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I have found an study of the university of Maryland about an 2.3 Mio m³ big blimp for mars :
http://www.lpi.usra.edu/publications/re … d.pdf]MARV: Martian Airborne Research Vehicle 448KB PDF
Unfortunately I cannot read the complete PDF, cause it is (as it seems) not properly coded.
Hi Dook;
have you seen this:
http://www.lpi.usra.edu/publications/re … pdf]MARVIN: A Proposal for a Long-range Pressurized Rover 473KB PDF
IMHO this Rover resemble's your proposal but without solar cells.
[edit]:
I just forget the next PDF from the second HEDS-UP Forum :
http://www.lpi.usra.edu/publications/re … /texas.pdf [ 584KB PDF ]
They showed an inflatable rover concept with an really ingenious airlock äähh suitport. The spacesuit is stored outside of the Rover and only the accessport into the spacesuit is sort of an airlock here.
For starters, SpaceShipOne went through a cautious and exhaustive flight test program. It has also been designed for quick turnarounds and almost-assured reentry.
The other competitors have mostly gone for simpler, vertical takeoff and landing approaches. This is a way of achieving first flight quickly with assured reentry, and there is nothing really wrong with it. However, Rutan's air-drop approach is arguably better for the purposes of a tourist vehicle. It keeps the tourists off their backs while they are waiting to launch, gets them to launch altitude with a piloted, powered aircraft, and returns them to earth gently on a runway.
Most distressingly, the DaVinci team wants to compete for the X-Prize on its first flight in what looks like a tight race with Rutan. If they weren't playing catch-up, they might have time to launch a few missions to the upper amosphere before attempting the X-Prize.
I am afraid of what will happen if somebody gets killed in the initial suborbital flights, as the US or Canadian governments may decide to regulate the industry into the grave. Rutan's approach has minimized this possibility by slowly pushing the envelope and fixing the bugs (and even then they nearly met disaster.) The DaVinci team had better get it correct the first flight.
WOW, You have read my mind.
IMHO DaVinci should stop now. IMO it is ridiculous to go from Zero to 100km in one go without any tests at all. The chances for an successful launch are in my opinion slim. If they don't stop with this stupid behaviour and adopt an reasonable "build a little..test a little" approach they could seriously damage the complete XPrize and the suborbital launch attempts from other companies with an better development strategy.
I don't care if the pilot gets killed or not (this is really up to him) but I fear the reactions of the public and the FAA if this launch goes wrong.
How we will feed our crew on the long journey.
Farming for the Future
http://www.nasa.gov/vision/space/prepar … rming.html
farming too:
http://www.usu.edu/cpl/research_dwarf.h … _dwarf.htm
http://www.usu.edu/cpl/research_photobi … otobio.htm
http://www.usu.edu/cpl/research_hydropo … ponics.htm
Second, the problem of dragging a docking station well below orbital velocity has nothing at all to do with drag, the problem is that if the dock is not moving at orbital velocity, then its momentum will not be enough to counteract gravity. But instead of falling out of the sky immediatly, the space station above pulls on the docking station to cancel gravity out. But, since you can't get somthing for nothing, the docking station will drag the space station down out of orbit and the whole thing will fall without constant rocket thrust to keep it up there.
There is no problem at all.
The dock is moving slower than orbital speed, the counter-balance is moving faster than orbital speed and the space station in the middle is moving at orbital speed.
Together the complex of all three parts is moving at orbital speed. So unless you cut the tether the system will remain in orbit just like an normal space station like the ISS.
The added benefit of such an system is, that the docking station is moving (in this example) only at 79% of the orbital speed so you need only around 62% of the energy to reach the docking station. This would make SSTO's very simple and practical (see also the website "affordable Space Flight"). And with the counter balance moving faster than orbital speed you can save a lot of fuel going to the moon, mars or only GEO too when you launch space crafts or just satellites from the fast moving counterbalance.
Yes, the docking station will drag down the system when an Shuttle docks and nothing is done. But it does not happen fast cause the weight of the shuttle is far lower than the weight of the complete station and you don't need normal fuel to raise the orbit of the system with the docked shuttle. You can use an ion engine instead or even an electrodynamic system to raise the orbit. Just let electricity flow in the tether and the interaction with the magnetic field of the earth will raise the orbit of the station without any fuel.
All in all you don't need a lot of energy for this cause when the shuttle departs from the dock then the orbital system will raise it's orbit from itself and you have only to counter the effect of the payload in the long run unless the payload from and to earth is the same, then (theoretically) you don't need any fuel at all.
One Reason for a tethered space station is artificial gravity. Another reason may be an elevator between orbits.
Do You mean something like this:
http://www.affordablespaceflight.com/]h … light.com/
and this:
http://members.aol.com/Nathan2go/]http: … Nathan2go/
?
If anything becomes of the xprize I hope it maybe a scare to the Big guys on the rocketry block and Nasa. For if any achieves orbital status, look out for private industry may soon to follow.
I don't think that you need the XPrize to scare the big guys. IMHO they are already (slightly) afraid of SpaceX. SpaceX promises to launch around 4.5 tonnes into GTO for around US $20Mio instead of the around US $80Mio the other companies charge. If they can really fulfil this promise then the big guys will be very afraid.
I think the Heliostat is a good idea.
Hi Dook;
Thanks.
Originally I had something else in mind. Not an real Heliostat, but an Heliostat-like Mounting for the Solar Cells. All of the blue-shaded area's and lines where intended to represent the Solar-Cells in different positions.
So when you drive fast the "Heliostat-Mounting" of the Solar-Cells would swivel down and the Solar-Cells would align with the roof of the Rover ( see upper picture with the blue line ) and when the Rover is standing or only moving slow ( maybe <5mph) then the "Heliostat-Mounting" would swivel up and the solar-cells on this hugh mounting could face the sun regardless of the movement of the Rover and the position of the Sun.
But I like your idea too.
Manfred
Hi Dook;
I think I had an idea how you could improve the efficiency of the SolarCells without any new technology: Use an Heliostat.
See here my idea: http://www.8ung.at/mboeller/Heliostat-S … System.jpg
With this system you should be able to produce max. energy from sunrise till sunset. So instead of the 3 KWh/m² on an flat surface you could produce up to 0,59KW/m² x 12h = 7 KWh/m² or more than 2 times the normal amount of energy. An added advantage is, that the driving direction will no longer affect the energy production, cause the Heliostat will allways face the sun in an opimal way.
The SolarCells here are even a little bit bigger than in Your proposal. So with the (2 x 2x5.6 m² 22.4 m² x 7 KWh/m² x 20% efficiency for the GaAs SolarCells you can generate more than 30KWh per day. Enough for 2 hour of driving at full speed!
I hope you like it.
Manfred
Hi;
More information on Alkaline Fuel Cells, including efficiency:
http://www.utcfuelcells.com/space/space … uttle.shtm
Thanks! Seems the type of fuel-cell NASA is using in the Shuttle is far more efficient as the fuel-cells used in cars today. But IMHO the efficiency of 70% is only true when the fuel-cell works at 100% power and not at lower power ratings (see my last posting). IMHO you should use the fuel-cell only when necessary to feed the NiMH-accumulators and completely shut down the (thermally insulated) fuel-cells between this "battery loading" action. The Rover would be driven solely from the Accumulators then. With this mode of operation you should get the most out of the stored Hydrogen.
Another reason I didn't use the constant 4 wheel drive is that the front and rear wheels have different gear ratio's. Not that it would be a big problem but the front wheels are geared lower than the rear wheels to help with hills and climbing over rocks.
Yes I have seen that, but normally you don't need different gears between the front and rear wheels cause normally (I don't know if this is true for your E-Motors) E-Motors have an very wide and flat torque curve so IMHO it should not be necessary to have different gear ratio's between the front and rear drives.
Hmm, tried to find Fortubat on the web but all the sites were in French.
Sorry the website is only in German or French language. The important link is this one : http://www.fortu.de/punkt07.html.]http: … nkt07.html. You can see that they promise or guaranty (I'm not sure here) an energy density of at least 200 Wh/kg and promise an further increase to 250 Wh/Kg in the (near?) future.
Yes, the fuel cells use and convert a lot of energy to heat but I think this is necessary to keep the inside of the vehicle warm. The structure of the vehicle will be as thin as possible (maybe 1/2" carbon composite?) and even with insulation the inside of the vehicle is likely to get very cold at night since the only things operating would be the oxygen/pressurization system, the carbon dioxide removal system, and the heat lamps.
I don't think that you need a lot of further heating inside the vehicle. Most of the heating will be necessary on the outside to heat all the equipment mounted on the outside. Otherwise it will fail.
The heating of the inside should be fairly easy and simple cause the 2(?) Astronauts alone will heat the inside of the Rover with ~ 2x100 Watt and IMHO the carbon composite will have an very low amount of heat fluctuation if you use Sandwich-Panels with an simple plastic honeycomb "spacer" in between two thin carbon-composite sheets. IMHO this will also lower the weight of the structure cause the highest loading of the structure will surely come from the buckling due to the internal Air-pressure and an Sandwich-Structure can withstand this sort of loading better than an compact structure with the same weight. The only problem with an Sandwich-Structure is that it can debond if the internal Air-pressure in the honeycomb gets too high due to heating; at least that's what happened with the composite-tanks of the failed X33; but the latest test tanks withstand all testing without problems so this problem is solvable.
Manfred
Hi Dook;
I don't think that 4x4 is only available with the motors in the wheel.
OK, so this was only an misunderstanding. But I still find it an little bit strange that you don't want to spend the few additional bits and MIPS to support an more sophisticated 4x4 drive. I don't care if it is included in the vehicle or on MIL-Standard radiation hardened Laptops, but IMHO without such an system you will loose an lot of traction and/or energy due to the slippery soil.
I'm a little confused by your next paragraph. The hydrogen in the storage bottles supplies the fuel cells which combine hydrogen and oxygen to make heat, electricity, and water. Most of the water is then converted back into hydrogen and oxygen
OK, then forget about this paragraph. Again an misunderstanding from my side. I thought that you would use the Hydrogen only as fuel to feed the fuel-cells and the water supply of the Crew, but would not close the cycle ( H2 -> e -> H2 ). [Also see below]
Now the batteries (batteries=accumulators??) are Nickel Metal Hydride for the most part....
Yep at the moment NiMH seem to be the best way, but you should look about other types too. Even if you won't include the Alu-Accu's from Europositron, which I can understand very well, you should at least think about advanced Lithium-Accu's from the company FortuBat cause they already reach around 200-250 Wh/kg with the possibility to reach even 400Wh/kg in the future. The Accu's from FortuBat for example need less than 1/3 the weight and only 40% the volume of an NiMH-Accu to store the same amount of Energy. They promise that the Accu works down to -25°C, so I'm not sure if this is good enough.
Also if you use Accumulators with such an high energy density you can simplify your Hydrogen System and maybe use the Hydrogen only as an fuel cause the Accumulators would have enough capacity to store all the energy the solar cells supply. This would make it possible to use nearly all of the solar energy instead of loosing nearly 50% due to the hydrogen cycle too. This could be possible with the NiMH-cells too but I'm not sure if the capacity of the NiMH-Accus is high enough.
I knew nothing about the Europositron battery idea. The website did not give much information other than very high expectations (over 5 times that of lithium-ion???) of power storage.
Yep; so I really hope they can bring this technology to market, cause then Laptops, Handys, PDA's etc...would finally have an decent runtime.
The alkaline fuel cells have an efficiency of 70% the other 30% is lost as heat which is necessary to keep the inside of the vehicle warm.
Are you sure? I have only seen one rather unreliable claim of ~65% efficiency for an small fuel-cell until now. Normally fuel-cells with the correct size to suit your vehicle (normally used in cars) have only an efficiency of 50-55%. Only far larger units have an higher efficiency of 60-70% but this are roughly Multi-Megawatt-Units. Smaller fuel-cells always have an lower efficiency than larger fuel-cells.
believe your figures for the 800 mile range are only for one use of the stored hydrogen and oxygen.
Yes, because I was not sure if you would split the water again into H2 and O2 to fuel your Rover.
Argg... I just read this description. Well that seems to be an really complicated system. They even use 1100 Watt, or maybe up to 50% of the produced energy during low-power conditions to heat the fuel-cells to the correct temperature. WOW imho really inefficient. I was not able to find something about the efficiency of the Shuttle fuel-cells in the document.
Manfred
I read lately in the BIS-Spaceflight that even the gravity on Mars (0.38g) is not enough to sustain the bone mass or muscle's of people. At the moment they assume that 0.4g is the absolute minimum requirement for longtime health. I found this rather disturbing, so I hope they are wrong.
Heh. That mannamachinepic is a *very* thinly disguised joke.
Well at least you can buy an book about the Manna-Machine.
Look here : http://www.fernhouse.com/mannamachine.h … chine.html
Well, I don't want to talk about the strange theories of this guy, but IMHO the technology could really work. In Germany some companies already produce Algae that way, using small but long tubes filled with an Algae-Soup and exposing all that to sunlight. So if you substitute the Sunlight with highly efficient and tuned laserlight (quantum-point lasers are around 80% efficient) then it should be possible to shrink the system down quite a lot. This could make it possible to produce really healthy food in an very compact system. And because of that I mentioned the Manna-Machine as an way to produce (sort of) artificial food.
Well;
all this talk about artifical food reminds me a little bit about the old "Manna-Machine" using algae to feed the people. Maybe you should think in this direction when you think about artificial food. Algae are the best food available to mankind. So the best way to produce food could be to cultivate Algae like Spirulina or Chlorella within an machine or system. Algae together with Soya would certainly be good enough for most things we eat. The Algae could be used as the basic food and the Soya ( beans, milk, yogurt, cheese, tofu, tempeh, miso, shoyu ) to fill the holes and simulate a lot of different products like meat, cheese, milk etc....
http://www.fernhouse.com/mannamachinepi … nepic.html
http://www.soya.be/]http://www.soya.be/
Hi;
Thanks that you come back to Your Rover. I like it very much. Last time it was not possible to further dicuss a few things due to the strange behaviour of the Thread. I hope You don't mind when I start from this old point again.
Regarding the CFK/GFK-Wheels : Do You have an link for this sort of Wheels? I was not able to find something myself on the net. Thanks.
Regarding the 4x4 drive:
Propulsion: 4x4 is available but I think they should only use 2 wheel drive as long as it works to save power. Plus I don't like the motors being built into the wheels, too much vibration, mars dust, and you need some kind of slip ring to transfer the electricity to the rotating wheel. I still prefer the reduction gearbox idea because it is much more simple.
Why do you think the 4x4 drive is only available with motors in the wheel? I wouldn't alter your gearbox-design but would use 4x4 all of the time, but with an intelligent distribution of the load like it is used in modern cars. The Audi Quattro is an good example. Most of the time only the front wheels are in use to preserve fuel, but when the drivers needs 4x4 it works immediately.
I fear that an normal drive is not good enough for mars. The MER rovers for example have to work hard against the slippery soil despite their 4x4 drive. This will be even more of an problem for an bigger and heavier vehicle. So it could be that 4x4 needs less energy than an normal drive.
Regarding the hydrogen-fuelcells:
Water: I'll have to double check my figures but I believe the fuel cells produce quite a lot of water so the problem was too much rather than not enough. That's why I put in the shower.
Upps. I assumed that you use the hydrogen as an "battery" here being recharged each day from the solar cells; but it seems you use the hydrogen as an fuel only otherwise you would have to make sure that your water is always very clean so the Hydrogen-cells can work at top efficiency all of the time. For me it is a little bit odd to use the hydrogen only as fuel (on mars).
The amount of fuel stored in the Hydrid cells should be enough for an long ride so I think that's ok. With 700lb total weight for the hydrid cells I think the Hydrid itself will be arond 600lb. This 600lb can hold up to 54lb (=9%) of hydrogen when you use the new lithium-hydrid material now in development. This amount of hydrogen can hold 800-880Kwh of energy (not 100% sure if one Kg H2 has 33 or 36Kwh)
So you have around 500Kwh of available energy when the conversion efficieny is ~60% in the fuel cells, enough for >40h continous driving. So the range would be 800 miles @ 20mph.
IMHO one of the big problems with hydrogen fuel cells like the one in development for the Helios UAV is the low conversion efficiency. From electricity to Hydrogen and back to electricity you loose up to 70% of the primary energy. Even when you use highend equipment the combined efficiency of this process is only ( e -> H2 = 80%; H2 -> e = 60% ) 48% at the most. So even then you loose more than 50% of the energy you capture with your solar cells. IMHO thats not good enough for mars, especially when you take into account the low amount of solar energy available on the surface of the mars.
IMHO you will have to include emerging technology to make your Rover work as intended. The most problematic point seems to be the energy supply so the following to technologies could help you here :
Solar Cells with ~50% efficiency :
http://www.lbl.gov/Science-Articles/Arc … ...ll.html
http://www.stp-gateway.de/Archiv/archiv … 923-e.html
If this sort of Solar cells are developed in time, and at the moment it seems so, then you could generate 2.5 times the electricity per m²
Energy storage with Alu-Accumulators:
http://www.europositron.com/en/techniqu … iques.html
Here you can both improve the efficiency of the energy conversion from the 48% with the Hydrogencells to most likely 90-95% with the Accumulators and reduce the weight of the Rover cause the Alu-Accumulators can take over the task of the hydrogen-Storage System and the NiMH-Accumulators in one lighter System.
Manfred
Approximate solar cell power estimate:
http://powerweb.grc.nasa.gov/pvsee/publ … insolation available = 3 kW-hr/m2 per day
A 100 m2 averages out to 12KW.
Pulling a large solar array or several would be sufficient.
IMHO you have forgotten to include the efficiency of the solar cells. With GaAs-Cells with ~20% efficiency you would need around 500m² for the 12 KW.
Sure you can do *a lot* of preliminary stuff, but a spinning tether (A.K.A. Skyhook) , while using similar hardware, is not a Space elevator, the dynamics are totally different. Space elevator has one fixed point on the surface, Skyhook has none, for starters...
I don't agree.
IMHO you can use Tethers for much more than an "big" space elevator only, and you don't have to wait for the big breakthrough to get long and perfect nanofibres to make all the other systems work. Most of them work with todays materials or with slightly better fibres. Look at http://members.aol.com/Nathan2go/]this site. Here you can find a few rough suggestions what is possible today without waiting for the future to happen.
I'm afraid there's no such thing possible as a small scale proof of concept...
Sure you can do it.
Start with an spinning tether facility in Low earth orbit like the one in development from http://www.tethers.com.]http://www.tethers.com. Links:
http://www.tethers.com/LaunchAssist.htm … ssist.html
http://www.tethers.com/papers/HASTOLAIA … APaper.pdf
When you have gained enough experience you can move on to an real tether in low orbit. Links:
http://www.affordablespaceflight.com/]h … light.com/
[edit] forgot this link : http://members.aol.com/Nathan2go/]Space Tethers for Space Tourism
From here you can start build an complete tether.
With this incrimental approach you gain already a lot cause you can reduce the speed requirement to reach orbit from 100% down to ~70% so the payload for such an suborital SSTO or better SSTS vehicle would be far higher than with an normal SSTO or any RLV. This in the end will lower the price for payloads so much that the building of an tether in GEO-orbit becomes feasible.
M2P2 is an nice technology cause it's acceleration does not depend on the distance to the sun, and you can "transform" a mere 20KW of plasma-power into 500times, or 10MW of propulsion. So an M2P2 is really efficient.
What do you mean by that? "Watts of propulsion" does not really have any meaning. Thrust is measured in Newtons (1 Watt= 1 Newton meter/second).
Edit: John Slough seems to be using 1 "propulsion" MW= 2 Newtons. This is somewhat misleading, by this standard the 60% efficient Deep Space 1 ion drive would have actually been 2000% efficient.
What do you mean by that? "Watts of propulsion" does not really have any meaning. Thrust is measured in Newtons (1 Watt= 1 Newton meter/second).
I mean, or better Slough means that you need only a 20KW plasma-source to get the same amount of thrust as with an 10MW propulsion unit otherwise. I think he talkes about ion drives here but he does not specify it.
Edit: John Slough seems to be using 1 "propulsion" MW= 2 Newtons. This is somewhat misleading, by this standard the 60% efficient Deep Space 1 ion drive would have actually been 2000% efficient.
Really? Don't you forget that the M2P2-propulsion has an far higher specific impulse as the simple ion drive like in DS1. You cannot only count Thrust, you have also include the specific impulse here. Slough imho uses an virtual "exhaust velocity" of around 800km/sec or ~80000 sec for the M2P2 [this is an guess, I have not checked the slides, but the equations work] but the DS1 has an specific impulse of only 3000 sec AFAIR.
Theoretically if you would decrease the specific impulse of the M2P2 from 80000 sec to 3000 sec the Thurst would increase from 2 Newton to ~53,3 Newton. This an simple and crude calculation only using the equations Wkin=m/2 * v² and F = m*v with v= exhaust velocity so the result is not correct but should be in right ballpark.
Oh, M2P2 is rather "old" news now.
They have an NIAC-contract since a few years an I read all the tech-pdf's about the M2P2 on the NIAC-homepage.
M2P2 is an nice technology cause it's acceleration does not depend on the distance to the sun, and you can "transform" a mere 20KW of plasma-power into 500times, or 10MW of propulsion. So an M2P2 is really efficient. The highest velocitiy you can reach with the M2P2 is the velocity of the sunwind, or around 800km/sec which is not enough for interstellar travel, but really good enough for stellar travel.
Link1 : http://www.niac.usra.edu/files/library/ … pdf]Plasma Magnet ~ 5.5MB
second link : http://www.niac.usra.edu/studies/ [look for Slough, John]
Thanks for the link to the "dusty" M2P2. I didn't know about that..seems even better than the normal M2P2.
Also, mboeller, do you have a link for Ion-Wind drives? I google'd to no avail.
Sure;
One of the best know Ion Wind Drives was called Ionocraft 40 years ago. Here is an really good description of it :
http://www.rexresearch.com/desev/desev. … /desev.htm
I hope you don't mind the overall source, but this page is IMHO really packed with informations.
Hi;
based on the ATO-Handhout from JP-Aerospace and the following page [ http://www.grc.nasa.gov/WWW/K-12/airpla … t.html]air density ] I tried to figure out if the ATO is possible or not.
Basics (see link) :
air-density @ 140000 feet = 0,002675 kg/m³
air density @ 200000 feet = 0,000271 kg/m³
From the Handout it seems the DarkSkyStation has 5 fingers each around 2000m long with an diameter of around 125m
So the Volume of the Station is 122718464,8 m³. That means the Station can weigh up to 328 tonnes, which is imho an reasonable figure.
The ATO reaches an max. height of 200000 feet using buoyant lift only. The ATO has only 2 "wings" with an length of around 1800m and an diameter of ~110m ( this is an upper figure, cause as it seems the "wings" look more like real wings in reality ). The Volume of the ATO is < 34211944,5 m³ then.
So @ 200000 feet the ATO can weigth ~ 9280 Kg at the most. If the wings are elliptical then the volume and the buoyant lift is even lower.
IMHO the ~ 9 tonnes for the ATO seems far too low to support an nearly 2km long vehicle with ion drives, fuel, structure, and payload.
So I have to ask, are my calculations correct, or not?
One final remark;
IMHO the ATO cannot use an normal ion drive to reach LEO, cause then the weigth of the fuel would be too much for the ATO.
So maybe JP-Aerospace use an alternative drive. I think two different systems could work :
1,) Ion-Wind Drive. This sort of Ion drive uses the surrounding air as fuel and accelerates this air with HV-electricity to accererate the vehicle. An german university tries to use this sort of engine to propel small UAV's, so imho this is an viable alternative.
2,) Plasma-Skin Drive. This is an real black-world-drive. So far not much is known about it. The Plasma-Skin-Drive is also able to mask an aircraft from radar, so most of the work is done from the military and hidden. I have found only one sourse of open informations : http://jlnlabs.imars.com/plasma/html/s_ … dpthr1.htm I'm not sure if this will even work, but it matches the comments from JP-Aerospace about their drive quite good IMHO.
The first post of that topic somehow got borked, now the second post froze as well.
Hi Dook;
I still have the old thread "Simple Mars Vehicle" saved on my computer. I can open an new Thread with all the old posting's inside as the first posting if you like.
Manfred
Sorry, I have no direct Information about the Light-Craft, but when you are interested in general Laser-Launch informations then maybe this link is for you :
http://www.niac.usra.edu/?link=mar04_mt … ...ows_mtg
Look at the bottom of the page :
Jordin Kare: Modular Laser Launch Architecture: Analysis and Beam Module Design
The PDF has ~1.3MB
They are already working on self replicating robots for Luna so maybe they will be available when we finally settle on mars :
http://www.niac.usra.edu/?link=mar04_mt … ...ows_mtg
Look for the PDF from Gregory Chirikjian; he has done a lot with his LEGO bricks (!).