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NASA Ground Tests Ion Engine

herda05 writes "New Scientist reports from a press release by NASA on a successful ground test of the HiPEP (High Power Electric Propulsion) ion engine, which is the first 'major milestone' for Project Prometheus. Also some pictures and more info on the HiPEP engine."

54 comments

  1. Wow... by Bob+Vila's+Hammer · · Score: 1, Redundant

    "This new class of NEP thrusters will offer substantial performance advantages over the ion engine flown on Deep Space 1 in 1999. Overall improvements include up to a factor of 10 or more in power; a factor of two to three in fuel efficiency; a factor of four to five in grid voltage; a factor of five to eight in thruster lifetime; and a 30 percent improvement in overall thruster efficiency. GRC engineers will continue testing and development of this particular thruster model, culminating in performance tests at full power levels of 25 kilowatts.

    All I have to say is damn!, I'm impressed.

    --


    --"The perfect example of the man of action is the suicide." - William Carlos Williams
  2. Xenon gas? by El · · Score: 2, Informative
    The HiPEP thruster operates by ionizing xenon gas with microwaves.

    Is there really a lot of xenon gas in outer space? Wouldn't ionizing hydrogent work a lot better? And, is it really a vacuum chamber if it's filled with xenon gas?

    --

    "Freedom means freedom for everybody" -- Dick Cheney

    1. Re:Xenon gas? by gl4ss · · Score: 2, Informative

      they take the xenon with them.

      harvesting type of engines/probes are still quite far off afaik so it hardly matters.

      --
      world was created 5 seconds before this post as it is.
    2. Re:Xenon gas? by NanoGator · · Score: 2, Informative

      "And, is it really a vacuum chamber if it's filled with xenon gas?"

      A couple of implications can be drawn here:

      - There is nothing but xenon inside the chamber.
      - There isn't enough xenon in the chamber to generate significant pressure.

      --
      "Derp de derp."
    3. Re:Xenon gas? by CXI · · Score: 3, Informative

      The third inplication is that the chamber is a vacuum and the xenon is stored in a tank and expelled to generate thrust, as in actually the case.

    4. Re:Xenon gas? by saden1 · · Score: 1

      When do I get my Ion Cannon? And how much damage will it be able to do?

      --

      -----
      One is born into aristocracy, but mediocrity can only be achieved through hard work.
    5. Re:Xenon gas? by deglr6328 · · Score: 4, Informative

      what is "hydrogent"? :) The reason Hydrogen is not used and Xenon IS, is because xenon is ~130 times more massive per atom than Hydrogen is. Therefore you'll get much more momentum from accelerating the Xenon out the back of an ion engine at a given speed than you will a Hydrogen atom. And for that matter why stop at Xenon? This guy is working on Bismuth powered Hall thrusters.

      --
      - "Hear that?! The percolations are imminent! Cease your ingress!"
    6. Re:Xenon gas? by kinnell · · Score: 4, Informative
      Therefore you'll get much more momentum from accelerating the Xenon out the back of an ion engine at a given speed than you will a Hydrogen atom

      Close, but...

      The speed isn't a constant for different gasses. What's important, as you point out is momentum.

      Change of momentum = impulse = Force * time.

      The advantage of heavier ions is that they accelerate slower, thus staying within the engine for longer. As a result, the force is applied to the ions for longer, therefore the change in momentum of the ions is higher, therefore, the change in momentum of the vehicle is also higher.

      --
      If I seem short sighted, it is because I stand on the shoulders of midgets
    7. Re:Xenon gas? by Muad'Dave · · Score: 2, Funny


      Oh great! There goes the price of Pepto-Bismol. (Yes, it contains the metal Bismuth).

      --
      Tiller's Rule: Never use a word in written form that you've only heard and never read. You will end up looking foolish.
    8. Re:Xenon gas? by EABird · · Score: 1

      Oh great! There goes the price of Pepto-Bismol. (Yes, it contains the metal Bismuth).

      Oh the irony...

    9. Re:Xenon gas? by theMerovingian · · Score: 1

      Bismuth can also be found on the surface of Venus, although I didn't get modded up for my pepto-bismol reference.

      Yes, I'm bitter.

      --
      "If you think you have things under control, you're not going fast enough." --Mario Andretti
    10. Re:Xenon gas? by Anonymous Coward · · Score: 0

      And how much damage will it be able to do?

      Diddly per shot but it'll hold an unbelievable amount of ammo.

    11. Re:Xenon gas? by IAR80 · · Score: 1

      They have a reservoir of ion gas and also the density of hidrogen in outer space is extremly low something like 1 atom for 10cm^3.

      --
      http://ebgp.net/ccc/
  3. Now all I need... by teridon · · Score: 2, Funny

    is a portable 25-kilowatt reactor. Pluto here I come!

    --
    I hold it, that a little rebellion, now and then, is a good thing. -- Thomas Jefferson
    1. Re:Now all I need... by Aglassis · · Score: 1

      Not hard to find, your car (if you have one) is probably about 100 KWt. Not that that is very useful in space, but 25 KW is still a pretty tiny amount of power generated (down here on Earth). Unfortunately in modern spacecraft, 5 KWe is a large amount of power.

      --
      Suddenly, the hairy finger of a familiar monkey tapped me on the shoulder. It was time.--G. T.
  4. Obligatory TIE Fighter comment by schnits0r · · Score: 2, Funny

    I still want my TIE Fighter.

  5. Xenon tends to explode less often... by bscott · · Score: 1

    As the other respondant said, Xenon is the fuel they take with them. Several obvious reasons spring to mind - it's a bit easier to ionize a gas than, for example, solid propellant... also, it's a lot less volatile than hydrogen. I'm not sure why Xenon was chosen over other inert gases, but it could be because it's the heaviest one (thus more thrust per atom) that is affordable?

    --
    Perfectly Normal Industries
  6. Am I interpreting this correctly? by NanoGator · · Score: 1

    Okay, this isn't exactly my area of expertise, so please forgive me if I'm asking an ignorant question. If they're propelling xenon gas out the back of the engine, then how much do they have to bring aboard? Is that where the x000 seconds of impulse figure comes in? Would the gas come out hot/cold/inbetween? Why'd they choose xenon?

    --
    "Derp de derp."
    1. Re:Am I interpreting this correctly? by SmallFurryCreature · · Score: 4, Informative
      Ion engines are very efficient with their propelant. So yes the longer you want to burn the more you need to carry but it is a fraction of what you would need to carry for a normal rocket engine. ION engines work by constantly burning of a tiny amount of fuel/propelant amazingly effciently. The accelarition is awfull but it can just keep on accelaring for years.

      This I think makes it only usefull for long flights. No tie fighters. Fortuanly real space flight has a lot of long flights.

      --

      MMO Quests are like orgasms:

      You may solo them, I prefer them in a group.

    2. Re:Am I interpreting this correctly? by Leroy_Brown242 · · Score: 2, Insightful

      That's a good point.
      Space is massivly huge. Nothing like Star Treck of Star Wars ever illustrated very well.
      Years and years and years of vast nothing.

      A slow burn over days or weeks would build a pretty good speed though.

    3. Re:Am I interpreting this correctly? by Usquebaugh · · Score: 1

      Your still thinking to small.

      Try millenia ** millenia ** millenia of vast nothing

      A slow burn over a couple of years would be better :-)

    4. Re:Am I interpreting this correctly? by jerde · · Score: 5, Informative

      Ion propulsion works very differently than any other type of normal rocket. The idea with ion engines is that they're able to take individual atoms of their "propellant" and accelerate them to high velocities, using electricity as the energy, rather than some sort of chemical reaction.

      Rockets in space work by taking some mass and throwing it in the opposite direction you want to go. Imagine yourself floating in space holding a bowling ball. You wouldn't have to push the ball away from you very hard to get yourself moving, since it's very heavy. But what if you only had a ping-pong ball: to get yourself moving quickly, you'd have to "throw" the ping-pong ball away from you very very very fast, to make up for its very small mass.

      Chemical rockets take some combination of chemicals that react strongly together, creating heat. The result is a hot gas at high pressure, which blows out in the direction of the rocket nozzle, providing thrust the other direction.

      The xenon ion engine takes xenon gas at very very low pressure, ionizes the atoms so that they're electrically charged, and then uses electric force to fling them at VERY high speed out into space. The velocity is much higher than in any chemical rocket. But ion engines aren't very strong -- the process works with just a little tiny bit of xenon at a time, so the engine as a whole winds up giving just a very gentle push. But since not much xenon is used up, the xenon that you have will last a LONG time.

      That's the "specific impluse": a measure of how much a rocket can push you "per pound" of fuel. This page says that the space shuttle's chemical engines have a specific impulse of 460. This latest ion engine has a specific impulse of 6000!

      So with the same weight of fuel, the ion engine would get you going about 13 times faster by the time you used up the fuel.

      - Peter

      --
      INsigNIFICANT
    5. Re:Am I interpreting this correctly? by NanoGator · · Score: 1

      Thank you. I found that very interesting. :)

      --
      "Derp de derp."
    6. Re:Am I interpreting this correctly? by hubie · · Score: 1

      A nice article on plasma engines can be found here.

    7. Re:Am I interpreting this correctly? by OneOver137 · · Score: 1

      Basically, you figure out how long your mission lifespan is, say 10 years. Double that for a safety factor. You need to know how much propellant you use during normal stationkeeping cycles and add in the estimated number of delta-Vs you'll need to do--a total WAG. These delta-Vs will be for repositionings and collision avoidance, hence the large fudge factor.

  7. Re:Help! parsing the title! by Sayten241 · · Score: 1

    Ground being an adjective modifying "tests". As in "NASA tested it on the ground".

  8. Re:Help! parsing the title! by drakaan · · Score: 2, Informative
    A "ground-test" is a test performed prior to putting the tested item in its normal operating environment (in this case, it's an appropriate description, since it stayed on the ground).

    "NASA Ground-tested an Ion Engine" would have been a less headline-ish way of saying it.

    --
    "Murphy was an optimist" - O'Toole's commentary on Murphy's Law
  9. Re:Help! parsing the title! by embobo · · Score: 1

    "NASA Ground-tests Ion Engine." If I remember my APA style guide correctly, when forming a compound verb the parts should be joined with a hyphen unless the compound word is in the dictionary (i.e., the on-the-fly construction of the compound word is frequent). There are some exceptions to this rule as well, such as the hyphens aren't dropped if doing so would create confusion of the word with another word. It goes on and on...

  10. Very very very low thrust by G4from128k · · Score: 3, Informative

    Before anyone has visions of nimble fighters, we must remember that ion engines have extremely low thrust. A quick calc based on the numbers in the article, which I hope I did correctly, suggests that the thrust is only about 0.3 Newtons (1 ounce for you Imperialists). What makes these engines exciting is that they can sustain that thrust of years. Estimated fuel consumption is only about 14 grams per hour.

    Slow and steady wins the race.

    --
    Two wrongs don't make a right, but three lefts do.
    1. Re:Very very very low thrust by edunbar93 · · Score: 2, Informative

      Actually, what makes this new development exciting is the fact that the ion engine used on the Deep Space 1 probe produced much less than 0.3 Newtons of force... I don't recall the actual thrust, but it was roughly analagous to the amount of force a single piece of paper exerts on your hand if you were to hold it up near the earth's surface. So probably somewhere around 0.01 N. And yet, they were still able to measure the amount of acceleration due to the engine.

      --
      "No problem. I have the capacity to do infinite work so long as you don't mind that my quality approaches zero."-Dilbert
  11. The real impressive engine... by momerath2003 · · Score: 3, Informative

    One of the earlier "nuclear" test engines was this puppy, the nuclear thermal rocket. If you have seen a video of it when it was being tested, you would know that that thing is one mighty beast. The soviets also attempted to design one (both the Soviet and the American versions had the purpose of getting people to mars) which looks a lot cooler. I would love to have a model of that sitting on my desk. :)

    Anyway, this nuclear propulsion is somewhat related to the newer Xenon method albeit with lower specific impulse but much higher acceleration.

    --
    I had but a simple dream, to destroy all humans.
    1. Re:The real impressive engine... by Suidae · · Score: 1

      Great links, thanks for the info.

    2. Re:The real impressive engine... by lommer · · Score: 1

      Hrm, on the first page you linked is states that the NERVA engines acheived thrust-to-weight (TTW) ratios of "three to four". Does this mean it had a TTW ratio of 3:4, or TTW ratios ranging from 3:1 to 4:1?

      If the best TTW ratio they could get was 3:4, that's not very impressive as they would then need an airframe and an atmosphere to provide effective lift, and this is just the engine we're talking about here...

    3. Re:The real impressive engine... by IAR80 · · Score: 1

      There is not much more a man can do on Mars that a probe cannot. Getting man to Mars is just good publicty.

      --
      http://ebgp.net/ccc/
  12. And therein lies the problem by SuperBanana · · Score: 2, Informative
    Now all I need is a portable 25-kilowatt reactor.

    Yep. And considering current "MMRG" units and SRGs(check out their homepage- they're basically two of I-dunno-how-many nuclear-powered generators NASA has at the moment) top out at 100W per module, well...

    I think the problem is that NASA, rightly so, is extremely nervous about putting nuclear stuff into orbit, because of the frequency with which these things blow up. So it tends to be very simple, not very efficient(the MMRG only captures 100 out of 250w produced), and not very powerful. For example, the MMRG modules produce heat just by natural decay, and they're designed to survive a crash as a whole intact(nasa notes that previously they were designed to burn up, but are now designed to stay intact- probably because things don't always get high enough to burn up).

    Problem is, even with solar power- which starts getting pretty sparse(why they came up with the nuclear power sources)- a large(sheet of plywood sized) solar panel isn't much, at least on earth(you get more power outside the earth's atmosphere). It'd take a LOT of that sized solar panels to power such an engine. Probably somewhere above 50 for starters...

    1. Re:And therein lies the problem by datenwolf · · Score: 2, Informative

      I just want to remind you of the "Deep Space 1" probe, which is the very first utilizing a ion drive. The thrust isn't much, but a ion engine can run over a long period, allowing much higher "burnout" velocities, than the chemical rocket engines that are neccesary to launch a rocket.
      And it has a power of only 1kW. IMHO such powerfull engines make most sense at solar swingby manouvers where you've a lot of light energy avaliable.

      On earth it's the best to burn the whole fuel in a very short time(*) but in zero g this doesn't matter.

      * think about, what happens, when you reduce the thrust so much, that the rocket would just levitate. You burn and burn fuel, but don't gain speed. But burning the same fuel in a short time gives you a lot of speed.

    2. Re:And therein lies the problem by confused+one · · Score: 2, Informative

      Actually, it's already been (in) development. DOE's been working on it for a decade and has working prototypes.

    3. Re:And therein lies the problem by Anonymous Coward · · Score: 0

      Do you actually have statistics on the frequency at which rockets carrying nuclear powered cargo blow up? I do believe that stat is currently 0.0000% , which is pretty reliable to me.

    4. Re:And therein lies the problem by penguinoid · · Score: 1

      If they want to put nuclear reactors in space, they might need new safety systems. Systems as on earth will not AFAIK work in space.

      --
      Don't waste your vote! Vote for whoever you want, unless you live in a swing state it won't matter anyways
  13. Cool. by falsification · · Score: 4, Funny
    I always liked ion engines. Back in the star frontiers, when I was a ranger, my commando team would hide in a freighter's hold. Listening to that steady purr of the ion engine made the days before hitting down the warp pass quickly by. We played jimble-jack, and 3-D chess, sure, but mostly you just sat on your ass on a crate smoking sourweed. It was kind of rough, because one of my comrades was a Vrusk, and the other was a Yazirian. They didn't like one another. Plus, the male and female Dralasites kept humping. It got to smell pretty bad in that hold. Eventually, we unwarped. We sneaked up to a Sathar and pirate base. They thought we were just smugglers, but they wouldn't have, except for that ion engine. Old, but reliable. We lost a lot of men that day, dammit all. And the Vrusk. Had to mercy kill him with a laser pistol. It was worth it, though. Disabled their chemical rocket system. We killed or captured the entire lot of bad guys. There was dead worm everywhere. The vibroblade was whirring that day, I'll tell you. It was beautiful. At that point, the base was about to fall into an event horizon, but with our trusty ion engine freighter, we got out of there, right before a dual star system was sucked into the black hole, which created a supernova.

    Those were the days.

  14. Re:Help! parsing the title! by coolmacdude · · Score: 1

    Hah, when I first scanned it quickly I thought it said Ion Cannon.

    --

    -You may license this sig for only $6.99.
  15. So..... by FinestLittleSpace · · Score: 2, Interesting

    .... can someone actually tell me what potential application this has... i.e. how far it'll get a rocket.... will it just be a quicker trip to mars for probes or are we looking at something which could send probes out the solar system and beyond...? If so... how long will/would it take to get to amrs, and simiarly, are we anywhere near reaching the nearest star after the sun? :)

  16. Question? by Richard+Allen · · Score: 0

    Does anyone know the feasability of using a gas engine to get the vehicle started at a faster pace that what the ion engine would begin with? Then, unload the standard engine once it is empty and kick on the ion for the remainder of the trip. Would that initial boost get it to it's distant destination quicker?

  17. Re: Wait a minute! by Anonymous Coward · · Score: 0

    If I remember my 25th century history lessons correctly, Dralasites and Vrusk are essentially the same species. The Vrusk were erroneously renamed by pioneers from Lotar who didn't know of the Dralasites and gave the Vrusk that name from the moon they inhabited. I could be wrong.
    And oh yes, the many hours of jimble-jack. I really miss those tournaments on Senwan 4! That place reeked of sourweed!

    Good times. Good times.

  18. Xenon happens to be a fission product... by That's+Mister+Jesus · · Score: 1

    ...which may mean you could produce more Xenon in space if they can come up with a way to get the xenon out of the fuel rods. This assumes, of course, that any real ion engines will be nuclear powered - which of course they will.

  19. Nuclear power in space by dido · · Score: 2, Insightful

    What they really should be doing is coupling ion engines to nuclear reactors. Then you'd have a power plant capable of producing a large quantity of energy for a long time, and keep going for many, many years.

    I remember reading somewhere that nuclear-powered ships could keep going and going for 20+ years or more. The only reason why such nuclear aircraft carriers eventually must return to port is other supplies like food and water for the crew, not fuel. Same thing goes for ballistic missile submarines, which can stay submerged for years on end, using the power from the nuclear reactor to produce drinkable water and breathable air for the crew. A typical deterrence patrol for an Ohio class SSBN only lasts for two months only because that's probably how long a crew can stay cooped up in a very small space without going crazy. :)

    Only thing is there are all these groups that seem to be afraid to put anything nuclear in space for some reason. If anyone's still really serious about doing manned space exploration, we'll have to do this eventually, I think. Solar just won't be able to produce the kind of power required to provide extended life support and reasonably fast travel at the same time. It's no good to be cooped up in a space capsule for eight months to get to Mars, and back again... These ion engines could probably produce a lot more thrust with the kind of juice a nuclear reactor onboard could put out, possibly even enough to accelerate the ions to relativistic velocities, and then we could have some real serious speed, to make interstellar travel, at least by machines, a realistic possibility.

    As for radiation shielding, that's something you'll have to deal with anyway, nuclear reactor or not. Even a small coronal mass ejection could produce far, far more radiation than the power plant would.

    --
    Qu'on me donne six lignes écrites de la main du plus honnête homme, j'y trouverai de quoi le faire pendre.
    1. Re:Nuclear power in space by IAR80 · · Score: 1

      The main concern with nuclear powered spacecraft is not putting nuclear waste material in space but a lanch gone wrong.

      --
      http://ebgp.net/ccc/
  20. Spy Magazine take on Star Trek by Latent+Heat · · Score: 1
    I thought someone (Spy?, National Lampoon) had a "realistic" Star Trek where Kirk was retiring to his wardroom for periods of months or years and telling Sulu to notify him when they got to anywhere.

    One of my big disappointments with the name "Trek" was my initial belief that it would be a trek, that the ship would require long times to reach interesting destinations after the fashion of old West wagon trains, but with the warp drive zooming around to encounter aliens at every corner was kind of a cheat.

    Oh, and the episode with the Romulan cloaked ship that was destroying Federation outposts was a direct ripoff of a WW-II film about a German U-boat and an American destroyer in a deadly cat-and-mouse game, and it had pretty much the same dialog about the U-boat captain admiring his destroyer captain enemy about his intuition as to where to lay down depth charges.

  21. Re:Help! parsing the title! by Latent+Heat · · Score: 1
    I never quite mastered the hyphen rule, but I think the hypens join together a compound adjective, for example, half-assed. The reason half-assed is hypenated is that if I am making a half-assed argument, I am not making a half argument or an assed argument: the adjective only has meaning as an adjective (modifier or describer of a noun) if it is presented as the whole half-assed.

    Now the work cluster f*ck is not hyphenated because it is a compound noun: while f*ck is normally a verb, it is used here as a noun.

  22. Next step the "grape drive" .... by rgclark · · Score: 1

    From: Robert Clark (rgclark@my-deja.com) Subject: Microwave powered ion drive. Newsgroups: sci.astro, sci.physics, sci.space.policy Date: 2000/07/30 Found this site while looking up info on microwaves: Physics inside a Microwave Oven http://home.earthlink.net/~marutgers/fun/microwave /microwave.html One of the demonstrations on this page appears to show plasmas being generated by heating grapes with a microwave oven. Nice Quicktime movies here. It's also described on the page: HOW THINGS WORK: Microwave Ovens http://rabi.phys.virginia.edu/HTW//microwave_ovens .html Would this provide a low energy means of creating the plasma required for ion engines? One means of creating the required plasma is by irradiating the propellent gas with intense laser or x-ray beams to strip off the electrons of the atoms of the gas, producing an ionized plasma. However, these are both high-frequency forms of EM radiation and therefore require high energy to produce. Microwaves being longer wavelengths require less energy to produce. Another means that is actually used for the Deep Space 1 probe is to use electrons emitted by a cathode to irradiate the gas, ionizing it. How does the energy requirement for the heating element of a cathode compare to the energy requirement for producing the microwaves? If this can be exploited as a low energy means of producing plasmas then this might be used not only for low thrust engines as on DS 1 but also for lauching ships into space by beaming the microwaves into a reaction chamber of a rocket lined with, er, grapes. -- ________________________________________________ "In order for a scientific revolution to occur, most scientists have to be wrong" -- Bob Clark ________________________________________________ Another recent story discusses the applications of using cold plasmas: Force Fields and 'Plasma' Shields Get Closer to Reality, http://www.space.com/businesstechnology/technology /cold_plasma_000724.html An advantage of the cold plasmas is the low power required to generate them. However the article mentions that hot plasmas can be generated with higher densities. Perhaps the microwave plasma generation method can match the efficiency of the cold generation system while allowing the high densities of the hot plasmas. From: Robert Clark (rgregoryclark@yahoo.com) Subject: Plasma propulsion for access to space? Newsgroups: sci.astro, sci.physics, sci.space.policy, rec.arts.sf.science Date: 2002-11-05 21:21:09 PST http://groups.google.com/groups?th=87680963df54e46 c Bob Clark

  23. Re:Help! parsing the title! by smari · · Score: 1

    Lucky for all humanity, APA = American Psychology Association. For one, most people aren't American. Second of all, NASA folks' are Scientists, not Psychologists (thank heavens), and thirdly: The APA Style really sucks.

    Psychology is a science, of course.. but it doesn't matter. The APA rules are evil.