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Revolutionary Ion Thruster To Be Tested On International Space Station (abc.net.au)

Three Australian researchers have developed "an ion thruster that could replace the current chemical-based rocket propulsion technology, which requires huge volumes of fuel to be loaded onto a spacecraft." Slashdot reader theweatherelectric shares this article from the ABC News: An Australian-designed rocket propulsion system is heading to the International Space Station for a year-long experiment that ultimately could revolutionize space travel. The technology could be used to power a return trip to Mars without refuelling, and use recycled space junk for the fuel... It will be placed in a module outside the ISS, powered, as Dr Neumann describes, by an extension cord from the station. "What we'll be doing with our system is running it for as long as we can, hopefully for the entire year on the space station to measure how much force it's producing for how long."
In the early 2000s "it was basically a machine the size of a fist that spat ions from a very hot plasma ball through a magnetic nozzle at a very high velocity," and the researchers are now hoping to achieve the same effect by recycling the magnesium in space junk.

132 comments

  1. Could be dangerous by LesFerg · · Score: 2, Funny

    Didn't they watch Space 1999? The entire station could suddenly be thrust into an unknown part of the galaxy.

    --
    If I had a DeLorean... I would probably only drive it from time to time.
    1. Re:Could be dangerous by Anonymous Coward · · Score: 1

      Didn't they watch Space 1999?

      Did you? Space 1999 started with an explosion at a nuclear waste dump on the moon.

    2. Re:Could be dangerous by Anonymous Coward · · Score: 1

      That's lots of ions...

  2. Is this the S7 ion thruster? by Anonymous Coward · · Score: 0

    uh huh. thought so

    1. Re:Is this the S7 ion thruster? by Bob_Who · · Score: 1

      I think its Space Porn.

  3. This is the missing piece by 110010001000 · · Score: 2, Funny

    This is the missing piece we need for our colonization of Mars and the planets and beyond. With this and Musk we are well on our way to Mars. We truly live in exciting times!

    1. Re:This is the missing piece by ShooterNeo · · Score: 4, Informative

      No it isn't. TLDR, read atomic rockets, n00b. Or, since you won't be reading it : high specific impulse ion drives have existed in various test forms for years. They are easy to make and they all have high efficiency, albeit some designs are more reliable than others. The problem with all of them is the nasty equation KE = 1/2 m * V^2. That means the higher the exhaust velocity (and thus specific impulse which is the fuel efficiency), energy required goes up with the square of exhaust velocity.

      Plenty of ion thruster designs, including VASIMR, have reasonable energy efficiency. The problem is that you still have to pay the bill even if the efficiency were 100%. You still have to supply as much electrical power as the kinetic energy of the escaping propellant.

      This is a big problem. Even the most exotic nuclear power generator designs anyone has drawn up, the nuclear generator is a heavy ass piece of equipment being propelled by barely any resulting thrust from the ion drive. It means that you might have great specific impulse but trips to Mars still take months. What you need is also high thrust. That's why the best engine for space travel that currently is feasible is still plain old nuclear-thermal. You only get an ISP of about 1000 (compare to 15k for this particular thruster), but you get thousands of times more thrust. You can complete your Mars injection burn in about half an hour instead of having to run the engine for months. That in turn increases efficiency because there is always 1 optimal point to do your engine burns at.

    2. Re:This is the missing piece by dmoen · · Score: 1

      Ion thrusters aren't the best for Mars colonization, because then it takes too long to get to Mars. The trip to Mars is very dangerous, due to space radiation and the effects of microgravity on human health. For actual colonization, as opposed to just an Apollo-like exploration mission, you want to minimize the transit time. In Andy Weir's "The Martian" (he worked out a realistic plan for a Mars mission and did all the math), ion engines are used, but the travel time is 250 days. In Musk's plan, powerful rockets are used, and the travel time is 90 days.

      I agree that nuclear rockets would be even better, if the political problems could be overcome. (Maybe we'll have to mine uranium from the asteroid belts before we have manned, nuclear interplanetary travel. Or maybe China will do it.)

      --
      I have written a truly remarkable program which this sig is too small to contain.
    3. Re:This is the missing piece by Anonymous Coward · · Score: 3, Funny

      Then simply 3D print ion thrusters on Mars and bring Mars closer to the Earth.

      Do I have to do *all* the thinking around here?

    4. Re:This is the missing piece by 110010001000 · · Score: 0

      According to the claims this will help us go to Mars. Are you calling them liars?

    5. Re:This is the missing piece by Anonymous Coward · · Score: 0

      Whoosh.

      Someone didn't notice that they're responding to a troll.

    6. Re:This is the missing piece by 110010001000 · · Score: 1

      Then why do they claim it is for going to Mars? Are they liars?

    7. Re:This is the missing piece by Anonymous Coward · · Score: 0

      The only conceivable use for ion propulsion in colonization is for non-manned supply rockets for which an acceptable voyage duration would be measured in multiple years or decades. In other words, they contribute *nothing* in solving the critical path obstacles which need to be overcome for successful colonization. This article indicates that serious people do envision our future where machines (unmanned/remote systems), spending decades in interplanetary space, explore or possibly (if the economics are there) mine our Solar System. This is, by far, the most rational way forward, when economic and safety priorities are paramount.

    8. Re:This is the missing piece by Ian+Whitchurch · · Score: 3, Insightful

      Nahh, he's saying he's a fan of atomic rocket and he doesnt think anything else has the thrust to do what he wants, and so he does the circular firing squad thing that the space sector has been doing for the last fifty years.

      Even if he is right, there is still a need for non time sensitive cargos of canned goods, metal powders for your advanced manufacturing printers, copper wire and all the other crap colonists will need, and thats where being able to go 'it'll take 500 days and we dont care' becomes important, even if it isnt the ion drives that are taking the humans to Mars they are still helping.

    9. Re:This is the missing piece by ShooterNeo · · Score: 1
    10. Re:This is the missing piece by ShooterNeo · · Score: 1

      Oh, since you probably won't read the whole article, the key paragraph is this :

      "But wait, there’s more. To achieve his much-repeated claim that VASIMR could enable a 39-day one-way transit to Mars, Chang Diaz posits a nuclear reactor system with a power of 200,000 kilowatts and a power-to-mass ratio of 1,000 watts per kilogram. In fact, the largest space nuclear reactor ever built, the Soviet Topaz, had a power of 10 kilowatts and a power-to-mass ratio of 10 watts per kilogram. There is thus no basis whatsoever for believing in the feasibility of Chang Diaz’s fantasy power system."

      What is key about this paragraph is the argument applies to _any_ electric thruster, not just vasimr. All are basically useless for going to Mars.

    11. Re:This is the missing piece by Lumpy · · Score: 2

      100 years of 10 pounds of thrust never stopping, will get you going INSANELY fast in space.

      --
      Do not look at laser with remaining good eye.
    12. Re:This is the missing piece by Anonymous Coward · · Score: 0

      YHBT. DFTT. HTH. HAND.

    13. Re:This is the missing piece by Lumpy · · Score: 1

      Because we will need to send several satellites first. this engine will make those nuclear powered birds able to keep their orbits without carrying a metric buttload of fuel.

      --
      Do not look at laser with remaining good eye.
    14. Re:This is the missing piece by Anonymous Coward · · Score: 0

      Please don't feed the troll.

    15. Re:This is the missing piece by Rei · · Score: 3, Informative

      We know how Zubrin feels about VASIMR. There's also good reason to disagree with him. For example, his nuclear reactor criticism? He himself proposes building a powerful nuclear reactor to power colonies on Mars, so he's not self-consistent. His power density figures aren't anywhere close to realistic. He talks like 50W/kg is some sort of unachievably optimistic goal, when in reality ATK Ultraflex solar arrays already get 150W/kg (and MegaFlex 200W/kg), figures that have been going up significantly with time; high power nuclear designs for future space missions are measured in kilowatts per kilogram. His complaints about the funding that's gone to VASIMR versus other things are unfair, as VASIMR hasn't received all that much funding - certainly not enough to develop a nuclear reactor as he mentions. And nobody is going to develop a power system for VASIMR without having first validated the propulsion system (something Zubrin apparently doesn't want them to do). He tries to portray its various ion drive competitors as better, without mentioning that the primary reason for choosing VASIMR is its high peak thrust levels. Lastly, Zubrin's dismissal of the dangers of in-transit radiation is not shared by most researchers.

      --
      Everybody point at the libertarian and laugh.
    16. Re:This is the missing piece by Rei · · Score: 3, Informative

      It's a stupid comparison that's not to Zubrin's credit. The reason that no powerful space nuclear reactors have been developed is because there hasn't been any demand for them. Nuclear reactor power to weight ratios don't scale up linearly, they scale up vastly higher than linearly. Figures of 1000W/kg aren't just some sort of out-of-a-hat fantasy numbers, they're based on the very real work in the field. More to the point, even solar is already in the low hundreds of watts per kilogram, so again, Zubrin's acting like 10W/kg is the state of the art and 50W/kg overoptimistic is beyond absurd.

      --
      Everybody point at the libertarian and laugh.
    17. Re:This is the missing piece by ShooterNeo · · Score: 2

      1 kw/kg is still a tall order. You end up needing to use things like droplet radiators to even approach a number like that. As it so happens, solar panels are inherently much lighter because they can be a paper thin sheet of layered junctions - you can actually get much higher power/mass with solar than any heat engine nuclear reactor design anyone has drawn up. The only reason it sucks to use a solar-electric spacecraft to go to Mars is the sunlight incidence per square meter plummets to 44% out there.

      In any case, Zubrin is basically correct. You may save on radiation shielding and propellant mass even if you _could_ make a nuclear electric thruster work (and you don't need vasimr - a big array of Hall or MPD or 30 other ways would work) but now you have to launch and run in flight that nasty high power nuclear reactor. He's totally right about that in that you're trading off a simple system (some tanks of propellant and/or a simple nuclear thermal rocket) for whatever exotic system you need for that level of power density.

      He wants to see someone make it to Mars before he personally dies of old age, and nuclear-electric is not the way to accomplish that. This is understandable.

    18. Re:This is the missing piece by ShooterNeo · · Score: 1

      Figures of 1000W/kg aren't just some sort of out-of-a-hat fantasy numbers, they're based on the very real work in the field.

      Care to cite? I've looked fairly extensively for anything on this, and no, everything I read said it was fantasy.

    19. Re:This is the missing piece by Anonymous Coward · · Score: 0

      Yes, building a machine that will work for 100 years with no resources and people around it is perfectly reasonable and doable.

    20. Re:This is the missing piece by Rei · · Score: 1

      There's a nice breakdown here for different technologies, table 1. Keep in mind that they cite things in kg/kW, not kW/kg; you have to have an energy source, energy conversion, and heat rejection mechanism - and if it's manned, a neutron shield (although there's a variety of possibilities beyond a dedicated shield, such as shielding with cargo, propellant, significant distances, etc); and that the conversion efficiency must be accounted for.

      --
      Everybody point at the libertarian and laugh.
    21. Re:This is the missing piece by Rei · · Score: 1

      "Simple" is the last word I would choose to preface "nuclear thermal rocket". ;) ISPs on nuclear thermal aren't that great, and variable-impulse ion propulsion is much more mission profile flexible. And again: he calls for engineering high power nuclear reactors anyway, shipping them to Mars anyway, for things like ISRU - so why not use such a reactor en route, if you're going through the effort to develop one regardless? And contrary to your "before he personally dies of old age" statement, we're much closer to high powered ion-propulsion than we are to nuclear thermal rockets.

      Don't get me wrong, VASIMR isn't my preferred approach... honestly, I'd love to see more effort going into dusty / foggy fission fragment reactors. But I can certainly see how it would be useful for a wide range of missions, and how developing high power sources for space applications is something we need to do regardless.

      --
      Everybody point at the libertarian and laugh.
    22. Re:This is the missing piece by ShooterNeo · · Score: 2

      Ok, so 3 kg / kw electric is 3 times worse than it "needs to be" for a 39 day trip to Mars.

      Terrible. And if I actually look at the chart you linked on page 3, that's solid core fusion (0.15 kg/kWout) + Rankine Heat Engine(.14/kg heat IN) + Neutron Shield(1 per kw HEAT) + single phase radiator, 600 K(.98 kg per kilowatt HEAT).

      I already know this is going to be terrible? Why? Because it's talking about HEAT kilowatts. With 600 K radiator (efficiency is even shittier at higher radiator temperatures, see the laws of thermodynamics for a source), you get maybe 33% efficiency with the Rankine cycle. I can work out the exact numbers if you demand but it's not going to matter.

      so 3 * 0.15 + 3* 0.14 + 3 * 1 + 3*.98.

      6.84 kilograms of heavy ass shit per kilowatt of electric power supply, best case, using conventional nuclear generators. Zubrin was right. You were talking out your rectum. Disagree? Prove it with numbers.

      Sure, you can do a shit ton better with Aneutronic fusion and TWDEC. Direct conversion is 90% efficient so your heat to reject just plummeted. Go ahead and use a droplet radiator at 1000 K. And use the electricity from direct conversion to run the magnets of _another_ fusion engine where it crushes pellets of fusion fuel and the products of the reaction all escape at high velocities out the exhaust. Now we're talking, an engine that gives a respectable ISP and at the same time is lightweight so (relatively) high thrust. But that's far, far future. Scientists haven't even managed to properly contain fusion plasma yet and have only the vaguest napkin sketches of such a device.

    23. Re:This is the missing piece by ShooterNeo · · Score: 3, Interesting

      It's a cylinder. Inside it are rods. The rods have channels in between. There is HEU fuel inside the rods and they are made of high temperature alloys.

      For a practical Mars mission, your spacecraft would have 2-4 NERVA engines, each a little smaller than the last. On earth departure, you eject the rods that block the fuel channels and dampen the reaction. Engine is cold and has never been run at that point. You run the engine until the burn is complete. Then separate the hot radioactive mess of an engine that is melting down because when the propellant flow stops, so does the cooling.

      That's the simplest way to do it. No nuclear power reactor, it's 1 time use. The pumps, radiation shield, and so forth you don't stage separate, you just eject the core and pressure vessel cannister it is. (so it can be extremely light, under a metric ton)

    24. Re:This is the missing piece by Required+Snark · · Score: 0

      And if any of that highly radioactive material ends up on Earth, we'll just store it in your back yard.

      --
      Why is Snark Required?
    25. Re:This is the missing piece by Gavagai80 · · Score: 1

      Voyagers 1&2 are closing in on 40 years, and only their limited power supply will force them to shut down. Granted running an engine that long is likely to be significantly more complex than other instruments.

      --
      This space intentionally left blank
    26. Re:This is the missing piece by eis2718bob · · Score: 2

      If you have an experiment that shows a violation of conservation of momentum, the correct response is to send a grad student down to find out where the mistake is.

      Not hold a press conference and start packing your bags for Proxima.

    27. Re:This is the missing piece by MichaelSmith · · Score: 1

      The problem with all of them is the nasty equation KE = 1/2 m * V^2. That means the higher the exhaust velocity (and thus specific impulse which is the fuel efficiency), energy required goes up with the square of exhaust velocity.

      But thats just your input electrical energy being turned into kinetic energy of the reaction mass, and ultimately the vehicle.The more energy you pile on at that point, the more velocity change you get.

    28. Re:This is the missing piece by ShooterNeo · · Score: 1

      You start the Mars injection burn in high orbit. You end it on a trajectory that will forever remain in solar orbit if no more engine burns are made. The engine is not radioactive when it is put in a rocket and launched, in fact you launch the engine unfueled and launch the fuel sections in separate rockets. Each fuel section would not have enough fuel to form a critical mass, so even in the worst possible accident the damage would be limited.

    29. Re:This is the missing piece by MichaelSmith · · Score: 2

      The big problem with fission -> electric -> ion drive is that your fission reactor needs a cold sink which can absorb its entire power output. To do that you will need a lot of radiating surfaces and associated plumbing. It adds up to a lot of mass, perhaps more than the reactor and shielding.

    30. Re:This is the missing piece by ShooterNeo · · Score: 1

      Yes but the heavier your power generator needs to be. So the higher the ISP, the worse the effective thrust. The worse the thrust, the longer it takes to get somewhere.

    31. Re:This is the missing piece by MichaelSmith · · Score: 1

      Voyagers 1&2 are closing in on 40 years, and only their limited power supply will force them to shut down. Granted running an engine that long is likely to be significantly more complex than other instruments.

      Totally incomparable. My multimeter is as old as my long dead first car.

    32. Re:This is the missing piece by MichaelSmith · · Score: 1

      Well okay but its better overall than liquid fuels and if you want to send a pipeline of supplies to mars, its a good way to do that, while inefficent fast cruise stages take the humans.

    33. Re:This is the missing piece by ShooterNeo · · Score: 1

      That's what I said. _Although_ you could use droplet radiators to reduce that problem hugely.

    34. Re:This is the missing piece by ShooterNeo · · Score: 1

      More or less. Uncrewed nuclear-electric "barges" have the obvious problem that they are technically very complex and if anything goes wrong, there is no crew aboard able to conduct repairs. Also, nuclear reactors meant for space might be extremely expensive, the cost exceeding the cost of a few heavy-lift rocket runs full of fuel. As Mr. Musk has demonstrated, it's entirely possible to launch rockets that are mostly reusable, so the cost of a few swimming pools full of additional propellant might not be as expensive as you would expect.

      You might be able to solve the maintenance problem with semi-autonomous robots that can carry out tasks and even learn, told in general terms what to do from a control station on earth.

    35. Re:This is the missing piece by MichaelSmith · · Score: 1

      But uncrewed solar electric barges are well validated technology. There is one orbiting Ceres right now. With a top up of reaction mass it could keep going for decades.

    36. Re:This is the missing piece by pslytely+psycho · · Score: 2

      Actually I think he is referring to this when he said read atomic rockets. Instant armchair physicist. It is quite interesting and written so that I could follow at least the concepts, although I lack the math to verify its accuracy:
      http://www.projectrho.com/public_html/rocket/engines.php
      I was introduced to it a few days ago after buying the video game Children of a Dead Earth. A space battle game using n-body physics.
      He certainly could of been more eloquent in stating his case, quite unnecessary. As you replied to him, I thought you might find the site of interest.

      --
      Donald Trump, on a crusade to make Nixon look respectable
    37. Re:This is the missing piece by Anonymous Coward · · Score: 1

      Yes, a radio floating in space on inertia alone is exactly the same thing as massive machinery designed to generate power.

      Things are always so simple when Space Nutters/programmers are in the conversation, one wonders how come they haven't colonized Jupiter yet. It's simple, send a 3D printer to the Asteroid Belt, 3D print some terraforming machinery and nuclear space rockets, send all that stuff, and the 3D printer, to Jupiter, and within weeks it'll be just like the Bahamas.

      Simple, and easy to do. It's the government's fault it won't let us do that.

    38. Re:This is the missing piece by Anonymous Coward · · Score: 1

      That's because you are a Luddite who doesn't understand that computers got better, therefore everything gets better.

      Why, the first Boeing 747 flew in 1969 and took 6 hours to cross the Atlantic. My cell phone has more memory than that 1969 plane, therefore it must fly much faster now.

    39. Re:This is the missing piece by Rei · · Score: 1

      Why are you pretending that there were only the technologies that you hand-picked available, when the table actually listed numerous options with a wide range of masses? Why are you pretending that a neutron shield must be inert mass used for nothing other than shielding, and that increased distance between crew and propulsion isn't likewise an option? Why are you pretending that the table doesn't already list conversion efficiency? How close attention did you actually pay to what you were reading?

      --
      Everybody point at the libertarian and laugh.
    40. Re: This is the missing piece by ememisya · · Score: 1

      According to this information (http://memory-alpha.wikia.com/wiki/Ion_propulsion) this technology is 252 years early.

    41. Re:This is the missing piece by Bengie · · Score: 1

      KE scales with the square of the exhaust, but the amount of KE required scales N^2, so the squaring cancels out and you're left with "net-work done scales linearly with the exhaust velocity and logarithmically with the mass of the propellant."

    42. Re:This is the missing piece by tsotha · · Score: 1

      The NERVA engineers were never able to keep the fuel rods from cracking and chipping under thermal stresses and pressures from the reaction mass, making it too unreliable to use in practice (one of the reasons the program was abandoned). It's possible that's a problem that could be addressed, but of all the technologies discussed on this thread nuclear thermal is the one with the highest technical risk. It would be far easier and cheaper to build a nuclear reactor.

    43. Re:This is the missing piece by St.Creed · · Score: 1

      The only reason it sucks to use a solar-electric spacecraft to go to Mars is the sunlight incidence per square meter plummets to 44% out there.

      I know folks are working very hard on space based lasers. They've become a lot more powerful and cheaper over the past decade. Of course, they have to be careful with the wavelength or suddenly they have an orbital weapons platform, rather than a propulsion, but... it could be a nice combination with the solar sails.

      --
      Therefore, by the (faulty) logic you're using, you're just a cow with a keyboard - osu-neko (2604)
    44. Re:This is the missing piece by Anonymous Coward · · Score: 1

      Will this be doable?
      can we have 10 ion thruster vehicles doing Earth Mars round trips until they until they reach a decent speed? then every time we want to send something to Mars send a module with just enough fuel to match speed with whichever one is closer to Earth at that moment and hook to it?
      It would not be easier but I don't thing is beyond our capabilities and the cost expensive at the start will be reduced by multiple uses

    45. Re:This is the missing piece by ShooterNeo · · Score: 1

      Because nothing else on the table exists as a real system.

    46. Re:This is the missing piece by ShooterNeo · · Score: 1

      Unfortunately the math doesn't work out for trips from Earth to Mars. A laser, like any other source of light, is still subject to the 1/r^2 law. The r is the effective radius of the lens, which you can make pretty big, but Earth to Mars is an enormous distance and only a tiny fraction of the energy would hit a solar sail a few kilometers across with a practical mirror you could make in orbit.

    47. Re:This is the missing piece by HiThere · · Score: 1

      Sorry, the missing piece is a closed cycle ecology. Well, nearly closed. This could be important, but it's not crucial as there are other ways of making ion rockets work in near-solar space. But the closed cycle ecology is needed if you want to get people living away from Earth. (i.e., the general category of "flexible ion rocket" is extremely important, this particular gadget is one possible implementation. But even all together without a [nearly] closed cycle ecology you're only facilitating robot exploration.)

      P.S.: when you're talking about a habitat large enough to rotate for gravity, and with a good radiation shield to protect from the sun, you're talking something significantly heavy. Don't expect an ion-rocket of any sort to move you quickly. For an ion rocket 30 pounds of thrust is unbelievably large, and when you apply 30 pounds of thrust to something that masses 1,000 tons you're going to get very slow changes in momentum. (I grabbed "30 pounds" out of the air, but it resonates with some memory I can't identify, a Google search turned up "...the VASIMR has 4 Newtons of thrust (0.9 pounds) with a specif..." http://www.universetoday.com/4...

      --

      I think we've pushed this "anyone can grow up to be president" thing too far.
    48. Re:This is the missing piece by ShooterNeo · · Score: 1

      That's not at all what the articles say on it. It says it was essentially a flight ready technology. A few chips can either be solved by better QC or just determining the probability of failure due to the chips. 0% chance of failure is never possible, any vehicle humans has ever invented has a nonzero chance of failing spontaneously and killing you in use.

    49. Re:This is the missing piece by mcswell · · Score: 1

      Well, just wait ten years for controlled fusion power.

    50. Re:This is the missing piece by mcswell · · Score: 1

      I had a 40 year old electric drill (Oster brand!) that I inherited from my father. It did finally wear out, though, after lots of use. I was kind of glad; it used a cord, and the battery kind is much easier to use.

      Which makes me think--maybe this spacecraft just needs a very long extension cord!

    51. Re:This is the missing piece by ShooterNeo · · Score: 1

      Are you trolling? Of course fusion would be nice, but there's very little reason to think that lightweight, controlled fusion is imminent. It might happen but I wouldn't bet on it.

    52. Re:This is the missing piece by mcswell · · Score: 1

      Not trolling, joking. Controlled nuclear fusion has been ten years off since I was a boy in the 1950s. It's become a trope.

    53. Re:This is the missing piece by ShooterNeo · · Score: 1

      Oh. Sure. I mean it's not totally out there. Obviously you can do it, easy, with a few bits and bobs to make a radiation lens and a wee little nuclear bomb to get the party started. Works great. So doing the same thing, just on a smaller scale with a tiny puff of fusion fuel gas, has always seemed to be right around the corner. If a bomb that weighs under 100 kg can do it on a large scale, why can't you make it happen on a small scale with 100 tons or so of apparatus, including lots of superconducting magnets and capacitors and lasers and whatnot?

      Certainly there's been many attempts and there ARE tiny fusors that work, they just have pathetically low fusion rates.

    54. Re:This is the missing piece by dpidcoe · · Score: 1

      Oh man, I remember when I found that site about 8 years ago and lost about a solid week reading everything I could find in it. I kind of wish I could discover it for the first time again. It sort of ruined the "space sim" genre of games for me (or maybe more accurately: gave me the material I needed to explain why I was always inexplicably disappointed with them). On the plus side, it made a great resource for writing a hard SF short story for some BS english class I had to take, introduced me to some great hard SF books, and got me reading the Freefall webcomic.

    55. Re:This is the missing piece by RockDoctor · · Score: 1

      and got me reading the Freefall webcomic.

      [EXIT STAGE LEFT, not having read Freefall for several weeks.] What are Flo and Co up to?

      --
      Birds are not dinosaur descendants;birds are dinosaurs, for all useful meanings of "birds", "are" and "dinosaurs"
    56. Re:This is the missing piece by lhunath · · Score: 2

      I may come off as terribly ignorant now, but would it not be reasonable to use such an engine for a cheap permanent ferry between Mars and Earth that never stops? It could spend a few years gaining velocity before it gets put into use.

      --
      ``OK, so ten out of ten for style, but minus several million for good thinking, yeah?''
    57. Re:This is the missing piece by Lumpy · · Score: 1

      I have a Multimeter that was new in 1941 and it's currently far more accurate and reliable than anything you can purchase today.

      SO sad that simpson meters are not like they used to be.

      --
      Do not look at laser with remaining good eye.
    58. Re:This is the missing piece by St.Creed · · Score: 2

      Well, these guys (http://www.deepspace.ucsb.edu/projects/directed-energy-interstellar-precursors) seem to think it may work, at least for small packages.

      "As an example, on the eventual upper end, a full scale DE-STAR 4 (50-70 GW) will propel a wafer scale spacecraft with a 1 m laser sail to about 26% the speed of light in about 10 minutes (20 kgo accel), reach Mars (1 AU) in 30 minutes, pass Voyager I in less than 3 days, pass 1,000 AU in 12 days and reach Alpha Centauri in about 20 years. "

      Apart from Mars being 0.52 AU away right now, it would take 15 minutes to pass Mars. Unfortunately, if you want to stop you need to put on the brakes after a few minutes. But still. That said, having an orbiting 50GW laser array over our head might make some nations a tad nervous.

      Original article: https://arxiv.org/ftp/arxiv/pa...

      Here's the calculator: http://www.deepspace.ucsb.edu/...

      A russian billionaire is funding this: http://www.sciencemag.org/news...

      I've a picture of him at the press conference here: http://i33.photobucket.com/alb...

      --
      Therefore, by the (faulty) logic you're using, you're just a cow with a keyboard - osu-neko (2604)
    59. Re:This is the missing piece by tsotha · · Score: 1

      No, it's nowhere near flight ready. The chipping problem isn't caused by bad QC; it's caused by stresses on the rods.

      There's a reason nobody is seriously contemplating use of this technology.

  4. Interview with Dr Neumann by SpaceDave · · Score: 5, Informative

    For those interested, there is a lengthy and interesting interview with Dr Neumann about this on The Space Show. http://thespaceshow.com/show/0...

  5. It Just Can't Be by JimSadler · · Score: 1, Flamebait

    Being totally brainwashed and deliberately misinformed I know for certain that it is absolutely impossible for the French or anyone other than an American to discover or develop anything. That is why it is so critical that we admit no immigrants so that our glorious superiority can not be contaminated by foreign thoughts. Donnie Trump explained that to me.

    1. Re: It Just Can't Be by Anonymous Coward · · Score: 0

      Please die. Thanks!

    2. Re:It Just Can't Be by Anonymous Coward · · Score: 0

      So inside your stupid, lame attempt at snark there is a point that you probably don't recognize.

      How many physicists, engineers, etc. does NASA employee?

      What are the all doing? Really? What the fuck are they doing?

      $18 billion dollars, a roster of world class people and what thruster technology is going up to IIS for testing? Nothing against Australia, but they aren't really a powerhouse in aerospace.

      Is NASA not even interested in such devices? Do they not even try?

    3. Re:It Just Can't Be by NotAPK · · Score: 1

      I haven't worked with NASA, but my experience is that a lot of US academics and technology businesses are very introspective and suffer from major issues with NIH.

    4. Re: It Just Can't Be by Anonymous Coward · · Score: 0

      We also got the first scramjet running too.....with materials found in Lowes.

      Not bad for a population and economy the size of Texas.

    5. Re:It Just Can't Be by Anonymous Coward · · Score: 0

      Donnie Trump explained that to me.

      [sigh] Donnie Dumbf explainered that to me. (and now I need to shower off the rapid spittle)
      TFTFY

  6. Some more information by Ian+Whitchurch · · Score: 5, Insightful

    Hi,

    I'm Ian Whitchurch, the CEO of Neumann Space.

    First of all, if you want more technical information about the Neumann Drive, there's an article in Applied Physics Letters. It may be available here

    http://scitation.aip.org/conte...

    If that isnt working, then you might know someone with an APL subscription, or it might be somewhere on the internets under "A centre-triggered magnesium fuelled cathodic arc thruster uses sublimation to deliver a record high specific impulse Patrick R. C. Neumann, Marcela Bilek and David R. McKenzie".

    Secondly, it's not just the Neumann Drive that's going up to the Bartolomeo platform on the ISS. We're planning on taking a bunch of other peoples small projects, which deserve to go into space, but cant by themselves get a ride into orbit, or an easy method to get power, heating, cooling and communications once they are there. If you're interested, you might want a look at this fine Airbus DS press release.

    https://airbusdefenceandspace....

    There is also information available about the Facility for Australian Space Tests on our website, at http://neumannspace.com/fast/

    Thirdly, Im happy to answer further questions people might have.

    Finally, our poor, poor website. Also, the original post lacks a poll, which itself lacks a Cmdr Taco option. What the heck am I supposed to vote for ?

    1. Re:Some more information by Rei · · Score: 3, Informative

      Thanks for chiming in and linking the paper, and my apologies for exposing yourself to the comment environment here, which has become rather toxic concerning space issues of late. The fact that the press coverage comes across as "hype-y" doesn't help any.

      While I think your premise of using space junk is... let's say "optimistic", in the anywhere-close-to-near-term timeframe.... the engine concept itself seems quite sound and interesting. I can't read the paper (not going to shell out $30 for it... not your fault I know, the publishing world is terrible), but - how sensitive is it to the geometry of the cathode? Is your concept that things would be melted down and cast (or extruded, or any other mechanism) into your desired geometry? I assume that at present you're doing something like feeding in wire off a spool to act as the cathode?

      --
      Everybody point at the libertarian and laugh.
    2. Re:Some more information by Ian+Whitchurch · · Score: 5, Informative

      It's press coverage - it's going to be hypey, and thats just the world we live in. As indeed is toxic comment environments :)

      While running on space junk would be nice, it doesnt need to happen for the drives to be useful. If you're rocking 11 000s of specific impulse, then it's simple enough to bring a shipment of cathodes up from earth, transfer to a SEP tug and take them to where they are needed. The fact they are solid, and therefore dont need to be kept at the correct temperature and pressure helps a lot.

      Cathode geometry is something we need to do more science on. At the moment, we've been working with one inch diameter circular cathodes, and the 'star' erosion pattern appears to be a thing. Yes, we're definitely looking at cast/extruded cathodes. We've got some ideas about how to move cathodes forward, and thats on the 'to do' list for the model thats going up to the ISS.

    3. Re:Some more information by MrKaos · · Score: 1

      Wow - thanks for commenting here and welcome. Please excuse the rude ACs.

      I'm curious about the using space debris as fuel, if I read that right? If magnesium is the top "fuel" can it use something like aluminium and have a lower specific impulse?

      I think Cmdr Taco is jealous of Dr Neumann's beard!

      --
      My ism, it's full of beliefs.
    4. Re:Some more information by Ian+Whitchurch · · Score: 1

      If it's solid and conductive or semiconductive, we can use it.

      That said, Im expecting to find worse power efficiency as well as lower specific impulse from "mixed metal fuel rods" - but if you didnt have to pull it up from the bottom of a gravity well, it might be worthwhile.

    5. Re:Some more information by Anonymous Coward · · Score: 0

      Thanks for your input and the paper links. Superb work, best of luck from all of us spacefreaks!

    6. Re:Some more information by MrKaos · · Score: 1

      thank you, I hope we see these engines buzzing around the solar system, I am fascinated.

      I'd imagine when you have more current you can accelerate faster?

      What about radioactive metals, depleted uranium for example, does the engine behave differently because the fuel is a radio isotope?

      --
      My ism, it's full of beliefs.
    7. Re:Some more information by Anonymous Coward · · Score: 0

      Um, by any chance are you familiar with Ian Brown's development of MEVVA Ion Sources at LBL back in the Eighties? We were getting some rather huge high-charge state pulses with, back then, comparatively long cathode life times. One problem that we had was containing Space Charge and Emittance, which would not be much of an issue here:
      https://www.researchgate.net/publication/3148940_The_metal_vapor_vacuum_ARC_MEVVA_high_current_ion_source

      For the Peanut Gallery, the higher the charge state Q, the higher the accelerated energy of the Beam for given gradients in a LINAC. For Nuclear Physics, the trend these days is to generate as high a Q beam as possible initially. I've gotten 136Xe+27 from an ECRIS routinely two decades ago, and much higher Q is easily achievable these days with VENUS...
      http://cyclotron.lbl.gov/ionsources/venus

  7. Comparison, please by Applehu+Akbar · · Score: 2

    How does the energy input and thrust produced compare to NASA's current operational ion engine, which has been in use on the Dawn mission for the last ten years?

    1. Re:Comparison, please by Ian+Whitchurch · · Score: 5, Informative

      http://descanso.jpl.nasa.gov/S... is as good a summary as any about NASA's current ion engines, while the APL paper by Neumann, Bilek and McKenzie for the http://scitation.aip.org/conte... has information about the Neumann Drive.

      Short version is that xenon drives vary in specific impulse and power efficiency depending on the power levels, while Neumann Drives vary in specific impulse and power efficiency depending on the fuel used, while the power level affects how many pulses per seconds. Higher power levels appear to cause faster wear of the grid in Gridded Ion Thrusters, or the chamber in the case of Hall Effect Thrusters, as well as needing more investment in Power Processing Units and so on. Additionally, there is the issue of tankage, regulators and so on for dealing with the xenon itself, which means it's not a straight 1:1 comparison. That said ...

      TLDR : Magnesium in a Neumann Drive runs about 9 uN/watt and 11 000s specific impulse. A NSTAR running at ~1000 watts input has about 32 uN/watt and 2850s of specific impulse.

    2. Re:Comparison, please by Anonymous Coward · · Score: 0

      Not just the Dawn mission. Ion engines power all sorts of stuff like many of the geosynchronous satellites.

      This seems to be some sort of specialized version that reuses magnesium "space junk". Meh... This will amount to nothing as far as Mars missions and such. There just isn't enough energy there. They are simply recycling energy that has already been spent to make the magnesium pieces they are recycling.

    3. Re:Comparison, please by Zelig · · Score: 3, Interesting

      The Neumann thruster is all about saving launch capacity. Most of the ion thrusters we have now work with e.g. Xenon gas; you have to loft their fuel, and your engine mass budget has to include the material handling for the propellant; tanks, valves, etc.

      The idea of the neumann thruster is that your reaction mass comes from a simple sold puck which is gradually ionized; so you immediately win on a bunch of hardware you don't have to lift.

      And then, you can use as reaction mass the sorts of stuff which is already up there in orbit. Got some excess second stage, which you've lofted to orbit at ruinous cost? Instead of dropping it back into the atmosphere to burn up, melt it into a puck at the focus of some mirrors, and then use it as reaction mass for a few years.

      Space junk turned into valuable fuel. Big win. .... IF it works.

    4. Re:Comparison, please by NEDHead · · Score: 2

      Not fuel, reaction mass

    5. Re:Comparison, please by Anonymous Coward · · Score: 0

      Thank you Captain Pedantic for your valuable contribution to this thread.

  8. Alternative Propulsion by Anonymous Coward · · Score: 0

    Be great if Milner and Zuckerberg would put up the cash or shut up and design a photonic laser thruster for the ISS to test the interstellar "nanocraft" concept before the most expensive object in history / Russian-U.S. peace keeping effigy gets burned up instead of funding studies. Be even better if they also funded a propulsion system like the Magnetic Sail that could slow down on the other end an interstellar journal and not require a laser that threatens the existence of the space capabilities of a nation state and provide justification for starting another arms race.

  9. The main problem is safely grabbing the space junk by Gravis+Zero · · Score: 4, Insightful

    The problem with space junk is less about getting to it and more about getting to it safely. Everything in orbit is travelling a minimum of 17,000 mph. Have you seen what happens when car into a wall at only a 100 mph difference? Think two flimsy satellites colliding with a 400 mph difference. There will be hypersonic shards of metal everywhere.

    --
    Anons need not reply. Questions end with a question mark.
  10. Ion thrusters were invented in 1959 by melted · · Score: 1

    The first use of an ion thruster as the main engine was in 1998 in Deep Space 1. Russians use it quite a bit to correct orbits of some of their satellites. IOW this is not a new technology.

  11. EM Drive -v ION drive = 1st space robot wars by seoras · · Score: 4, Interesting

    I'd like to see an EM Drive put into testing up there too (yes, yes, yes - I know it's defying the [known] laws of science. No reason not to test it in space since it seems to pass all tests on earth)

    Hey maybe we could strap the ION Drive face-to-face with an EM Drive, throw them out the hatch and see who pushes who around!

    1. Re:EM Drive -v ION drive = 1st space robot wars by Ian+Whitchurch · · Score: 1

      *shrug* If they want to be a customer, Im happy to sell them space and give them a power allowance.

    2. Re: EM Drive -v ION drive = 1st space robot wars by chaboud · · Score: 1

      So, knowing nothing about the particulars of an emDrive...

      What would it cost to get a 1kW 50kg half-height fridge a ride-along with you? Is this "ambitious Kickstarter" territory or "have a rich uncle Gates or Bezos" territory?

      What are the primary driving constraints? Size? Weight? Power?

      Thank you again for dropping in on Slashdot to discuss this.

    3. Re: EM Drive -v ION drive = 1st space robot wars by Ian+Whitchurch · · Score: 4, Insightful

      Is this a casual conversation, or are we talking, like *numbers* here ?

      If it's the latter, the 1kW is going to be the biggest constraint - you're asking for a lot of power.

      As far as costs go, I'd say we're looking at 'not especially ambitious' Kickstarter, especially if you're happy for it to not come back, and to cut that power demand down a little.

    4. Re:EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      As much as I intuitively think this is snake-oil, I guess I would like it to be proven too if it doesn't cost too much to try. Breakthroughs in science are usually made by the crack-pots. Lets put this EM drive to the test.

    5. Re:EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      I'd like to see an EM Drive put into testing up there too

      Cannae claim they'll be putting their Cannae Drive on a cubesat within two years to prove that it really does work. They've made the claim and set the timetable so let's see what they actually do (or don't do).

    6. Re:EM Drive -v ION drive = 1st space robot wars by Gavagai80 · · Score: 2

      Name one breakthrough in science which was made by a crackpot -- someone who was dismissed as not being a real scientist, rather than simply considered to be incorrect by fellow scientists.

      --
      This space intentionally left blank
    7. Re: EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      The vacuum tube.

    8. Re:EM Drive -v ION drive = 1st space robot wars by joe_frisch · · Score: 2

      Anyone who wants to fund the experiment is of course free to do so. I'd advise against it though,. The EM drive claims to violate conservation of momenum (4-momentum if you are being picky), under conditions that are not in any way outside the range of typical experiments. The theory, at least as presented in the AIP advances doesn't make any sense at all. The experiments are tricky and easy to get wrong. (the thrust is tiny so forces on cables etc could easily distort the measurement).

      I know the argument about long shots and Pascal's wager, but there are an infinite number of possible experiments, so trying random ones doesn't make sense.

      An earth based measurement with a superconducting cavity (which would allow large fields with very small RF power), would probably be a better / cheaper test.

    9. Re:EM Drive -v ION drive = 1st space robot wars by rubycodez · · Score: 1

      vulcanized rubber - Goodyear was a loon, read his story sometime. wore gooey smelling clothing articles made of rubber his was experimenting with, house had globs of rubber on wall, in kitchen, poisoned himself with his experiments

      AC motor, generation and transmission tech - many of Tesla's ideas just wrong, we use others daily. He was a weirdo

      science of genetics - Mendel was dismissed as crackpot during his life (you know of the monk's S&M cocaine orgies right?), value of his work realized almost two decades after death

      statistical thermodynamics - Boltzman, shamed as crazy guy in life, hung himself. value of work realized after death

    10. Re: EM Drive -v ION drive = 1st space robot wars by rubycodez · · Score: 1

      Fleming wasn't considered crackpot at the time

    11. Re:EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      wicked insinuation of crackpot-ism. Who specifically are you accusing of being a crackpot, and on what basis do you make that accusation?

    12. Re: EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      But Lee De Forest was.

    13. Re:EM Drive -v ION drive = 1st space robot wars by steveha · · Score: 1

      (a) Appeal to authority. Facts are true or they aren't, and the majority opinion of scientists doesn't affect that.

      (b) Catastrophism was proposed by J. Harlen Bretz as an explanation of the geologic features of the Channelled Scablands in Washington state. Basically he mapped out a bunch of geologic features and proposed that they were created by a catastrophic event: the unleashing of a tremendous volume of water that carved out new geologic features in a matter of days.

      He was completely dismissed as a crackpot when he proposed it; not just wrong, but also not qualified to have any opinions on geology. The accepted dogma of the time was that everything in geology takes geologic time, not just most things (a strict form of uniformitarianism). 40 years later, his theories became accepted as correct by the mainstream geology community.

      P.S. The modern view of uniformitarianism in geology is that most of the time things change slowly as they have all along, but sometimes catastrophic events like a megaflood or a volcanic eruption or a meteor impact can have a sudden effect. This just seems like common sense to me, but I guess the strict form of uniformitarianism seemed like common sense in 1923.

      --
      lf(1): it's like ls(1) but sorts filenames by extension, tersely
    14. Re: EM Drive -v ION drive = 1st space robot wars by rubycodez · · Score: 1

      No, he was accused of fraud and patent infringement and poor management.... not being nuts. He received awards for his invention.

      Some of his predictions are funny: "As a growing competitor to the tube amplifier comes now the Bell Laboratories’ transistor, a three-electrode germanium crystal of amazing amplification power, of wheat-grain size and low cost. Yet its frequency limitations, a few hundred kilocycles, and its strict power limitations will never permit its general replacement of the Audion amplifier."

    15. Re: EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      No, he was nuts. He thought a high vacuum would be detrimental to the operation of the triode. He fundamentally misunderstood what he invented.

    16. Re: EM Drive -v ION drive = 1st space robot wars by Tablizer · · Score: 1

      That might be true, but doesn't invalidate the original point.

      Christopher Columbus was also nuts, and a more sane person probably wouldn't take the trip. Serendipity is sometimes fueled by stupidity.

    17. Re:EM Drive -v ION drive = 1st space robot wars by cwsumner · · Score: 1

      Better to test the "EM drive" in space.

      If it turns out to work, and we don't know what is producing the thrust, do you really want the "q-rays" that it produces going through your house?? ;-)

    18. Re: EM Drive -v ION drive = 1st space robot wars by Anonymous Coward · · Score: 0

      1 kW in space isn't that extreme. That's about 1/100th of the ISS solar panels. IOW, you'd need about 2.5 square meters. Won't fit on a cube sat, but you might be able to put it on a secondary payload for another launch (especially since the orbit is a don't care) Ballpark figure: $5M-10M.

  12. Don't give it to SpaceX!! by Anonymous Coward · · Score: 0

    Don't give this to SpaceX if you want it to actually make it to orbit!

  13. Re:The main problem is safely grabbing the space j by Anonymous Coward · · Score: 0

    ... There will be hypersonic shards of metal everywhere.

    Um, I know this may be a dumb question, but I'm trying to get a handle on how fast those shards would be going.

    So, what's the speed of sound in space?

    Thanks,

    P. Edant.

  14. ObPlanetes by Anonymous Coward · · Score: 0

    yeah yeah

  15. Probably just making a point by Okian+Warrior · · Score: 2

    ... There will be hypersonic shards of metal everywhere.

    Um, I know this may be a dumb question, but I'm trying to get a handle on how fast those shards would be going.

    So, what's the speed of sound in space?

    Thanks,

    P. Edant.

    The speed of sound is dependent on temperature, but doesn't vary all that much - 1200 km/h to 1000 km/h at about -60 C.

    Once you get to vacuum, "the mean free path" of the particles becomes so long that the atmosphere begins to act less like a gas and more like individual particles. Changes in pressure are not propagated efficiently in this situation, so the idea of "sound" starts to lose its meaning.

    I think the OP was just making a visceral point. If we use the sea-level 1200 km/h speed and note that orbital velocity is about 28000 km/h then depending on the angle the shards could hit anywhere from 0 to twice the orbital speed.

    A 1 gram bolt hitting the front of your spaceship at 28000 x 2 = 56000 km/h would deliver an energy of 121,000 joules on impact (if I did the calculations right), equivalent to about 25 grams of TNT.

    Roughly 1000 times impact of a sledge hammer. (10 kg hammer going 5 m/s => 125 joules).

    1. Re:Probably just making a point by Anonymous Coward · · Score: 0

      The speed of sound is dependent on temperature...

      No, it depends on density.

  16. Last link by nitehawk214 · · Score: 1

    The last link says something about recycling space junk but it is just a link the wiki page on ion thrusters.

    Is there an actual article about this and is there research in this area?

    --
    I'm a good cook. I'm a fantastic eater. - Steven Brust
    1. Re:Last link by Ian+Whitchurch · · Score: 1

      Personally, I'd start by looking at the work on solar furnaces and space manufacturing.

  17. Twin Ion Engine by Anonymous Coward · · Score: 0

    Star Wars, here we come!

    1. Re:Twin Ion Engine by Anonymous Coward · · Score: 0

      One thing you could do with a reactor in space that you can't do on the ground is use distance for your shielding. Put the engine and reactor at the front end of several k's of rope, angle the exhausts and simply use distance as shielding rather than lead. Radiation flux will be falling off as the cube of distance so it won't take insane distances to get below background. That'll get the output/kg up a lot. Just leave the damned thing in orbit until you need it for a return trip.

      And *cough* we know that works (Points up).

  18. Sloppy diagram by Traf-O-Data-Hater · · Score: 2

    How on earth (or halfway to Mars) did the 'Tigger' typo in the diagram slip past checks? Or did no-one at the company look over the 'How it works' page? And that unsecured capacitor in the video makes me shudder.

  19. It's better for cargo then for people by Required+Snark · · Score: 2
    This seems to be a very good low acceleration long haul thruster, similar to other competing ion drives. They are all of a type. Neumann seem to have done their homework in figuring out how to match solar panel output to mission profiles.

    However, ion thrust technology has some real problems when it comes to moving people around the solar system: transit time. If you look at this description, it turns out that the fastest travel time from Earth to Mars they quote is seven months. That's not from LEO but from a station at L5 to a Mars orbit where there is another orbiting station. Getting out of the gravity well is assigned to chemical rockets. This architecture requires a lot of infrastructure investment. Without these stations it's likely the transit time are much longer, closer to the 9/18 month burn and coast transfer orbits.

    Long term exposure to weightlessness is not good for humans. For example, space station cosmonauts (tweaked you on that one) have long term vision problems. Even worse is the radiation exposure outside the Van Allen belts. The manned mission to Mars community, including NASA, seem to be underestimating the seriousness of this problem. It's not just about cancer. There are other long term problems like heart disease and general decline in health and longevity. For example, the long term effects of exposure to radiation from Chernobyl have been terrible in affected areas in Belarus and the Ukraine. (There is a huge coverup over this situation, so you don't hear anything about it. Even the World Health Organization seems to want to sweep it under the rug.)

    It's surprising that no one here has made any comparison to the recently released road-map from SpaceX. They propose a 30 day transit time without needing any orbital infrastructure either at Earth or at Mars. They are further along then Neumann, having their first generation hardware already proving itself in space flight, while Neumann is only now doing a flight test. Even so, it's unclear if ion or chemical engines are the best way to send humans to Mars, assuming that is a good idea in the first place,

    Looking at the specs, if the Neumann system works as advertised it would be well suited for exploring the outer solar system. If paired with an RTG It would allow significant size missions to the outer planets that could go into orbit and not be limited to flybys. They confidently describe continuous acceleration for years at a time with a single fuel slug weighing in at a few kilograms. Even though manned missions to Mars are more glamorous, exploring the solar system is equally important in the long run.

    --
    Why is Snark Required?
    1. Re:It's better for cargo then for people by Required+Snark · · Score: 2

      Sorry, I mistyped a 30 day trip time for SpaceX when it should have be 90 days.

      --
      Why is Snark Required?
  20. Big difference in these ion thrusters. by cbhacking · · Score: 1

    Neumann thrusters work very differently from existing ion thrusters, though. At a high enough level, the concept is the same - ionize some stuff, accelerate it using an electric field - but the details matter a ton. Or, indeed, several tons. The existing ion thrusters mostly use gases - xenon is popular - as reaction mass. That means your reaction mass is already conveniently in tiny individual particles (single atoms, since it's a noble gas) suitable for extreme acceleration, but it also means you need to have a bunch of tankage, valves, and so on... and once the xenon runs out, you're done. Xenon thrusters - especially the most efficient ones, which use grids that the particles fly through - have a limited lifetime, too; they wear out pretty fast if you use them with a lot of power.

    Neumann thrusters use solid fuels, usually metals (though they also tested with pure carbon, and it worked reasonably well). There's no tankage, no moving parts such as valves (although the fuel rods may occasionally need replacement), and no risk of your fuel leaking off into space. What's more, in theory you can simply use metal that is *already in orbit* (such as discarded rocket upper stages, end-of-life satellites, or even outright junk if you can catch it safely) and that means you can easily "refuel" while in orbit. The performance you get varies depending on the reaction mass, with some metals producing absurdly high specific impulses (11000 seconds?!? That's far better than existing ion thrusters) and some producing more moderate efficiency but permitting quite high thrust (well, relative to other ion thrusters; it's still measured in m/s of delta-V per month) if you have the power (without eroding any part of the thruster except the fuel rod, unlike a conventional ion thruster running at such power levels).

    Some of it, like the in-space "fueling", is more than a little difficult, but the basic idea seems sound. It's also a pretty new technology, and they've already come up with some improvements (such as a magnetized "nozzle" that gives better thrust, presumably meaning it improves electrical-power-to-thrust efficiency) so I'm sure the technology will mature still further as research on it continues.

    --
    There's no place I could be, since I've found Serenity...
  21. Actual links by cbhacking · · Score: 1

    http://neumannspace.com/ - the web site of the company / research lab building these things. Kind of hype-y, of course, but has some good info.
    http://neumannspace.com/scienc... - the section of the site that gives an overview of how the Neumann thruster actually works, how efficient it can get, and so on. Includes links to blog posts about a number of the fuels they've tested, such as http://neumannspace.com/blog/f... (which has an utterly ludicrous specific impulse).

    --
    There's no place I could be, since I've found Serenity...
  22. About time by Anonymous Coward · · Score: 0

    I wondered when someone was going to ditch lightweight gasses and try to use denser materials (water, iron, etc). They're a lot easier to store, have a much higher thrust to weight ratio and are usually much easier to find in space. I suppose the only problem is power, they're talking about arc welding levels of power, which either requires pretty large solar arrays or nuclear. Its seeming more and more apparent that we need larger power systems for spacecraft, it is the only thing limiting various ion/plasma thruster designs from achieving significant size to replace chemical propulsion.

    1. Re:About time by rubycodez · · Score: 1

      nope, you want very light ion because the specific impulse/efficiency advantage is entirely due to high exhaust *velocity* not mass

  23. Re:The main problem is safely grabbing the space j by tomhath · · Score: 1

    The problem with space junk is less about getting to it

    Actually, that is the problem. Maneuvering to intercept a piece of space junk requires a huge amount of energy when you're already traveling 17,000 mph, that's a lot of momentum to change.

  24. Early 2000's by LifesABeach · · Score: 1

    NASA was funding this technology in the early 1970's. The article taped on the wall at my school was of a hand holding the actual engine to show its size. It had enough power to move a ping pong ball, in space. It does look like the engineers have "improved" the design.

  25. interesting but doesn't solve the big problems by 0111+1110 · · Score: 1

    This is quite obviously *not* any sort of general replacement for chemical fuel due to the low thrust. A Nuclear Salt Water Rocket or Fission Fragment rocket otoh might do it. I wonder if this tech would be useful for micro-ships.

    --
    Quite an experience to live in fear, isn't it? That's what it is to be a slave.
  26. Re:The main problem is safely grabbing the space j by HiThere · · Score: 1

    But the junk you're trying to reach is also moving exactly at orbital velocity for whatever orbit it's in, it's just at a slightly different angle. And almost all of it is moving in nearly the same orbit. So the difference in velocity would be relatively small. Of course, "relatively small" is still pretty large, but the GP's estimate of 400 mph is probably a reasonable guess. But the masses are low, so a reasonable catcher is probably possible. But you'd need to wait until a shard approached you (preferably on an skew course), and then shoot out a net to catch it. Not easy. Much easier to scavenge from the second stage that launched you.

    --

    I think we've pushed this "anyone can grow up to be president" thing too far.
  27. Crackpot [Re:EM Drive -v ION drive = 1st space r by Tablizer · · Score: 1

    Name one breakthrough in science which was made by a crackpot

    "Crockpot" is probably relative. Einstein's ideas were greeted with skepticism, bordering on ridicule, as was the multiverse model of quantum physics. Even rockets working in the vacuum of space was bashed by some in the mainstream.

    There is often groupthink and "best practices" of the time, and going against those can get one labelled as a crackpot. Humans naturally protect their turf.

    I've been labelled such myself for claiming that human grokkability is more important than shear parsimony in terms of "productive" programming code, in debates among certain academics. (I'm not claiming all academics.)

    The problem is that "parsimony" is easier to measure than human grokkability, but being easier to measure does not make a factor more important. My detractors seem to mistake ease-of-measurement for importance.

    Humans have to read and maintain the code, not machines nor mathematicians. (At least machines processing the code is usually not the bottleneck.)

    They claim that "emergent" benefits appear if one follows parsimony, but so far have not shown this the case. Their case is very indirect, seemingly claiming that if you follow parsimony, you'll filter out "bad" programmers, and academically gifted programmers would replace them and be many times more productive, justifying their higher salaries. This has been tried before without lasting benefits. Companies also value people skills, writing skills, UI skills, domain skills, and other things that "raw" academics are not necessarily better at. Those not in the field often don't understand the value of those aspects.

    Plus, I suspect they want the industry to value academics more, and are thus biased by their wallet to push for academic-centric development. Thus, protecting their turf.

    Did I wander into a tangent here?

  28. Re:Crackpot [Re:EM Drive -v ION drive = 1st space by cwsumner · · Score: 1

    Did I wander into a tangent here?

    Yes, but you are right! 8-)