only once your already IN space. even then, there is extremely slow acceleration. I think the construction of a space elevator http://en.wikipedia.org/wiki/Space_Elevator would be a much greater step towards "casual" space flight. even so, very cool.
Fascism is the greatest political ideology ever conceived. Sorry.
Comment removed based on user account deletion
Look, we still can't go faster than light, ok guys?
I remember reading about Deep Space 1 and it's Ion engine about 8 years ago. I was most impressed that the thrust is about that felt on your hand by a piece of paper when held on Earth. The key is that it accelerates the ship to a speed much greater than traditional rockets, not how quickly it does that. Besides, you don't want to go from 0 to 60 in .058 seconds, unless you want to be a smear on the bulkhead.
Saskboy's blog is good. 9 out of 10 dentists agree.
throw that sucker on a generation ship and head out to colonize.
You Know You Are A Geek when a /. story with the name "New Ion Engine Being Tested" makes you nearly drop the beer and wonder how a defunct game company is producing new engines.
:p
Nonetheless, I blame John Romero for my own confusion and/or angst, because it makes me feel better.
Ion engines are a form of electric propulsion and work by accelerating a beam of positively charged particles (or ions) away from the spacecraft using an electric field.
Cool. So can I put one on my Hummer and drive in the Carpool lane with all those Priuses?
The theory of relativity doesn't work right in Arkansas.
The space elevator is not a trans panetary propulsion system. I think they're both good ideas for the intented usage of thier makers.
This innovation came from the addition of another grid (from TFA) used in the process of accelerating the ions. Is there any reason that they couldn't just keep adding grids with varying voltages? And why are the last two voltages both low? Wouldn't it make sense to alternate them?
The test model achieved voltage differences as high as 30kV and produced an ion exhaust plume that travelled at 210,000 m/s, over four times faster than state-of-the-art ion engine designs achieve. This makes it four times more fuel efficient, and also enables an engine design which is many times more compact than present thrusters, allowing the design to be scaled up in size to operate at high power and thrust.
Since KE=(mv^2)/2, wouldn't an ion engine with over four times the exhaust velocity have over 16 times the efficiency, all other factors being equal? And wouldn't an increase in ion KE produce a proportional increase in the erosion rate of the dual low-voltage grids, along with a concomitant shortening of the engine's usable service life?
One step closer to my TIE Fighter.
I am so creative, look at my cry for attention in my sig.
Think momentum, not energy.
I've got a bad attitude and karma to burn. Go ahead. Mod me down.
...the one described in this earlier slashdot story? If so, it looks like they've progressed from concept to prototype.
I thought, when I saw it, that we needed to build a lot of spaceships with two of these, and we would be well on our way to interstellar empire. Just as geeky, I guess, but in a different way.
That's neat! Now if we could hook up two of these babies together, and perhaps add solar panels for additional power, we'd get space craft with twin ion engines. Hrm. Twin ion engines... where have I seen that before?
if this ion engine is any more efficient than the one posted on Slashdot last month. Let me check... nope!
It's simply amazing how many posts get duplicated on this site... it must be part of a plan to drive that advertising revenue stream up a little more.
Bill
It's my Sig and you can't have it. Mine! All Mine!
Thanks, ArcSecond, that makes sense. But we still use KE to calculate how quickly the plasma stream will erode the low-voltage grids, right?
Yup - just stinks. Mod this to funny please.
The real question is; do the Europeans have a 'Flux Capacitor'?
In fact, these would be quite complimentary technologies. Ion drive is pretty much worthless for exiting any kind of gravity well (such as launching from earth) and a space elevator only really gets you as far as orbit. Take the space elevator to orbit, use a little bit of conventional thrust to get out of orbit, then fire up the ion drives and eventually hop to the next planet, where your reverse the process.
I'll never make that mistake again, reading the experts' opinions. - Feynman
You think we won't use this to build a fleet of TIE fighters? They could remake Star Wars a third time, but it would be "right here, right now" rather than "A long time ago in a galaxy far, far away."
How are sites slashdotted when nobody reads TFAs?
'the good old US of A is putting proven and effective technology into getting back to the moon. '
This is Europe and Australia putting technology into space. US space technology these days is either space based spying on the world or spin from the Whitehouse.
Whether this is efficient to do depends on the speed of the ions. As the velocity of the ions increases, the mass increases and therefore the energy required to achieve the same level of acceleration also increases. Of course, the grids have mass, as does the energy source, so you increase the amount of force needed to achieve the same acceleration.
The ESA are a lot of things - many of them unprintable - but I am prepared to believe they're smart enough to have done studies on multi-stage accelerators as most European physicists have worked on them. (Many particle accelerators in Europe were of this kind, at one point.) If they're only using one grid for acceleration, there's a good chance they'll have crunched the numbers and decided that a single grid was the best bet.
Unfortunately, politics in European space research is (almost) as bad as in NASA, so it cannot be automatically assumed that the solution adopted actually is the option the engineers and ion engine scientists would have preferred. For that reason, I would certainly encourage anyone who knows the science to offer up guesstimates on what different configurations would be like. I would ALSO encourage CmdrTaco and the Slashdot team to see if they can pester someone at the ESA into giving an interview.
It's a small world and it smells funny; I'd buy another if it wasn't for the money; Take back what I paid (SoM)
Now, according to the present thread of discussion, the European space agency is developing a new ion engine. In essence, we are talking about an impulse-powered engine.
Warp engines. Impulse power. Hmmm.
So, when do we make "first contact" with the Vulcans?
Now, according to the present thread of discussion, the European space agency is developing a new ion engine. In essence, we are talking about an impulse-powered engine.
Warp engines. Impulse power. Hmmm.
So, when do we make "first contact" with the Vulcans?
TIE fighters are just short range fighters.
Mode (3) smart-aleck mode. Press * to return to main menu.
ESA is currently using electric propulsion on its Moon mission, SMART-1. The new engine is over ten times more fuel efficient than the one used on SMART-1."
It seems with there is either a typo, or the mathmatics department of the ESA is outstandingly confident that they will pass all known ways of making nearly perpetual energy, since the engine itself is going to be 10x more feul effecient then the engine used on the mission, which is the first said engine.
That or the Brits are being outstandishly cocky at the US space progam.
~--~
Do not mind the one with the crazy, for he is sane
Way off topic, barely makes sense.
Why not just increase the number of ion engines? If one gives for example a 1 m/s thrust, wouldn't 20 of them combined give a 20 m/s thrust? I know its not that simple, but you will see significant increases in acceleration, I am sure. Put together a platform with 50 of them, slap on a crew compartment and storage spage, and you have your first in-system exploration ship to go gadding about in! I'd probably throw in a nuclear plant for the giant frickin lasers myself (purely to clear debris, naturally ;)), but we could build all that right now...
What he can't kill, he has sex on. Trent.
So while the ESA is desperately trying to generate some positive press to help people forget about their recent failings the good old US of A is putting proven and effective technology into getting back to the moon.
Care to point out some of the recent failure sof ESA?
As a sidenote: the currently only ion drive propulsed moon orbiter is a european one
angel'o'sphere
Cost free eBook I read (by iBook/Kobo/Amazon/ObookO/Gutenberg etc.): "The Green Odyssey" by Philip Jose Farmer.
I'm just happy that new propulsion technologies are being researched. Put an atomic power generator driven by one of this babies and let's take off for Mars.
Xatrix Security - Computer Security news portal
very little acceleartion thus they'd only be able to get a ship to the moon by creating an increasingly eccentric orbit around the earth then eventually transferring to a very eccentric moon orbit and normalizing. Such a process would take a month at least and more realistically 3-6.
How fast will 50 of them get you there?
What he can't kill, he has sex on. Trent.
You *completely* missed the point. This is not about going to the moon, but about going to the end of the solar system and beyond. Ion engines could be far more fuel efficient than chemical engines. The SMART-1 was only a proof of concept.
Now the real problem to be solved is from where to get the electrical power. Solar cells are a no go if you go away from the sun and nuclear power is horribly inefficient.
PS: you should have been modded -1, Jingoistic Moron - but this is slashdot after all. Sigh.
Actually, in many cases you can get where you want to go with little or no thrust at all, simply by riding the elevator up past the altitude of geosynchronous orbit. The higher above that altitude you go, the greater the centrifugal force from being spun around the Earth, so it's just a matter of calculating when to let go of the elevator.
I don't care if it's 90,000 hectares. That lake was not my doing.
Okay, here's a dumb question for you: I've got a pretty good idea what would happen to me if I stood right behind a traditional rocket while it was lit. But what would happen to me if I stood right behind one of these while it was running? Instant death? Intense pain? A refreshing tingly sensation?
I don't care if it's 90,000 hectares. That lake was not my doing.
What if you view the speed you're going at as a 4-dimensional vector with the basic 3 axis of space and the axis of time. That way, speed would (should) be a constant, where, if you accelerate more in the space domain in any direction, your speed in the time domain would decrease. Now, if you could accept that travelling faster than the speed of light is impossible only due to this vector being constant in size, you could accelerate until it is on the other side of the timeplane, thereby allowing you to travel through time.
Didn't think about what paradoxes you'd need, and you'd probably bump into yourself at the moment of turnaround, but aside from that...
No research done whether this could be true, but it's an idea I've been playing with.
I realize these ion engines have a low thrust/acceleration as a tradeoff against their better fuel economy, which means they're really meant for the long-duration missions such as to the outer planets, etc. Yet I wonder if this new ion thruster design, and also the Double Layer Helicon Thruster that was also recently tested, will result in ion engines that could take man to Mars?
It would be nice if upcoming unmanned space missions could put these new ion engines through their paces, to see how much performance we can squeeze out of this technology. Let's see how high they can make the thrust go. I read on the newsgroups that ion engines could one day emulate the VASIMR concept which can achieve a wide variety of thrust characteristics.
Or what about a 2-stage rocket design? Just have a regular chemical rocket first-stage with high thrust to escape the earth's gravity, and then from there use ion engines to power the 2nd-stage.
These ideas have been floating around NASA and the defense industry for years.
Ion engines, yes. Dual-Stage ones? I was under the impression that they were new.So why haven't these engines been put into use?
What are you talking about? Dual-Stage ion engines are just being developed, and conventional ion engines are/were in use both on NASA and ESA probes.As a result the only projects suggested were either unmanned deep space probes
You seem to be implying that unmanned space exploration is useless. It is anything but. If at all, the presence of humans in space is of questionable scientific value.they provide very little acceleartion
If you had RTFA, you'ld have seen that this new technology remedies exactly that problem and woud lend itself for Mars missions.Well... on earth, nothing would happen, as this kind of engine only works in vaccuum... The mean free travel lenght of those ions in air would be meassured in mircrometers...
:D
In vaccuum, you would die rather violently, due to shortage of air....
So i dont think this is a practical concern...
Of course, if you were in a spacesuit, there would be an issue...
The process (hitting an object with high energy noble gas ions) is also used on earth, where to precess is used to alter surfaces of materials. Its called "sputtering", or "plasma etching". So i guess you can get a general idea of what it does... It cant penetrate your spacesuit, but will happily kick layer by layer of atoms from its surface.
If you waited long enough, it would open holes/ect, but it you be very damaging to sensor equipment/solar cells even with short exposures.
Think of a very low power slaver desintegrator from the ringworld novels
HI O WISE PRINCE. WHT TOOK U SO DAM LONG?
They have, check Deep Space 1. NASA's Dawn Mission will also use ion thrusters, and over 100 soviet satellites have used ion thrusters in the past 30 years.
"The way we can tell it's C# instead of Haskell is because it's nine lines instead of two." -- wadler
...and to my TIE Interceptor!
Is anyone even trying anymore? Just because the engine exists doesn't mean anyone will put it to use?
Ion engines are already in use. If these guys have come up with a performance increase then that new development will certainly see use... unless it's prohibitively expensive (unlikely), someone comes up with something better almost immediately (unlikely), or the world ends very soon (also unlikely).
Did you properly read the article? The new higher KE is possible because they managed to reduce the erosional effects.
12,000 seconds Isp? Sheesh. You may need to see a therapist about your specific impulse fetish.
Once you get over ~3000 seconds Isp you don't really need to keep improving it. Who cares if your propellant fraction is 15% or 20% ? As long as it's not over 60% (as is often the case with chemical propulsion) you are doing fine.
Most space probe engineers would gladly trade lower Isp for higher thrust so they don't get too old by the time the vehicle finishes accelerating. Higher *energy* efficiency would probably be welcome, too.
Stop worrying about the risks of nuclear power and start worrying about the risks of not using nuclear power.
Hybrids rarely use the electric engine while cruising on the expressway, and as such will have the same fuel economy as a comprable gasoline-only engine. Diesel cars and motorcycles use much less fuel than conventional vehicles; but not hybrids.
The wheel is turning, but the hamster is dead.
Indeed torque can be a big problem in space, even if you have gyroscopes.
If the propulsion engine has a small offset in thrust wrt the center of mass of the spaceship, this generates torque. The gyroscopes can absorb this by accelerating, but only up to a certain amount (because, obviously, they cannot continue to increase their speed indefinitely).
At that point the gyroscopes must be "unloaded" by firing some appropriate thruster and consuming propellant.
They have a similar problem on the ISS (but there the torque is generated by friction with the upper atmosphere and small gas leaks), where the american gyroscopes must be periodically unloaded firing the russian thrusters, using precious propellant (this, of course, isn't due to a fault in the gyroscopes).
One of the good things of ion engines is that they can very finely tuned to not have pratically any off-center thrust: the Smart-1 spacecraft has almost never had the need to use it's gyroscopes to absorb thrust generated by the ion engine.
And, of course, the torque generated by really big motors (e.g.: Space Shuttle or Ariane 5 main engines) must be corrected by the same engines with a closed-loop control, because there is no way a gyroscope can absorb that much torque.
There's a hidden treasure in Python 3.x: __prepare__()
Very cool stuff, but reading I couldn't help but thinking that this is strikingly similar to pentode/tetrode tubes in ooold electronics. OK, you're dealing with charged particles and not electrons (so I guess more a thyratron than a hard valve), but still, much the same principles are involved, even up to the multiple grids to counteract each problem that comes along. Kinda cool to see this stuff being dredged up again.
You seem to be implying that unmanned space exploration is useless. It is anything but. If at all, the presence of humans in space is of questionable scientific value.
they provide very little acceleartion
Agreed.
.... now there's an idea with potential...
LESS fuel efficient, the fuel is the energy source (solar or nuclear in ion engines case). It's a shitload more mass efficient though...
is that a typo in the article? are they really accelerating their propellant to 70% the speed of light?!?
http://kered.org
Does anyone know how these engines avoid accumulating a net charge over time? If you're emitting a stream of positive ions for a long time, and you're not taking in any negative ions, you would have an increasingly large negative charge. It seems that this would decrease the thrust over time, not to mention electrocuting the vessel upon re-entering an atmosphere.
If you can read this sig, you're too close.
Imagine a day when we actually discover another inhabited planet and incorporate every means of advanced sophisticated propulsion we know to get there, only to approach their planet full-thrust.. backwards! and then deploy parachutes to land...
Practical? Sure. Graceful? No. Awe-inspiring first impression? Nah-uh.
[I have no name!:/]# _
But think about the environmental impact of doing something like that. You are wasting a non-renewable resource that rightly belongs to everyone on Earth. I don't think anyone should be able to do something like that until we are really clear on the impact on Earths like from the rotation slowdown that would happen from this. Even more I think we should impose a ban on any and all fly-by assisted missions.
The velocities theorized by this technology are mind boggling, but wouldn't a collision with a tiny piece of space dust be, for all intents and purposes, completely catastrophic for the vehicle at that speed? A collision with a grain of sand when travelling at 70% of the speed of light would involve a VERY large quantity of kinetic energy. Without some kind of shielding beyond our current technology levels, wouldn't the vehicle would be severely damaged?
http://www.google.com/search?q=esa+failure
One simple rule for its versus it's
> I think we should impose a ban on any and all fly-by assisted missions.
I think you're trying to be funny here...
It still takes the same amount of thrust (or, I should say, just force) to ride the elevator up to geosynchronous orbit as with any other system. The advantage of the elevator is that you don't need to also lift your fuel with you; it's transmitted as electricity through the elevator (or as a laser beam or some other system).
But, a space elevator is definitely not a "free ride" into space. There will always be gravity to overcome, and that takes energy.
"In particular, Aichmann and Nimtz have recently transmitted Mozart's 40th Symphony as frequency modulated microwaves through an 11.4 cm length of barrier wave guide at an FTL group velocity of 4.7 c, receiving audibly recognizable music from the microwave photons that survived their barrier passage. The transit time through the barrier was about 81 picoseconds and was observed to be constant for barriers with widths varying from 4.0 cm to 11.4 cm."
Nimtz is a clever PR guy but a lousy physicist. Every physics undergrad should know that both the group and phase velocity of electromagnetic waves can have arbitrary values and that this doesn't contradict special relativity. The important question is how fast information is being transmitted and for this neither the group nor the phase velocity is suitable.
OS Reviews: Free and Open Source Software
But a fair amount of energy could in theory be recovered on re-entry. Picture a pulley system where a roughly equal mass travels down one side of the elevator while pulling the "launch" cargo up the other side. It realistically wouldn't be a rope, but probably magnetic braking similar to regenerative braking in an automobile or some similar technology, and energy gained from this would supplement the energy needed to lift the cargo going up. This wouldn't exactly be a free ride either due to friction and other inefficiencies, as well as the simple problems with trying to schedule equal loads up and down; but such a system could mitigate part of the energy costs of launch.
I'll never make that mistake again, reading the experts' opinions. - Feynman
No, he raises an important point.
How do you return the rotational energy to the earth? Losing it would be a REALLY BAD THING for the planet. Has anyone done the math on this?
+++ATH0
The earth already is loosing rotaional energy. Quite a bit in fact. It happens naturally. The moon has pretty much lost all its rotational energy.
50 will get you there a little faster, but the extra weight and power requirements put so much overhead on the launch that the cost is not worth it - you can launch the equivalent of a convertible car into orbit for maybe less than 10 million USD these days, but a hummer would cost you maybe 200 million USD.
The efficiency of this engine beats the numbers at small payloads - hence the wide adoption in smaller spacecraft and long-lasting missions. But when you want to get somewhere fast, it is really not an option. This is one reason why geostationary communication satellites are still being carried from low orbit to 36k-km level with old-style rocket fuel carriers, and not ion engines. It would just not be worth the wait, and you can't have your xxx million costing comsat sitting on the slow train for 3 months when it's life expectancy is only 3 years.
Yes I was, glad you got it.
The amount of rotation lost would be so miniscule that it would be almost immeasurable.
The Earth would lose less (much less!) than one second per century from the lost angular momentum due to a Space Elevator.
As the other respondent pointed out, the Moon is sapping much more rotational energy from the Earth than will anything Man does in the forseeable future.
Also, note that the elevator can also gain angular momentum for the Earth by "catching" ships.
The earth has so much rotational energy that we'll make almost no dent in it by launching craft into space with a space elevator. The Earth has about 2 × 10^29 J, I'm now sure what kind of speeds you'd get off the cable, but if you travelled to the very end (probably ~twice geosync unless there's a counterweight), you'd be at an altitude of 70,000km, and a speed of about 5000m/s. That means you'd have 12.5MJ/kg of mass that you sent up. In order to use just 1% of the earth rotational energy you'd have to launch 1.6 x 10^20 kg into space. That's a huge ammount, unless someone feels the need to put australia on Mars I don't think we'll have a problem...
Wait...
Does this get automatically modded down as it proves that I read past the first novel?
Xaotik Designs