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The only way for an object to orbit the sun in a circular orbit every 365 days is to be in the same orbit as Earth. If something is further out, it's got to move more slowly.
Wow, do these require monochromatic light or do they work on full spectrum? I'm just wondering if these would be effective at converting sunlight?
EGADS, what is it with all this really cool spacecraft propulsion tech at my own university I was unwaware of?
First it's M2P2 and now this PMWAC drive that were right under my nose!
This PMWAC really has my interest piqued, do you have any direct comparisons between this tech and VASIMR? They both seem to be high efficiency, variable Isp drives. Is there any clear advantage of one over the other?
ecrasez - NASA loves to brag about the expensive innards of their spacecraft. In the otherwise virtually unreadable commercial spacecraft company fiction that was recently posted on another site, there was an interesting anecdote about reentry shields. NASA made a big deal about how much temperature and energy the reentry shields would have to withstand. It turns out that all the Apollo reentry shield was made out of was a honecomb grid filled with the equivalent to high grade bathroom caulk.
Although spinning stuff like that is impressive, I can't help but wonder if NASA is shooting itself in the foot these days with talk like that. The average layperson just sees NASA bragging about how it's sattelites are made of gold and diamonds and then wonders why we can't seem to get the national budget balanced.
Honestly, modern jet engines on a 747 or your computer processor have just as many fantastic and amazing materials in them these days as anything NASA makes. NASA would be well served, IMO to stop playing the dazzle card if they want people to stop complaining about how much money they soak up.
GCNR: ??? I think the discussion was less about space based gem manufacturing but rather the use of precious materials in space probes.
I'm too lazy to go back to our old LEO to Mars thread and look up my calculations but if one posits a dry spacecraft launch and LEO fuelling, even standard chamical engines can throw something like 60 MT to Mars without too much trouble with a 120 MT liftoff cargo mass. If you start playing with things like ion drives and low energy transfer orbits (for non-perishables) your Mars cargo load starts approaching your LEO capacity.
As for accurate landings, NASA has been consistently improving their landing accuracy, Spirit and Opportunity were both pretty accurate throws. Also, the Mars 2008 orbiter (MRO) will have an optical camera/UHF transponder system that will greatly improve the ability of incoming spacecraft to figure out their location in space, further improving landing accuracy. If there's a landing beacon and nothing catastrophic happens in the orbital insertion, I don't see why we can't drop a payload on Mars within a 1 km oval.
For an example, look at Gravity probe B. It had a 1 second launch windown and ended up hacing a postitional accuracy 6 times what they were expecting. We've got the technical capacity to make it happen and NASA is already obviously planning on using that capacity to the fullest.
GCNR: Lift is produced by displacement. If an object is lighter than the air it displaces, it rises. Assuming a constant skin mass, the best lift will come from a vacuum inside the object. Until recently, the problems of air pressure collapsing the object and gas leakage into the object were too great. However, recent advances in polymer tech and so on have started to make this sort of stuff practical. The best way to do it is probably have a small cell foam of a high strength material. Smaller cells have a proportionally higher resistance to being crushed (although at a proportionally higher skin mass). The ultimate building material would be something like a carbon aerogel (which has recently beeen made but I don't know what the material properties are other than it's slightly magnetic for a few hours after creation) with a metallized skin around it.
As long as your skeleton materials and skin are light enough, such a balloon could theoretically go much higher than helium balloons. Although I'm highly dubious about the use of floating structures as launch pads, these superballoons could be used as high altitude astronomical platforms, etc.
The reason you see such precious materials being used is that some of them have nice properties and so, since weight is at a premium and the costs are so high anyway, you might as well splurge on the good stuff.
quartz - not a precious material, per se - quartz is just ordinary, high purity glass that cooled more slowly and so has a crystalline structure. Quartz has very nice optical qualities and very predicatable thermal expansion. It passes all light from fairly deep in the IR down to about 190 nm in the UV which makes it ideal for lenses and such.
diamond - very hard, clear and the best thermal conductor in existence. It is also one of the best electrical insulators in existence and therefore makes a fine substrate for very expensive computer ships that need to be resistant to radiation damage.
gold - a very good conductor, doesn't oxidize or rust or react chemically with other materials. Many somsumer electronics have gold on the electrical contacts for this reason.
silicon - not a precious material, basically purified beach sand. It's used for making computer chips. In that capacity, it is the single most pure material on Earth by far. Modern semiconductor tech requires silicon that has impurities in the part per trillion range.
sapphire - actually just aluminum rust. emeralds and rubies are sapphire that has various impurities in it. Useful because it is very hard and has some good optical properties.
An equatorial launch site doesn't necessarily mean an equatorial inclination, however. If the ISS were in a 22 degree inclination (or whatever KSC is at) It's simply a matter of Kourou having their rockets launch off at that angle to rendesvous with ISS. At 22 degrees off the equator, almost no cargo capacity is lost for the ESA and RSA so it would make sense for them to maintain a station at KSC inclination.
Sorry, I just moved and so all my stuff is still largely in boxes. If I find the latest Science and Sci Am, I'll check. In the meantime, check out this http://einstein.stanford.edu/]link. Go to the 'what is gp-b' then 'story of gp-b' and check out page 4. The diagram isn't as good as what I saw but still gives a good rundown. The whole 'story of gp-b' link is the best resource for getting info on GP-B. It gets a bit technical at points but is well written.
Incidentally, I found out that Gravity Probe A was launched back in 1976.
So, does this mean we can send up a motor module and push the orbital inclination of the ISS back down to something that makes even the tiniest bit of sense? Of all the compromises that tick me off about the ISS, the worst was how we sabotaged our own cargo capacity, safety of our astronauts and the functionality of the station that we largely paid for by accomodating the Russians by putting the ISS in that stupid 55 degree inclination orbit.
Why bother with gasses? Fill your 'airship' with vacuum. I know that my low temp freezer at work uses vacuum filled insulation, greatly reducing the wall thickness required. I'm not too faniliar with aerogel strength but could one simply evacuate the aerogel and cover it with a thin metal film? You'd greatly increase the lift capacity of an airship if there was no gas inside of it.
The problem with nukes is that you lack very good control. a few nukes could get the asteroid moving in the general direction of Earth orbit but you'd need to have some sort of conventional propulsion system to maintain proper control of the thing.
Interesting. I know that back in the 60/70's, in a bit of misguided PR, the US military tried to sell their 100 megaton hydrogen fusion bombs as 'humane' nuclear weapons because of the low fallout.
If it weren't for the fallout from the fission portion of nukes, the old 'plowshare' nuclear programs for building things like canals would have been quite useful.
The problem with those tabletop drive is that they would also produce essentially no thrust, even by ion engine standards. For a fusion drive to work it has to at least be in the neighborhood of breakeven or you might as well be using a standard ion engine with all the power you have to pump into the system.
The primary use of amorphous metals is in high temperature turbine blades. At the temperatures and speeds they operate at, the blades inevitably start stretching out like taffy and need to be replaced on a regular basis. Normal metals are composed of small crystallites that tend to stretch differently on the different axes. The internal stresses and defects that result can result in failure at the grain boundaries.
The two solutions are to either use single crystal blades where the entire blade is one big metal crystal or to use glassy amorphous metals where the whole thing is disordered and therefore doesn't have any crystalline boundaries in it. These days I think that amorphous metals are used more commonly because it's cheaper to make. Basically, you take molten metal, drop it onto a very rapidly spinning disk so that it's splattered into tiny droplets that then plunge into liquid helium. The cooling rate of millions of degrees a second prevent any crystal formation. The powder is them cold pressed into the final desired shape.
In contrast, single crystal metals are formed by taking a small seed piece of metal that's attached to the rest of the blade by a small channel that looks kind of like a pig's tail. The metal starts crystallizing on the seed as they progressvely cool the metal and the curlique channel causes all but one of the crystal grains to eventuall run into a channel wall and die out. The single crystal then grows out of the channel and into the die where the blade is sitting. Through very careful control of the temperature, you can ensure that the entire blade is a single crystal of metal - not easy to do.
Also, many of the so called nanomaterials really don't need nanotech to be created. For example, carbon nanotube composites are made with furnaces. These nanotube composites won't get you a space elevator but will give you materials with a strength to weight ratio much higher than steel.
Diamond is also starting to become a possible building material. New vapor deposition techniques can grow a gem-sized diamond in a week or two. The process can be scaled up arbitrarily. Although large diamond structural elements would still be horribly expensive, it entirely possible that in 20 years we'll see spacecraft with diamond and nanotube construction that weigh 1/3 what a current craft does.
The thing is that hydrogen is quite easy to spot. You look for certain spectroscopic absorption lines (Lyman Alpha lines, IIRC) that tell you where and how much hydrogen there is. There are areas of the galaxy that have high concentrations of gasses but unfortunately none of them are very conveniently located.
A Bussard ramjet would work but the problem is that you need a magnetic field generator that is far more powerful than anything we currently can make or can even think about making. It also requiresthat you are already going a significant fraction of the speed of light. If a bussard ramjet could be made to work it would be the most effective spacecraft drive in existence since it doesn't have to carry fuel along with it.
This is an idea that's been tossed around and if it worked, would be great. You'd probably want to work with one of the near-Earth asteroids since it greatly lowers the amount of work you have to do to bring it into Earth orbit.
The big problem (besides the huge rockets necesary to do this sort of operation) would be the consequences of messing it up. Dropping a big asteroid on Eath because you made an 'oops' is a very real possibility.
The Plank scale is something entirely different - that's supposed to be the fundamental quantum unit of length, something like 10^-35 m or something like that. A Plank length to an atom is equivalent to an atom vs approximately 10% of the entire observable universe. Very small.
Quantum effects are something one tends to see at under 10 - 20 nm or so. One sees things like surface plasmon confinement effects on metal particles below about 20 nm in diameter. True 'quantum dot' effects kick in for semiconductors at 5-10 nm and for metals at 1-2 nm. Things like electron position uncertainty are only a problem below a couple of nanometers.
For example, part of the reason that chips run so hot these days is that there's a lot of current leakage from the transistor gates into the circuits. Presently, the SiO2 insulator seperating the gate from the rest of the transistor is less than 5 nm thick. The use of high K dielectrics for the gate insulator allows the ates to be made thicker again, lowering current leak but is probably boing to be the eventual show stopper for current microprocessor tech.
The real advance tha a lot of people mistake for nanotech is self assembly. The ideal way to buidla computer is like how living organisms assemble themselves - through tiny subunits that put themselves together. Unfortunately, our knowledge of how to do this is still very primitive.
The exact composition of the Earth's core is speculative but we can make educated guesses. Seismic mapping has given us very detailed maps of the density of the core from which we can infer something about the composition. Furthermore, we can also infer a lot about the mantle and upper core composition from magma in eruptions. Ratios of helium isotopes tell a lot about the overall readioactivity of the lower layers of the Earth and we know that there is a lot of radioactivity going on.
The tidal infleunce of the Moon also probably contribues although I don't know the relative ratios of the two in contributing to the heating. Since most of the references refer primarily to the radioactive heating, I assume that the rads do the majority of the heating.
The fusion research community is highly politicized. The tokomak folks have basically taken over and any alternate designs have been marginalized, relying on shoestring budgets to keep operating. On one hand, the tokomak design is the most promising but on the other, the tokomak design has some serious issues which really recommend that we keep looking at alternate issues.
If you look for a history of the Fusor design, it's clear that it was internal company politics rather than design flaws that killed mainstream fusor research. Although ir's quite possible that the fusor design is inherently incapable of breakeven, there's no reason why it should be ignored as much as it is.
There's something along those lines going on. Right now, there's no way to easily treat mixed radioactive wastes. (mixed rad wastes are things like toxic organic compounds that are also radioactive and therefore need to be detoxified but are too radioactive for safe handling with the standard detoxification techniques.) D. radiodurans is being engineered to put the genes for breaking down organics like carbon tetrachloride into it so that you can use bioremediation on the mixed wastes. It's slow going, I know Lidstrom's lab's been working on their D. radiodurans projects for years now with very little success. The wierd genomic structure of radiodurans probably futzes up a lot of standard genetic manipulation techniques.
Having been offline for a week or so, I don't know if this came up in discussion yet:
http://www.space.com/news/us_china_040428.html]link
It turns out that the Chinese designed their capsules to be able to dock to ISS. They approached NASA to do joint missions but NASA basically told them they didn't know what they were doing and to take a hike.
The problem with superconductor rings is that the energy density is not that great. Even traditional low temp superconductors break down at really high magnetic fluxes. Cuperconductor rings are used for things like building sized UPSs but you're better off using something like methanol fuel cells for high energy density.
As much as I'd love to throw in behind that theory, molecular cladistics (tracing evolutionary lineage by looking at DNA sequences) shows that D. radiodurans is a pretty ordinary bacterium.
For a while, it was thought that its really wierd quadruple nucleoid DNA structure and incredible double strand DNA break repair ability was the source of its radiation resistance but recently, evidence has come out that calls that into question.
Unfortunately, whatever gives radiodurans its rad resistance, it's probably quite compatible and not something that would work with human DNA.