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NASA Unveils Plans For Electric-Powered Plane (techcrunch.com)

An anonymous reader quotes a report from New York Times: A new experimental airplane being built by NASA could help push electric-powered aviation from a technical curiosity and pipe dream into something that might become commercially viable for small aircraft. At a conference on Friday of the American Institute of Aeronautics and Astronautics in Washington, Charles F. Bolden Jr., the NASA administrator, announced plans for an all-electric airplane (Warning: source may be paywalled) designated as X-57 and nicknamed "Maxwell," part of the agency's efforts to make aviation more efficient and less of a polluter. "The X-57 will take the first giant step in opening a new era of aviation," Mr. Bolden declared. Maxwell is equipped with 14 electric propeller-turning motors located along the wings, which will all be used to create sufficient thrust during take-off and landing. Only two large motors on the tips of the wings will be used once it's up in the air. The plane is a result of NASA's "New Aviation Horizons" initiative: a 10-year program to create a new generation of X-planes that will make use of greener energy, use half as much fuel, and be half as loud as commercial aircraft in use today.

55 comments

  1. We've been over this by Mr+D+from+63 · · Score: 1

    The issues with electric planes have been beat to death here, this NASA plane appears to have no solution for any of them.

    1. Re:We've been over this by Anonymous Coward · · Score: 0

      The issues with electric planes have been beat to death here

      Where? Slashdot? I can't recall ever reading about electric flight beyond drones, though I'm sure there has to have been some in the past.

      What issues?

    2. Re:We've been over this by Jonathan_S · · Score: 4, Informative

      The issues with electric planes have been beat to death here

      Where? Slashdot? I can't recall ever reading about electric flight beyond drones, though I'm sure there has to have been some in the past.

      What issues?

      The main problems are batteries, not electric propulsion itself. That batteries are far heavier that fuel on a lbs/kw basis, plus you don't get the bonus of the plane getting lighter the longer it flies. And high bypass turbines on planes aren't as inefficient in use as the ICE in cars (and planes are much more weight sensitive than cars) so you can't trade weight and drivetrain efficiency for useful range like you can in electric cars.

      Also, for commercial planes they spend very little time on the ground between flights; so you don't have time to recharge batteries. So you're looking at a battery swap technology as well to keep the turnaround time comparable to refueling.

      That said, if the distributed electric propulsion is as efficient as NASA thinks it might still be a net win even if you have to pair up the electric motor and prop placement of this X-57 with an onboard electric generator. In which case all the downsides of batteries are irrelevant. (Then you could look into whether a hybrid design with a some batteries and a smaller generator made sense)

    3. Re:We've been over this by Rei · · Score: 3, Interesting

      And meanwhile, in the real world, electric planes are a real thing, actually rather popular in the light aircraft world, and a market that's growing by leaps and bounds every year. And actually have excellent performance vs. price figures compared to their ICE equivalents. Ranges are usually similar to those of electric cars, 150-400km.

      Can we ditch with the old battery-energy-density-versus-fuel-energy-density canard, as if a gallon of petrol is an entire vehicle? Even the long-range versions of the Model S, the batteries are only a third of the vehicle weight. There are other parts to a vehicle. An electric motor the size of a roomba has the power output of an entire typical gasoline engine in a typical passenger car. And you can ditch the transmission and a lot of other hardware as well. And it's only logical that this size difference would be the case. Electric motors have vastly less heat to dissipate - heat dissipation means mass. Electric motors have vastly fewer parts; complexity equals mass. Electric motors create force directly applied as torque on a driveshaft linkage (or even directly on the wheel), while ICEs produce it as pressurized gas, change that to linear momentum, then change that to rotational. Obviously the latter is going to cost you signfiicantly in terms of mass.

      This headline makes it sound like electric airplanes are new. They're not. They're not even in the one-off-prototype stage, there are a number of serial producers out there. The market is expected to be over 22 billion a year three years from now. I'm not sure I believe it's going to scale up that fast, but it most definitely is growing. It's not even just small manufacturers, even Airbus is currently tooling up to market their E-Fan.

      --
      Monkeywrench Ex Machina.
    4. Re:We've been over this by Anonymous Coward · · Score: 0

      except that everything you posted was hype instead of a workable product. That $100K you quote? Yeah, it's not a real price; it's not marketed. There will be at least $50K of liability and certification costs. Could you do it as an experimental amateur built? Absolutely. Can you do it to commercial aviation standards? Probably, but with current technology, not at a price/performance that will match gasoline. Sorry to burst your bubble.

    5. Re:We've been over this by Anonymous Coward · · Score: 1

      Energy density is not a parameter which can be waved away. Calling it a canard merely demonstrates that you are not content with reality. Ion engines are also wonderfully efficient, and similarly limited to small scale by the same energy density problems.

      The most direct path to cleaning up air and surface transport is the use of synthetic fuels, efficiently produced with high-temperature nuclear heat. Nuclear power sources are also ideal for large ships and indispensable for any serious activity in space.

    6. Re:We've been over this by Tough+Love · · Score: 3, Insightful

      Power isn't the only problem with the concept. The wing loading is too high - that plane will glide like a rock if the motors quit. I also wonder about the turbulent flow over the wing from the prop wash, it seems far from the ideal lift/drag solution.

      --
      When all you have is a hammer, every problem starts to look like a thumb.
    7. Re:We've been over this by dj245 · · Score: 1

      And meanwhile, in the real world, electric planes are a real thing, actually rather popular in the light aircraft world, and a market that's growing by leaps and bounds every year. And actually have excellent performance vs. price figures compared to their ICE equivalents. Ranges are usually similar to those of electric cars, 150-400km.

      Can we ditch with the old battery-energy-density-versus-fuel-energy-density canard, as if a gallon of petrol is an entire vehicle? Even the long-range versions of the Model S, the batteries are only a third of the vehicle weight. There are other parts to a vehicle. An electric motor the size of a roomba has the power output of an entire typical gasoline engine in a typical passenger car. And you can ditch the transmission and a lot of other hardware as well. And it's only logical that this size difference would be the case. Electric motors have vastly less heat to dissipate - heat dissipation means mass. Electric motors have vastly fewer parts; complexity equals mass. Electric motors create force directly applied as torque on a driveshaft linkage (or even directly on the wheel), while ICEs produce it as pressurized gas, change that to linear momentum, then change that to rotational. Obviously the latter is going to cost you signfiicantly in terms of mass.

      This headline makes it sound like electric airplanes are new. They're not. They're not even in the one-off-prototype stage, there are a number of serial producers out there. The market is expected to be over 22 billion a year three years from now. I'm not sure I believe it's going to scale up that fast, but it most definitely is growing. It's not even just small manufacturers, even Airbus is currently tooling up to market their E-Fan.

      I'm sure we will have electric planes but they will almost certainly remain the domain of small aircraft. The car analogy works well. Electric cars make sense but electric 18-wheelers don't and probably never will. A radical and fundamental shift in how we move cargo and people is more likely to me than an electric A330.

      --
      Even those who arrange and design shrubberies are under considerable economic stress at this period in history.
    8. Re:We've been over this by Anonymous Coward · · Score: 0

      maybe no an A330, but advanced Zeppelin type aircraft for cargo are more than a possibility, and for land before we started crazily moving everything by 18-wheelers there were trains, many companies had rail tracks right into their premises

      So no such fundamental shift in how we move cargo at all needed

    9. Re:We've been over this by Anonymous Coward · · Score: 1

      You this does not make sense: http://electrek.co/2016/06/13/nikola-motor-pre-orders-worth-2-billion-electric-truck/

      Seems a lot of pre-orders says otherwise.

    10. Re:We've been over this by Anonymous Coward · · Score: 0

      Power isn't the only problem with the concept. The wing loading is too high - that plane will glide like a rock if the motors quit. I also wonder about the turbulent flow over the wing from the prop wash, it seems far from the ideal lift/drag solution.

      Gotta love all the armchair engineers. Oh, the wing loading is too high, oh, it's too heavy...

      Whatever. We have planes that can carry FUCKING TANKS in their bellies. You can make the wings LARGER. You can make the engines more efficient. You can even make the plane run on an engine that generates electricity from fuel, and uses that, so that the engine can always run closer to peak efficiency, using a battery to store energy while the engine cycles on and off, and the batteries wouldn't have to be that heavy. Then the electricity generated could be used to turn the motors to which the propellors (or what have you,) are attached.

      Also, the power to weight ratios of batteries improve constantly over time, whereas the power to weight ratio of jet fuel doesn't change, with time, and is limited to the energy in the bonds of the atoms in the fuel.

      So go on arguing why it can't work, while smarter, better people than you are making it work.

    11. Re:We've been over this by Anonymous Coward · · Score: 0

      The first link are to pictures of theoretical planes, and gets a lot of other hits because it has the word airplane. The second link is performance data for one, experimental plane, that are claimed numbers. This plane is amazing, but not in production.

      The claim of 22 billion dollar growth article states:

      Among the three technology types including power electronics, thermal management system, and advanced materials & safety system; the power electronics market is expected to account for the highest market share during the forecast period.

      That's where the 22 billion comes from.

      I don't understand why the electric car/airplane gypsies, and the environmental the end is near gypsies, and some political types feel the need to tell tall tales to justify their wants and desires. Sure, electric planes would be very cool, electric motors are very torquey and torque = high rate of climb BUT (and this is a big BUT) spinning tales of hyperbole like this poster does hurts the advance of technology, it does not advance it.

    12. Re:We've been over this by Coren22 · · Score: 1

      So, to try and counter all electric 18 wheelers you trot out a hybrid electric powered by natural gas or diesel?

      --
      APK likes to ask for responses to the same things over and over. Maybe he just likes the responses?
  2. London to paris by invictusvoyd · · Score: 1

    In two days .

    1. Re:London to paris by BlueStrat · · Score: 1

      (London to paris)

      In two days.

      Depending on number of factors, that in itself may not be a bad thing.

      Where I can see possibilities here is possibly as propulsion for fractional-buoyancy/buoyancy-compensated mass air cargo/passenger transport craft design using gas filled cells to lessen the demands for lift and thrust.

      Some thing somewhere between a dirigible, a sea-going ship, and a passenger/cargo plane. Something that could take advantage of large scale economy savings combined with lower environmental impact. Imagine a large cargo or passenger ship that, once it clears a harbor/port area (or simply takes off from an airport), can lift itself into the air and proceed on course for it's destination on electric power with a significant percentage of the need for lift and thrust cancelled by positive-buoyancy gas cells, most or all of the electricity coming from photo-voltaic cells covering the upper hull/fuselage and lifting/control surfaces.

      Having the ability to land on land or sea and at the lower speeds involved adds a large safety factor as well in the event of unforeseen weather or technical/mechanical problems in the craft itself on long global navigation legs.

      If a ticket from London to Tokyo or Singapore to LA took two days but cost around the $100USD price point or even lower, many more people would travel and shipping costs included in the price of many things shipped long distances would plummet.

      The current state of energy storage technology and the energy densities achievable currently do not lend themselves to small craft yet to a level approaching the ranges, loads, speeds, and costs of current small aircraft. That will likely eventually change, but it will also likely be a while yet before the balance scales tip the other way

      But as I pointed out above, electric propulsion for aircraft may well scale up quite nicely with some creative engineering.

      Strat

      --
      Progressivism (aka US 'Liberalism'): Ideas so good they need a police/surveillance-state to enforce.
    2. Re:London to paris by Rei · · Score: 1

      Of course, in reality, small electric aircraft tend to perform better than their ICE counterparts. Power density comes much cheaper (in terms of mass, volume, and money) with electric drive than it does with internal combustion. It's energy density that electrics perform worse in.

      Some small electric aircraft have pretty crazy performance specs for surprisingly little money. Of course, if you've seen high performance drones designed for pulling tricks, you wouldn't find this surprising; you could never get that sort of performance out of an internal combustion aircraft.

      Energy density is always the achilles heel, and it limits electric aircraft currently to several hundred kilometers range. But, it improves at about 7% a year. People like to joke about all of the announced tech breakthroughs in batteries, as if they never materialize, when the reality is, they simply don't notice when they do, because the market moves by progressive scaleup, not leaps and bounds. Those silicon anodes, for example, that people were talking about here years ago? They started being used in commercial cells a couple years ago. Lithium-sulphur? They'll probably start hitting the market later this year or early next. Etc. You probably won't even notice when li-air start hitting the market - except that your cell phones will gobble even more power and despite that you'll get even longer lifespans with an even smaller battery.

      (Note that the cell phone timeline image above was made in 2009, you could put even thinner modern phones at the end of that... and throughout their history, the battery has been one of the biggest portions of the size of the phone)

      --
      Monkeywrench Ex Machina.
    3. Re:London to paris by joe_frisch · · Score: 1

      Lighter than air craft have a lot of problems. The energy use isn't as as low as you might imagine - there is no drag due to drift, but the large frontal area resulst in a lot of parasitic drag except at very low speeds. Winds, ice etc can be a serious problem, and they typically can't climb above weather.

      one example at http://www.zeppelinflug.de/en/
      carries 16 people, 80mph, 600hp total engines, range 600 miles (they don't give detailed specs).

      Compare with a 1960s beechcraft baron:
      6 people, 230mph, 600HP total engines, range ~800miles

      person miles / gallon seems to be in the same ballpark. The airship may be a lot more pleasant to fly in, but its isn't substantially more efficient .

    4. Re:London to paris by BlueStrat · · Score: 1

      Lighter than air craft have a lot of problems. The energy use isn't as as low as you might imagine - there is no drag due to drift, but the large frontal area resulst in a lot of parasitic drag except at very low speeds. Winds, ice etc can be a serious problem, and they typically can't climb above weather.

      one example at http://www.zeppelinflug.de/en/
      carries 16 people, 80mph, 600hp total engines, range 600 miles (they don't give detailed specs).

      Compare with a 1960s beechcraft baron:
      6 people, 230mph, 600HP total engines, range ~800miles

      person miles / gallon seems to be in the same ballpark. The airship may be a lot more pleasant to fly in, but its isn't substantially more efficient .

      Wasn't talking about lighter-than-air craft. What I'm talking about nobody has built an analog of yet that I'm aware of.

      Basically a giant electric powered airliner/cargo plane/lifting body that is capable of landing/taking off from land or sea which has *some* of the lift requirements met by adjustable/controllable gas cells located inside the craft. I'm talking on the scale of one of the giant container ships or "supertanker" oil ships, maybe even much larger. I'm thinking something that uses a combination of lifting-body design and surface-effect-cushion aerodynamics at just a few meters altitude above the sea, possibly, rather than lifting to a multiple-kilometers altitude? Not sure at this point what might be possible versus pragmatic and practical/efficient in that regard.

      Haven't thought out all the details yet. The comparisons you cite also both utilize '50s/'60s/'70s era engineering, technology, & materials and also uses internal combustion engines for power. Even in the example you cite, there is *some* savings, just not an impressive and/or worthwhile amount.

      Like I said, I'm basically typing a 'stream-of-consciousness' here as I consider the problem.

      Strat

      --
      Progressivism (aka US 'Liberalism'): Ideas so good they need a police/surveillance-state to enforce.
    5. Re:London to paris by joe_frisch · · Score: 1

      Ground effect planes are interesting. The Russians did a lot with those. https://en.wikipedia.org/wiki/...
      I think the biggest problem is that the low altitude environment is pretty hostile - waves, birds, floating obstructions etc. In principal though they are more efficient than airplanes.

      My comment really was that using buoyancy lift seems like it should provide a major fuel savings, but in practice (I've looked at other examples as well) it doesn't seem to make a lot of difference to the overall efficiency. It is very helpful if you want vertical takeoff - helicopters are very inefficient .

      The examples I gave used the same technology engines so I figured that canceled out. It also turns out that aircraft piston engines are pretty efficient - its simple design, almost single operating point, so its much easier to get good efficiency than it is for a car engine) . there has been little change in aircraft piston engine efficiency since 1960. Jets are actually less efficient, but the lighter weight more than makes up for that. Going to high bypss jets has made the biggest difference. Aircraft aerodynamics has improved some. I don't know if its possible to improve the aerodynamics of buoyant craft.

    6. Re:London to paris by legRoom · · Score: 1

      with a significant percentage of the need for lift and thrust cancelled by positive-buoyancy gas cells,

      As has already been pointed out, buoyancy cells reduce the need for lift, but increase the need for thrust at a given speed. The square-cube law favours larger airships for lower drag.

      most or all of the electricity coming from photo-voltaic cells covering the upper hull/fuselage and lifting/control surfaces.

      The power that can be collected via solar cells scales with surface area, but the power required scales with mass (and therefore volume). Thus, the square-cube law also favours smaller airships for greater power-to-weight, if solar power is the primary energy source.

      lifting-body design and surface-effect-cushion aerodynamics at just a few meters altitude above the sea, possibly, rather than lifting to a multiple-kilometers altitude?

      The volume of buoyancy cell required to lift a given mass increases exponentially with altitude, so a low cruising altitude is desirable to keep the size reasonable. However, deliberately cruising at "just a few meters altitude" is a very bad idea: many of the worst airship accidents in history were caused by the wind suddenly pushing on the vehicle's massive surface area in an unexpected direction, easily overwhelming the engines, ground handlers, etc. You need to cruise at a high enough altitude that a single unexpected down draft doesn't kill everyone on board.

      If a ticket from London to Tokyo or Singapore to LA took two days but cost around the $100USD price point or even lower...

      I don't think this will ever happen. At least in the USA, two nights in a cheap motel costs at least $100 (often much more). It seems safe to say that a flying motel will never be cheaper than one built on the ground. Also, the need to provide overnight accommodations, and room for people to stretch their legs, imposes a large weight penalty on passenger airships compared to airplanes.

      This is a fundamental reason that airships are unlikely to replace airplanes for general passenger service: life is expensive, and people's time is valuable. The richer the world gets, the less likely that a new, slower form of long-distance air travel will catch on, even if it is more energy efficient.

      Those concerns don't apply to cargo though, so the idea is still very much worth exploring.

      I'm basically typing a 'stream-of-consciousness' here as I consider the problem.

      Same here.

    7. Re:London to paris by legRoom · · Score: 1

      I think the biggest problem is that the low altitude environment is pretty hostile - waves, birds, floating obstructions etc. In principal though they are more efficient than airplanes.

      That, and the high air density at sea level requires a lower cruising speed to be efficient. The military, who funds much of the world's aerospace research, values speed more than efficiency. (They are only interested in efficiency mostly because it limits range, which is also important to them.)

      Jets are actually less efficient, but the lighter weight more than makes up for that.

      "Efficient" is a meaningless term, unless one specifies which two metrics are being compared.

      Jet engines generally have considerably better thermodynamic efficiency than piston engines: they convert a larger percentage of the chemical energy in the fuel into mechanical energy, and waste less in the form of unused heat and partially burned exhaust.

      They have inferior thrust efficiency at low speeds (less thrust is generated per unit fuel per second), but superior thrust efficiency at high speeds (trans-sonic and up). In fact, normal piston-driven propellers don't produce any (net) thrust at all at the normal operating speeds for many jets, and so are perfectly inefficient.

      With a good flight profile, burning through fuel faster in order to fly faster generally does not hurt the plane's overall fuel efficiency, as measured in fuel units burned per unit distance. What it does do is complete the journey faster, freeing the vehicle and its passengers/cargo to move on to another task, thus improving economic efficiency. The only reason that airplanes don't just fly as fast as they possibly can, is that drag increases sharply for airspeeds above Mach 1.

      TL;DR: Jets are used on nearly all large planes because they are more efficient in the metrics that count, not just because of their weight.

    8. Re:London to paris by joe_frisch · · Score: 1

      Its interesting (surprising) that turbine engines are actually a bit less efficient than most piston engines. See: https://en.wikipedia.org/wiki/... Note that the 1996 turboprop engine is less efficient than the simlar size and application piston engine. The turbine engine is much lighter so the overall aircraft efficiency is better. Similarly the diesel ship engines are more efficient that turbine ship engines of similar sizes.

      In turbines the maximum combustion temperature has to be within the operating range of the turbine blades. For a piston engine, the high temperatures in the middle of the cylinder don't have time to melt the metal before it is cooled on the next cycle. Piston engines can run with hotter combustion temperatures so they have better base Carnot efficient. There is a fantastic set of books by Taylor: "the internal combustion engine in theory and practice" that is great reading for anyone really interested in how engines work. I found a lot of surprises.

      You mention that the high exhaust velocity of jets reduces their efficiency in low speed applications. That is in addition to the above thermodynamic efficiency.

    9. Re:London to paris by legRoom · · Score: 1

      Your analysis assumes that the purpose of an airplane engine is to produce shaft power (the subject of the Wiki article you linked). This is incorrect, especially for jets (which ought not to be confused with turboprops).

      The true purpose of an airplane engine is to add kinetic energy to the airplane. The effectiveness of jets at this task relative to piston-driven propellers is far higher than your shaft-power based comparison would suggest.

      First, because jets (unlike turboprops) are intended to derive a significant portion of their thrust directly from the high-velocity exhaust stream, like a rocket. In a turbojet, shaft power is mostly used to drive the compressor. While turbofans are more similar to propeller engines in this respect, they are still distinct in that they deliberately leave a lot of energy in the exhaust stream.

      Thus, for a given shaft power rating a jet will produce much greater thrust than any propeller based system. Moreover, the higher the ambient airspeed, the greater the proportion of thrust that is derived from the exhaust stream, rather than the fan. Ignoring the exhaust stream when analysing the fuel efficiency of a jet engine will yield wildly incorrect results for turbojets at any speed, and for turbofans at cruising speed.

      Second, because sustaining the same amount of thrust at a higher airspeed adds linearly more kinetic energy to the aircraft. Consider:

      Prop: A 10 ton airplane is cruising at [125 m/s], maintaining constant altitude and speed using a piston-driven propeller exerting [20 kN] of force. The kinetic power imparted to the airplane is therefore [20 kN] * [125 m/s] = [2.5 MW].

      Jet: A 10 ton airplane is cruising at [250 m/s], maintaining constant altitude and speed using a jet exerting [20 kN] of force. The kinetic power imparted to the airplane is therefore [20 kN] * [250 m/s] = [5 MW]. (Yes, a jet can sustain a higher speed using the same amount of thrust - the plane just has to fly higher, where the air is thinner and creates less drag.)

      At the same effective specific impulse (Isp , a better measure of jet efficiency than the BSFC you linked), a jet can achieve greater practical fuel efficiency (fuel burned per unit distance) than a propeller plane, simply by flying faster and higher. This effect is very large - enough so to overcome significant differences in Isp as compared to a prop plane.

      TL;DR: The purpose of a jet is to move the airplane, not to spin a shaft. It's efficiency should be evaluated on that basis.

    10. Re:London to paris by joe_frisch · · Score: 1

      For subsonic planes like airlines, the "jet" engines are high bypass and the majority of the thrust comes from the ducted fan . Ducted fans behave like propellers, the ducts improve efficiency at near sonic speeds, but otherwise there is not much difference. There is a little thrust from the jet exhaust, but that is low efficiency because its velocity is so much higher than the aircraft efficiency.

      If you looked at the ISP of a prop plane it would be very high since the reaction mass is moving slowly. This sounds counter-intuitive becuase for a rocket a high exhaust velocity -> high ISP. The difference is that for a rocket the energy source and the reaction mass are the same thing. The momentum goes as MV, while the energy goes as 0.5MV^2 . So the energy / momentum goes as V. If you have an external medium to move (air), you want a low exhaust velocity (about the same as the aircraft speed). If you have to carry the reaction mass you want a high exhaust velociyt.

    11. Re:London to paris by legRoom · · Score: 1

      If you have an external medium to move (air), you want a low exhaust velocity (about the same as the aircraft speed).

      You seem to have skipped the most important parts of my posts. Even a jet that burns more fuel per unit thrust, can still be more efficient at actually moving the airplane from origin to destination, because the higher top speed means that it doesn't need to sustain that thrust as long to complete the journey.

      There is a little thrust from the jet exhaust, but that is low efficiency because its velocity is so much higher than the aircraft efficiency.

      Subsonic turbofans typically have a bypass ratio somewhere between [5:1] and [10:1]. Taking into account the mass of the fuel being mixed into the core air stream, this means that you are ignoring between [21.2%] and [10.5%] of the mass flow.

      Moreover, that portion of the mass flow is ejected at considerably higher speed, so you are actually ignoring an even greater percentage of the thrust - perhaps [30%] to [15%]? Maybe more at cruising speed, given that the rate of thrust lapse is higher for the fan output, than for the core. (My quick search didn't turn up any hard numbers on the speed of the core exhaust, specifically.)

      That difference in thrust is of the same magnitude as the shaft power efficiency difference for your turboprop example, and must not be neglected if you want the comparison to be meaningful.

      In turbines the maximum combustion temperature has to be within the operating range of the turbine blades.

      Finally, that one random turboprop you picked as the point of comparison isn't very efficient compared to a lot of modern turbines. Hard numbers are not easy to find, but even the 1966 [Rolls-Royce/Snecma Olympus 593](https://en.wikipedia.org/wiki/Rolls-Royce/Snecma_Olympus_593) had a thermodynamic efficiency of [43%]. This beats any of the airplane engines in your shaft power comparison.

      While the Concorde was an exotic, bleeding-edge design, materials science has advanced considerably since then, and modern high-end turbines have higher pressure ratios and peak temperatures. If you want to see good examples of this, you need to go look where the money is: large passenger planes (Boeing 777) and cutting-edge military aircraft (F-22 or A400M), not general aviation or small regional passenger planes.

  3. Re:Yay NASA! by Anonymous Coward · · Score: 0

    You know that first A in NASA is Air, right? You're a fucking idiot. This is their fucking job. Now, I'm pretty sure that their plan is to throw money at contractors and hope magic happens, but aircraft are most certainly in their charter.

    "Sec. 103. As used in this Act--

    (1) the term "aeronautical and space activities" means(A) research into, and the solution of, problems of flight within and outside the earth's atmosphere, (B) the development, construction, testing, and operation for research purposes of aeronautical and space vehicles, and (C) such other activities as may be required for the exploration of space; and

    (2) the term "aeronautical and space vehicles" means aircraft, missiles, satellites, and other space vehicles, manned and unmanned, together with related equipment, devices, components, and parts."

  4. Maxwell is a micro-aggressive name by turkeydance · · Score: 0

    triggering the Beatles: http://www.azlyrics.com/lyrics...

  5. going the way of manned space travel? by sittingnut · · Score: 0

    let us hope nasa will waste lost of money trying out all the inefficient ways of making electric planes.

    then hopefully russians will create cheap and effective electric planes that everyone (even the usa military ) can borrow, as they do with human space travel (again even usa military use russian rockets now ) .

    meanwhile eion musk will blow lots of hype trying get his cronies in usa government to give him money to make electric planes too(especially ones that fly on social media to give his fanboys much needed orgasms). as with all his projects this will be a subsidy worthy cause, even without crony capitalism.

    1. Re:going the way of manned space travel? by Brett+Buck · · Score: 1

      The Russians are't going to do shit. They have nothing like technology to do this - the Chinese are far more likely and are closer. The Russians plod on with steam-era rockets, which are practical but are a fallback to pre-V2-technoliogy. They aren't advancing any states of any arts.

    2. Re:going the way of manned space travel? by Rei · · Score: 0

      In fact, there already are Chinese manufacturers of electric planes, like Yuneec.

      As for Musk, he doesn't just want to make an electric airplane, he wants to make the first electric airplane to break the sound barrier. Ho-hum, I wish that guy would decide to try something ambitious for once ;)

      --
      Monkeywrench Ex Machina.
    3. Re:going the way of manned space travel? by Brett+Buck · · Score: 1

      Musk, not being an engineer or scientist of any sort, is probably used to people telling him things are impossible. Most of the time, engineers in the current day tend to immediately jump to "impossible" based on their experiences trying to make something of fix something simple due to crushing bureaucracy that they assume everything is impossible. When someone tells a management type something is impossible, they just don't believe the engineer any more, because the engineers are usually overstating the difficulties.

    4. Re:going the way of manned space travel? by legRoom · · Score: 2

      The Russians plod on with steam-era rockets, which are practical but are a fallback to pre-V2-technoliogy.

      That's a pretty ridiculous and insulting exaggeration.

      Up until SpaceX announced the Merlin 1C less than a decade ago, Russia was the unquestioned leader in Kerosene-Oxygen engine technology. There's a good reason that United Launch Alliance selected the Russian RD-180 for the Atlas V. More generally, Russian technology is competitive with (I do not say equal to) that of the West in many areas, such as rocketry, jet engines, airframes, avionics, weaponry, etc.

      Dismissing all of that as "pre-V2 technology" is nonsensical propaganda: facing off against a military limited to actual pre-V2 tech, the Russian military would absolutely dominate.

    5. Re:going the way of manned space travel? by legRoom · · Score: 1

      Building a supersonic electric airplane is certainly ambitious, but far from impossible.

      On the other hand, building a practical and economically useful supersonic electric airplane with current technology is impossible. Hydrocarbon-powered supersonic planes still run out of fuel quickly, even after hundreds of billions of dollars of investment in the concept. A battery-powered model will certainly not have useful endurance.

    6. Re:going the way of manned space travel? by Anonymous Coward · · Score: 0

      IMHO Musk has done more both for the push to affordable ground to orbit rockets and for the adoption of electric cars than anybody, and is working...pretty remarkable
      I really wish that NASA had the money and the focus to dedicate themselves in advanced concepts and technologies beyond the rocket engine

  6. Controversal design , 12 engines deadweight +drag by SuneSpeg · · Score: 1

    12 engines as deadweight and dragging props, that doesnt seem very efficient ? Even with foldable props, they will induce a significant drag. I am sure NASA can come up with a better solution for extra power needed for takeoff.

  7. So many motors??? by moosehooey · · Score: 1

    So they have 12 extra motors/props just for takeoff, that add both weight and drag? Why don't they just use one motor and drive one of the wheels against the ground?

    1. Re:So many motors??? by Rei · · Score: 1, Troll

      First off, airplanes putting electric motors in their landing gear is becoming a mainstream thing, it's a major fuel saving mechanism being employed by major manufacturers.

      Secondly as has been pointed out in many comments above, there are numerous reasons for the approach, as it lets you increase air velocity across the wing (giving better wing performance) and use props more performance-optimized to their current flight environment.

      Third, unlike ICE engines (the reason that this was impractical before), electric motors are very small and lightweight versus how much power output their produce.

      --
      Monkeywrench Ex Machina.
    2. Re:So many motors??? by Mr+D+from+63 · · Score: 1

      Motorized landing wheels for taxi makes sense for stop/start rolling on jet aircraft, but there's no benefit of those additions for flying and we don't see them on ICE prop aircraft, the type you are comparing battery craft against. You are touting electric aircraft awfully hard, but even with all the battery advances we've had the only electric craft making any traction are very short range/duration, single person recreational craft. Those look like fun, but there is a long way to go to get beyond the recreational market even with major battery improvements.

      And then, trying to compete with jets is another challenge altogether.

  8. Re:Controversal design , 12 engines deadweight +dr by ThosLives · · Score: 2

    You're forgetting that with the extra props across the wing, you need a much much smaller wing, and can have a wing with much higher aspect ratio*. The reduction in wing area and increased aspect ratio more than offsets any drag from the multiple (folded) props during cruise.

    *Those props aren't there for thrust, they are for increasing flow velocity over the wings.

    --
    "There are a dozen opinions on a matter until you know the truth. Then there is only one." - CS Lewis (paraprhase)
  9. Re:Controversal design , 12 engines deadweight +dr by Anonymous Coward · · Score: 0

    GP also ignorantly fails to understand that props efficient in high speed flight are inefficient at low airspeed and vice versa, so stowing climb props is a very good choice for an electric airplane.

  10. Re:Yay NASA! by Anonymous Coward · · Score: 0

    Space exploration? You make it sound like we have to send people up a few hundred miles in order to take pictures of things light-years away?

  11. Re:Controversal design , 12 engines deadweight +dr by tomhath · · Score: 1

    RTFA. Max speed is 175KT, not exactly "high speed". NASA also admits this won't be viable for commercial service, basically a hobbyist plan for short flights with very little payload.

    Bottom line though is that NASA is and has always been a PR machine. An all electric plane is a warm fuzzy story for people to read.

  12. Re:Yay NASA! by Rei · · Score: 0

    Indeed, research is a bit part of what NASA does - and IMHO, it should be bigger. I agree with Buzz Aldrin that NASA should revert to the earlier NACA model.

    --
    Monkeywrench Ex Machina.
  13. Electric airplanes . . . by Anonymous Coward · · Score: 0

    "Conventional" aviation supplies a product for market demand: high-speed, low-cost transportation. Low-mass, high-energy fuels make it possible: primarily kerosene, with some use of high-octane gasoline. Right now, electrical power will never replace hydrocarbon fuels because the energy density

                        energy unit / mass unit

    is too low. Even worse, the

                        cost / energy unit

    for batteries exceeds the hydrocarbon

                        cost / energy unit

    "price density". Yes, battery aviation now exists - with government subsidies, and yes, battery aviation fans will howl that government subsidizes hydrocarbons, etc. etc. etc. Hydrocarbon subsidies should end. This does not change the fact that battery energy density will never exceed hydrocarbon energy density.

    Now, maybe steam has potential:

    https://www.youtube.com/watch?v=nw6NFmcnW-8

  14. Um, no, you're wrong about long-distance trains. by Anonymous Coward · · Score: 0

    Take an electrified Amtrak train from DC to Boston. The cars are passive, all the pulling is done by the engine(s) up front.

  15. Re:Illutrates the flaw in electric vehicles by dontbgay · · Score: 4, Insightful

    The distributed motors are a feature, not a bug. With current designs, manufacturers can't go with more smaller engines due to efficiency losses. The engines installed on aircraft now are used to provide thrust and the resulting wind across the airfoil from that forward movement is what provides lift.

    This design is different because the smaller motors have higher efficiencies and are able to direct air over the airfoil directly instead of relying solely on forward thrust to provide the same wind. That adds to lift, which reduces takeoff distance, which reduces friction losses from the wheels.

    --
    Sig not found.
  16. Re:Illutrates the flaw in electric vehicles by joe_frisch · · Score: 1

    Lots of tradeoffs. Airflow over the wings helps takeoff performance, but the disrupted airflow from the props in cruise is likely top reduce efficiency. Generally for low speed aircraft you want as few total propeller blades as you can use in order to reduce the losses from blade tip vortices. (practical effects like prop diameter will often force you to more props and more blades).

  17. Not a hybrid and not for everyone by ukoda · · Score: 1

    The article states that the Maxwell X plane is a hybrid and goes on to detail it is electric propulsion and battery powered. That doesn't sound like a hybrid to me. I can only guess they either used the term in error or were think of future concepts.

    Interesting I would guess pure electric aircraft make up the majority if you include hobby quadcopters in that definition. I mention that as I think the takeaway from the article is that electric aircraft are practical in some niche areas and NASA's work will widen those niches. The changes need for EV cars to replace ICE are evolutions in batteries and is already close to the tipping point, but It is going to take some truly impressive breakthrough in battery technology before your will see traditional commercial jets like the A320, 737, 767 or A380 replaced. My guess we are are years, not decades, away from cars going all electric but for aircraft we are probably still talking decades.

  18. Re:Illutrates the flaw in electric vehicles by ukoda · · Score: 1

    My guess is the props on the takeoff motors fold in when cruising to reduce drag. Even if they do I would still worry about the remaining drag and the extra weight.

    But then again it is an X plane. That is why you build them, to see how good or bad the ideas are in the real world.

  19. Re:Controversal design , 12 engines deadweight +dr by Anonymous Coward · · Score: 0

    hah, even better, look up "climb prop" and "cruise prop" and realize there's a huge difference between the optimal pitch for 80 kts and 130 kts. (climb speed v.s. cruise speed). Considering that tip speed is close to 540 kts at max RPM, that's an 8% difference in speed which is significant.

  20. Howsabout variable pitch propellors??? by knorthern+knight · · Score: 2

    > GP also ignorantly fails to understand that props efficient in
    > high speed flight are inefficient at low airspeed and vice versa,
    > so stowing climb props is a very good choice for an electric airplane.

    Howsabout variable pitch propellors??? They've been around since the 1920's, and have been in practical use since the 1930's https://en.wikipedia.org/wiki/...

    Rev up 2 or 4 engines (admittedly a bit inefficient) for takeoff, and then back off to more efficient speed for cruising. 2 or 4 larger engines are cheaper and more efficient than 14 smaller ones. A bonus feature is that many "variable pitch propellors" can change pitch to *REVERSE* thrust. This is useful for backing up out of a hangar, as well as providing braking during landing on short airstrips.

    --

    I'm not repeating myself
    I'm an X window user; I'm an ex-Windows user
    1. Re: Howsabout variable pitch propellors??? by Anonymous Coward · · Score: 0

      Yup, I fly with 2 of them. However, the airfoil on the propeller isn't optimized for either climb or cruise, and the pitch adjusting mechanism is heavier then the prop itself. Given the very small size of an electric motor compared to a fuel burning engine, stowing the prop really makes sense, and windmilling it might actually be better.