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Most of the discussion has been about avoiding heat. Heat is relatively easy problem compared to radiation. Mercury has a magnetosphere like Earth. That means that cosmic radiation rains down constantly on both day and night side. Not only are the solar winds over 6 times more powerful in Mercury's orbit but it has no atmosphere to shield anyone on the surface. With the amount of radiation it is exposed to it is likely the entire surface of Mercury itself emits harmful levels of radiation. The only manned mission I could imagine is is one that directed robotic operation on the surface from Mercury's L2 point with the Sun. This would only be true if this did provide enough protection from most of the Sun's radiation.
JCO wrote:Colonization will not begin until we have enough exploration data to make a good guess about a colony location. Any colony that is attempted before then is doomed to certain failure. That said Mars "covered wagon" colonies to explore secondary site sound like a very good idea to me. Though initial exploration will provide enough data to choose a site with a very high chance of a successful colony it will not find prime locations for a colony to thrive. A mobile colony seems like a good idea of a way of prospecting for a prime location.
"Certain failure"? That's the sort of "Beyond there be dragons" mentality that kept medieval Europe constrained.
Your idea of the colonisation process sounds very Earth-bound. We aren't looking for lush pastures - because there are no lush pastures on Mars. We are simply looking for somewhere that has flattish ground, not too polar with ideally some good water, clay and iron resources close by.
No it is my prediction of the outcome of anything like Mars One if they actually do succeed in landing people on Mars. Without proper exploration missions attempts at colonization will almost certainly be lethal. In point of fact the reason map makers put "there be dragons" was not because of any belief in dragons but because most people who strayed from mapped territory never returned. They did not think dragons ate them but they may as well have as far as they were concerned.
JCO wrote:What your[sic] saying is you are coming up with the number on the fly and you have no real source.
What I'm saying is that developing the technology to the point where we'll actually be able to build a space elevator is going to be expensive, and my numbers were meant to show how that can easily sink the viability of a space elevator project. I used numbers because I thought they would convey this more clearly than words, I guess I was wrong in saying that. It doesn't matter that I made the numbers up because they're a way of explaining my claim. They are not themselves the claim. They could be off by an order of magnitude or more and my point would still be made, because the point is fundamentally valid: Space elevator technology is not present-day technology.
Your statement was presented as a cost benefit analysis. When I presented sources that suggested that your estimates were way off base and pointed out that you had provided no reference you followed up with a statement that you stood by your numbers. The only thing your number make clear is your lack of knowledge about the subject and your unwillingness to look at expert opinion.
JCO wrote:Your opinion is that the concept dreamt up by a fiction writer with a Master in english is a better technical authority than Dr. Bradley Edwards a former NASA engineer.
What are you talking about? I'm not treating KSR as a technological authority on anything. Again:
I wrote:I think Robinson may have dramatized that a bit
If you're citing that book, as it appears you are (?) then good. But I still think it's a concern. I don't see it addressed in that book. in a quick skim. It's definitely a concern worth considering, but given that we don't know what the tether is to be made of it's almost impossible to answer.
I was actually responding to a later quote of yours.
Regarding your second post: I don't think KSR had an accurate depiction of the fall for just that reason. But this stuff is going to be very tough stuff. It will come to the ground, and it's long enough to wrap around the Earth. The equator cuts through Indonesia, the fourth most populous country on Earth. Densely populated parts of India, Sri Lanka, and Southeast Asia are within ten degrees of the equator, as well as most of the Philippines, some of Brazil and the equatorial regions of Africa (Like the DRC and Kenya).
What I was citing was actually this source from a recognized expert in the field http://www.mill-creek-systems.com/HighL … tml#impact
Depending on the location of the break, the epoxy used, the dynamics of the fall, etc. the cable will re-enter the Earth's atmosphere at a velocity sufficient to heat the cable above several hundred degrees Celsius (figure 10.9.1). If the cable is designed properly, the epoxy in the cable composite will disintegrate at this temperature. This means the cable above a certain point will re-enter Earth's atmosphere in small segments or carbon nanotube / epoxy dust. About 3000 kg of 2 square millimeter crosssection cable (20 ton capacity) may fall to Earth intact and east of the anchor. Detailed simulations will be required to determine the possible sizes of segments that will survive and the health risks associated with carbon nanotube and epoxy dust. In terms of the mass of dust and debris that will be deposited, we can compare what will happen to what naturally happens now. Each year 10,000 tons of dust accrete onto Earth from space, the additional 750 tons of the first cable will increase that year's infall by 7.5%. A larger 1000-ton capacity cable would have a mass of 30,000 tons or roughly equivalent to 3 years of normal global dust accretion. Further investigations are required to determine the environmental impact of depositing this much dust along the Earth's equator.
Which includes a chart that makes it clear your concerns of even reaching Indonesia are completely groundless.
JCO wrote:For someone who claims to find the idea interesting you seem to have surprisingly little real knowledge of it. You sound more like someone who hates the idea and is inventing reason why it would not work.
One of the main reasons for the extremely limited progress in the past 40 years in space is because of an attitude that it is just not worth the effort. You mentioned the Panama Canal, one of the reasons this took so long to be realized is just that, too few thought it was worth the effort. I think Clarke was right, the SE will happen once the fools stop laughing.
I consider myself to be a realist. Often this is interpreted with pessimism. My focus is on details and technology and things that have been proven because I like to get into the nitty-gritty. If the details aren't there, I'm skeptical.
So: I think that tethers of all kinds for use in space are awesome. I think that arbitrarily low prices are awesome. I think that in the long run a space-elevator like system is how we're going to get there. But I don't think that the space elevator is something we're ready to do. If that makes me a fool or an ignoramus in your eyes then so be it.
My problem with your objections is that I have been providing specific details and you have not. You have based your opinion seems to be based on a 20 year old fiction an personal assumptions of the potential cost. You have failed to understand the difference between engineering specification for a specific use (standard building elevator cable) and scientific measurements of material properties (tensile strength).
I myself am a skeptic but I recognize the potential of ideas and their actual limitations. Some years ago I attended a talk by Dr. Edwards about the SE. At the time I expressed my doubt that it would ever be used to transport people as it would mean being cooped up for an entire week. I got the answer that they would be willing to do just that. Technology is not currently the real obstacle for the SE it is the gulf between the people who have no money who risk anything to get to space and the people with money who will use the Panama canal once someone else pays to build it.
Colonization will not begin until we have enough exploration data to make a good guess about a colony location. Any colony that is attempted before then is doomed to certain failure. That said Mars "covered wagon" colonies to explore secondary site sound like a very good idea to me. Though initial exploration will provide enough data to choose a site with a very high chance of a successful colony it will not find prime locations for a colony to thrive. A mobile colony seems like a good idea of a way of prospecting for a prime location.
I think floating craft in the Venus atmosphere is a good logical next step. I fully agree that this is something that must involve robotic missions well before we hope to send people. It should be fairly simple to send a probe there with a supply of liquid nitrogen that would be used to inflate a balloon after atmospheric entry. It would also be a procedure that was easier to test before launch as it would be all but identical to having a vehicle reentering Earth's atmosphere inflating a helium balloon before touch down. Unlike landing on the Moon or Mars we have an almost perfect analog environment for testing.
Lifting body drones could be used to 'orbit' Venus within its atmosphere and provide an exceptionally detailed radar mapping of Venus's surface. The main probe would provide an opportunity to for the first time study in detail the meteorology of another planet.
The article says they will try again.
http://www.space.com/28484-spacex-rocke … llite.htmlSpaceX will attempt to land the first stage of its 14-story Falcon 9 rocket after launching the Deep Space Climate Observatory (DSCOVR for short) from Cape Canaveral Air Force Base in Florida. Liftoff is set for Sunday, Feb. 8, at 6:10 p.m. EST (2310 GMT) and will be webcast live by NASA TV.
Here is hoping 2 is the charmer.
Regarding your first post that I was making those numbers up I offer the following pre-sponse:
I think it's excessively clear what those numbers were for, seeing as I said it four times.
I think that the development of metamaterials stronger than anything we've ever seen before is going to be expensive. I think it'll be very expensive, because it necessitates developing substantial nanotechnological capabilities and experience. I think that the amount of profit that can be gotten from a space elevator is small even if the magnitude of the annual payload is huge.
What your saying is you are coming up with the number on the fly and you have no real source.
Regarding your second post: I don't think KSR had an accurate depiction of the fall for just that reason. But this stuff is going to be very tough stuff. It will come to the ground, and it's long enough to wrap around the Earth. The equator cuts through Indonesia, the fourth most populous country on Earth. Densely populated parts of India, Sri Lanka, and Southeast Asia are within ten degrees of the equator, as well as most of the Philippines, some of Brazil and the equatorial regions of Africa (Like the DRC and Kenya).
Your opinion is that the concept dreamt up by a fiction writer with a Master in english is a better technical authority than Dr. Bradley Edwards a former NASA engineer.
For someone who claims to find the idea interesting you seem to have surprisingly little real knowledge of it. You sound more like someone who hates the idea and is inventing reason why it would not work.
One of the main reasons for the extremely limited progress in the past 40 years in space is because of an attitude that it is just not worth the effort. You mentioned the Panama Canal, one of the reasons this took so long to be realized is just that, too few thought it was worth the effort. I think Clarke was right, the SE will happen once the fools stop laughing.
Still, I'd like to develop a pencil that can be used in freefall, simply for any artists who decide to take a trip. Perhaps an ink consisting of graphite particles in suspension?
What you are talking about is called a grease pencil. Artist know it well. They also come in mechanical pencil varieties that would likely pass muster in space.
I think Robinson may have dramatized that a bit, since the cable will not actually be all that big. Even at just* 65 GPa, an elevator which could support 100 tonnes under Earth's gravity would have a cross-section of about 1.5e-5 m^2, or put another way it would be a string with a diameter of 5 mm. He described it as being something closer to 10 m.
Having said that, the small theoretical size does beg the question of how exactly one is supposed to affix large masses to such a small tether.
*Given the discussion we're having here, 65 GPa is indeed a low failure strength in context
Though I did enjoy the Mars series one thing to remember here is that Kim Stanley Robinson is not an engineer. He proposed a clever but unworkable design for an ES in the series. The actual design of the ribbon (not a cable) will likely be more like about a meter wide and less than a millimeter thick. The question of what would happen if the ribbon failed depends a lot on where the cable failed and what was done.
For example if the cable were to fail at or near GEO and nothing was done it would begin to fall to Earth. This would be caused by the fact that a majority of the mass of the elevator is traveling much faster than the earth is spinning and as the tension from the anchor pulls it closer to Earth it would begin to accelerate relative to the Earth's surface. It will only a few hundred miles before it reaches supersonic speeds at which point the ribbon will likely disintegrate. At that point the average velocity of the ribbon above ground will be much greater than needed to maintain an orbit and it will drag the part of the ribbon above the point of disintegration up into space. This would be a worse case scenario. As the elevator anchor is proposed to be several hundred miles out in the pacific it is very possible the major danger would be to aircraft in the direct path of the ribbon for about 1,000 miles. As this would take hours to happen a simple solution to this is to release the anchor and let the ribbon be pulled into orbit.
For the most part an SE would be designed for cargo as it would take up to a week to get to GEO on it. Climber could be designed with quick release systems and small attitude adjustment thrusters to allow cargos to move to safe orbits for retrieval later.
1) Space elevator
Research and Development costs: $450 billion
Construction costs: $50 billion
Operating profit: $1 billion per year
Lifetime: 25 yearsTotal costs: $500 billion
Total Profits: $25 billion
Net return on investment: -$475 billion
Annualized return on investment: -16.2%2) Much Cheaper Chemical Rocket Technology (e.g. reusability, or SSTO, or whatever)
Research and Development costs: $4.9 billion
Up-front Construction costs: $0.1 billion
Net increase in annual profit: $0.5 billion
Useful lifetime for this technology: 15 yearsTotal Costs: $5 billion
Total (incremental) Profits: $7.5 billion
Net return on investment: $2.5 billion
Annualized return on investment: +5.5%It is my claim that these numbers are representative of the costs associated with each of these two options. It's all about the money here. Realistically, because the space elevator would need to charge more money to make up the costs associated with building it, it wouldn't be able to create a reduction in the cost of sending payload to orbit.
I would like to note that your numbers are pure invention. You have sited no source and make multiple assumption such as the life span of the ribbon (I will stop calling it a cable because no one thinks that will be the design). I think you have drastically over estimated the cost of the elevator and underestimated rocket development.
The current projected development cost for the NASA SLS is around $40B.
http://en.wikipedia.org/wiki/Space_Laun … gram_costs
The space elevator has been estimated to cost a similar amount is estimated for development AND construction of the SE. The numbers are from a 2003 proposal but it allotted almost $5B to launch and boster to take the initial payload to Geo. By the end of this year the Falcon Heavy will have flown and will be able to deliver the entire in as little as one launch for the cost of $85M. This would be a reduction of $4B in the estimated costs. so even if other costs are higher it is likely to cost less than the SLS as this proposal includes an assumption of a 100% cost overrun.
http://www.mill-creek-systems.com/HighL … ter11.html
http://www.spacex.com/about/capabilities
My own preference is for very simple solutions. They usually cost less, which makes them more probable. Footholds and strap-your-self-down points at strategic locations are pretty well-proven and easy-to-do.
Often I like to "think Russian". Example: back in the 1960's, NASA spent several million dollars making a ball point ink pen that could function in zero-gee and in vacuum. The Russians used pencils (and solved the sharpenings-containment problem instead, pretty much with a simple enclosed sharpener).
GW
That has always been the Russian strategy quick and simple. The first satellite was a radio beacon. The first animal in space burned up on reentry as intended. The problem with this way of doing things is you do not learn much doing this way. They ran into a hard wall of what they could do quick and simple and have really gone no further.
There are fundamentally two sources of investment capital: Private and Public. I'll look at private first, because it's the default source of investment capital.
My basic contention is that your statement that "it is too good for its own good" is another way to say that the current demand for launch services doesn't justify the construction of a space elevator.
I do not take this personally but this did seem to provide a large number of examples of the assumption that it is impossible. Your statement that it was another way there was not enough demand for it seems to ignore the fact that I went on to say just that.
Comparing it to the highway system I think is a huge distortion of the scale. The main thing it ignore is the fact that the entire mass of the ribbon (cable) would be less than any of the numerous record breaking high rises recently built. The scale of the project would be epic but well within our current engineering capacity.
Your discussion of cost is for the most part choosing numbers. From what I have heard SpaceX hope to reduce launch cost by an order of magnitude. SE advocate suggest that it could reduce launch cost by 2 orders of magnitude. Also the cost to build payloads would be reduced by the fact that they would not need to be constructed to deal with the stresses of a rocket launch.
There's this pervasive myth among space elevator advocates that the only remaining impediment to building an elevator is finding a cable strong enough. I would like to make it exceedingly clear that this is very wrong.
Here are some other major technological hurdles to building a space elevator:
The fact is that all your technological hurdles are only engineering challenges. The ribbon is the only thing that is impossible today, we have yet to develop a material that is strong enough. Also you have a major factual error, the 350 km break length should actually stated as a sea level break length. It is stated that way because it is a way to ignore the change in gravity with height. A material would actually only need a 5,000 km sea level break length to reach GEO. So the T1000 fiber would only need to be 15 times stronger. Still a long way to go but a lot more doable.
Most of your "Technical hurdles" relate to ribbon failure. You discuss it as if you are unaware that the issues might have already been considered. For example cable designs that are more robust so micro meteor do not cause failure are being developed for use with currently available fibers because NASA intends to make use of tethers.
Your argument that it will have to be stronger to carry passengers assumes it will carry passengers. This is a myth of many space elevator advocate. It is very likely that a payload on the SE will take one week to reach GEO. It will take an hour just to reach the edge of the atmosphere. Unless it is as a tour bus to the edge of space I do not think many people will be riding the SE. The SE will be a cargo train, rocket will be the passenger planes.
I think another factor in the lack of development of this type of boot is the scale of the station. There is not a great deal of surface to walk around on. Also the science fiction back then assumed that moving in zero G would be like walking. In truth standing vertical would tend to just put you further from what you will likely need to work on. I think the 'gecko' like pads would be best placed on the side of the glove away form the thumb, elbows, knees and toes. This would provide the ability to climb/swim around the station and provide a variety of ways to anchor your self to do work.
I am sure someone has posted this some time in the past. In the long term I think this will be the best solution for getting to Mars. I have a theory on why it has attracted so few backers. It is too good for its own good. What I mean by that is it would work so well it would put itself out of business. A small design could lift 5 tons a day. In the first year of operation it would be able to lift almost 1,800 tons to GEO. That is more than ALL the payloads currently scheduled globally. Most of those payloads will not be ready to lift off for years.
Most think that we just do not have the technology for it. The fact is the only piece missing is the material for the cable. It will probably surprise people to find out that solving this may be closer then you may suspect. KONE is currently producing an elevator cable called UltraRope containing CNT that is one seventh the weight of a steel cable and twice the strength. Doing the math that should mean the their design should have 14 times the breaking length of steel. That would make it as good or better than any other material available. UltraRope is likely making use of somewhat dated CNT manufacturing techniques as it has been under development for the past decade. Rice University 2 years ago reported a new method of making CNT thread that should be scalable to mass production. The thread is reportedly has 10 times stronger than the next best CNT thread. The individual CNTs making up the thread are all less than a centimeter in length. Peking University has reported making individual CNT fiber of nearly 20 cm. As this was reported in 2009 and I have not heard much more about it they are not progressing quickly toward mass production of them. That said I think that the only thing in the way is the funding to mature the technology.
So what will an SE GEO do for transportation to Mars? Other that cutting the cost just to get too GEO the elevator cable can be its own counter weight. A payload released from the end of the cable would have enough velocity to reach the orbit of Mars. Once released the trip to Mars could take as little as 2 months. One hitch to that is that the ride up in the SE could take over 2 weeks.
JCO wrote:Exerting yourself in a BALLOON suit is a bad idea but if we do not come up with something much better there will be no point in going to Mars. If exploring Mars will entail people bobbing around like the Stay Puft Marshmallow Man for 6 months we may as well stay home.
Agreed. We're still working on that. I'm not sure we're putting enough money into it, either.
I think it is a safe bet that it is way underfunded at the moment. Even so there are 2 programs developing MCP suits. The budge to bring the technology to maturity will be miniscule compare to what it will take to design a habitat that will keep a crew alive for up to 2 years. Once funds for the big thing are available there will be more than enough money for the smaller projects.
JCO wrote:I take it you have not been on a bike recently. Either that or you are incredibly out of shape. Scuba diving can be very strenuous though diver are able to easily carry over an hours worth of air. With the low gravity a much larger life support carried on the vehicle would not be a great encumbrance. As for falling off, that is one of the reasons I suggested the recumbent trike; it is very hard to fall off of.
I walk or drive or fly wherever I'm going these days. I spent most of my childhood riding around on a bike. At 17, I joined the Navy and spent the next six years walking most places and carrying what little I owned. The Navy was anti-carrying-technology, apart from seabags, buses, and aircraft. Everything that could conceivably be hand carried was. I never owned a motor vehicle or a bike until after I left. I'm not saying you can't walk or bike everywhere, but it requires a bit of exertion and our explorers, unfortunately, don't have unlimited oxygen or food supplies.
This is a much bigger discussion that I cannot claim any real expertise in. What I believe is that we will need to grow food on any mission to Mars. If that is the case recent studies have suggested that there will be a surplus of oxygen produced. I think for the power level of most transportation on Mars humans will be more efficient than any motorized solution. One of the big factors in this is the energy density of humans. Think of the size of battery you would need to carry your Navy gear all day and compare it to the size of the 3 squares you got.
There's no traffic on Mars, yet, so you don't have to concern yourself by getting flattened by some clown talking on the cell phone in a SUV while you're riding your bike. That's a plus.
JCO wrote:The ones who question how effectiveness of are recumbent trike know nothing about the current state of the human powered vehicles in the CONSUMER market. http://www.terratrike.com/ This design could be easily modified for rougher terrain and in 1/6th gravity and almost no air resistance 50 or more miles a day is quite reasonable.
I'm not opposed to the idea of human powered travel, even on another planet, but how do we test all of this? Has anyone used one of these advanced consumer recumbent trikes when it's -100 outside? Whether the vehicle weighs 38% of what it does on Earth or not is of little consequence if you load it down with enough supplies. Have you figured out how are our explorers going to eat, take a dump, or replenish the oxygen for their suits (shouldn't be too hard)? How much would a pressurized HPV weigh? Could you use the HPV as shielding against SPE's?
The best way to test it is build it first for the Moon. If we can make one that works on the Moon we will be able to make one for Mars. My example was not a suggestion for the exact design of a vehicle for Mars but an example of the maturity of HPV technology. It will not be rocket science to adapt known technology for the martian environment. The ideal that the HPV may be too light to work efficiently on Mars is an interesting on. A good size CO2 scrubber and O2 tanks might be useful in providing enough mass for the HPV to be easily controllable. It would be very possible to build the suits to accommodate biological needs for an entire day but I do not think it very practical. This would suggest that any outside activity would be limited to about 4 hour periods. This would be the same no matter what mode of transport was used.
Reconsidering a pressurized cabin for a HPV I think it is possible but the airlock for it would likely make it impractical. You may be able to make one using the airlock suits being developed but that would be a more advanced design then you wanted to send with the first explorer.
I do not know a great deal about radiation shielding but I know shells for HPV are not uncommon. I see no reason that one could not be built that would provide some additional shielding. This will likely be important for any transport on Mars. Because of the longer excursions outside the open dune buggy design of the lunar rovers will be much less practical.
BTW: Factual error on my part. For some reason I was recalling martian gravity as 1/6th Earth not 1/3rd. So I was pushing the martian equivalent of only 1/2 a smart car on my trip.
You mean digging outside? I think you'll need help from a microwave blade - otherwise you would be trying to dig in frozen regolith. Maybe sand I suppose could be moved even in frozen conditions.
The ground will be frozen only if there is water in it. As the weather on much of Mars does reach above the melting point of water from time to time the top several meters of regolith will be free of permafrost. Below that level all you will need is a parabolic mirror to heat up the regolith. It will not be a fast process but from experience here on Earth machines do not do any better digging through permafrost. Once the water content of the regolith reaches a certain point it will be harder than concrete.
Exerting yourself in a spacesuit is not a particularly good idea and our space program and the Russian space program has confirmed that.
Riding a bicycle on Earth with no oxygen availability constraints is hard enough. It's also easy enough to fall off and be injured, which is probably not something you want to do on Mars.
A trike on Earth, who is most likely not wearing a space suit, could cover 50 miles a day.
Exerting yourself in a BALLOON suit is a bad idea but if we do not come up with something much better there will be no point in going to Mars. If exploring Mars will entail people bobbing around like the Stay Puft Marshmallow Man for 6 months we may as well stay home.
I take it you have not been on a bike recently. Either that or you are incredibly out of shape. Scuba diving can be very strenuous though diver are able to easily carry over an hours worth of air. With the low gravity a much larger life support carried on the vehicle would not be a great encumbrance. As for falling off, that is one of the reasons I suggested the recumbent trike; it is very hard to fall off of.
The ones who question how effectiveness of are recumbent trike know nothing about the current state of the human powered vehicles in the CONSUMER market. http://www.terratrike.com/ This design could be easily modified for rougher terrain and in 1/6th gravity and almost no air resistance 50 or more miles a day is quite reasonable.
Anyone who thinks that a electric vehicle would be better on rough terrain than a bike has not spent much time on a bike. As a kid would ride my one speed over all kinds of terrain and could carry it over any obstacle I could not ride across. When I road across the country between me, my gear and my bike I was over 250 lbs. The equivalent on Mars would be a vehicle with the mass of 1500 lbs. The Smart Car has only a slightly greater curb weight. Though I was active I was far from 'peak' physical condition when I began a trip of 4,000 miles. The people we send to Mars will likely be in much better shape than I was. A large portion of the world use human powered vehicles for transporting people and goods. People regularly ride over more difficult terrain then any motor vehicle can navigate.
I think a recumbent trike design would be prefered. The suits used on Mars will be much better than current designs but will likely still be be as restrictive as a wet suit. A trike would be much easier and comfortable to operate. A trike could be designed to carry substantial cargo and even passengers. A human powered vehicle does not require much more effort than walking. The driver of the trike could likely travel 50 miles in a day without a great deal of effort.
If mechanical counterpressure suits are used it would likely allow the wearer to be quite active. Your comment does suggest that most of the activities I am suggesting would need to be outside as there is limited space inside the habitat for activity.
I mentioned in the transportation thread that because of the martian gravity a vehicle with a pressurized cabin would likely not be too heavy to be human powered.
I do not think martian industry will be able to produce anything as complex as a Rolex for quite some time. What may be profitable is to license the recycling of the ships used to return other exports. The recycler would then sell the materials to various companies to produce certified 100% martian products. The products would be manufactured from material returned from Mars. The certification might even include materials that were manufactured on Earth to be used in constructing the martian cargo return vessels. This would provide a good deal more variety in the materials available for use in creating the products.
The problem with agricultural products is that they are less likely to be really unique and they tend to be low in value. A good bottle of wine is likely to cost $100 and I do not think that is anywhere near enough to make it worth shipping back to Earth.
Your plans also seemed to depend heavily on support from the academic community. I think you assume universities have a lot more disposable income then the actually do. As well as having limited funds schools are also unlikely to be good repeat customers. Once they have their kg of martian regolith the are likely to never buy another one. The one thing that could change this is proof that life is or was on Mars. If that is found the flood gate will open and funds for research on Mars will be all but unlimited (until life was found on Europe )
I do not think tourist of any kind will be a big factor in the martian economy until the round trip time is cut massively. The best case scenario for travel time with any technology that looks feasible is 2 months one way. I doubt that many people will want a vacation with that type of travel time.
Once space colonization is well established Mars will likely become the supply depot and ship yards for ventures in the asteroid belt and the outer solar system.
My main point is that the only sure source of income that I can think of that will meet the scale and consistency needed for a martian colony are unique luxury goods. The only things we are sure to find on Mars that meet these requirements are minerals and gems. Metals do not qualify because they are not unique.
There is a post in the transportation topics about riding bikes on Mars. For pure transportation purposes a human powered vehicle will likely be able to move at an equal speed and with the same safety as any other power source. It also provides another benefit that could be very valuable to explorers and colonist on Mars, exercise. The prolonged exertion of human powered vehicle could be very effective at combating muscle and bone loss.
That brings me to the point of this post. I think the key to humans health on missions will be identifying tasks where human effort will be as effective or more effective than a machine. The challenge would be to identify ways to efficiently make use of human effort. At the moment I can think of one other task that may fit into this category, digging. Humans may actually prove to be more efficient at digging in the regolith then a machine that could conveniently transported to Mars. Because of the difference in gravity digging on Mars may feel more like shoveling snow and any rocks smaller than a person would be fairly easy to move.
What do other think would be tasks that would make good use of human power?
I think bicycles may not be ideal for transportation on Mars but I can definitely see human powered vehicles dominating the landscape. With the exception of very heavy equipment. I road a bike from Vermont to California so I do know a bit about traveling by bike. It was a lot of fun but it had some hare limitation that 3 or 4 wheeled vehicles do not have. A trike designed for mars could actually have a pressurized compartment and still be fairly easy for the driver to power themselves. A human powered vehicle with the same mass as a motorcycle on Mars would accelerated slowly but once moving would require no more effort than a bike to keep it moving. Using human powered vehicles would also likely be a great help in combatting muscle and bone degeneration as it could be easy to get a good deal of physical activity as a normal part of daily life.
Mars actually does posses a kind of 'unobtainium'. The minerals on Mars are chemically unique from those on Earth. This is interesting to scientist but it will be much more interesting to someone producing any number of luxury goods. It is likely that finding interesting semiprecious stones will not be excessively difficult on Mars. Any such stone that can be identifiable as martian will be worth at least a couple of order of magnitude more valuable. For example high quality of jade is worth about $100 K per kg. Almost identical jade from Mars will likely be worth $10 million per kg. Another benefit of luxury goods is that it tends to have a dependable high demand market. If it is rare and looks pretty it will almost always be in very high demand no matter what the cost is.
I think the best way to think of what Mars will export is to look back to the colonization of the new world. Most of the exports that fueled the colonies were items that could not be gotten from anyplace but the new world. Spain's gold rush was relatively short lived and did not create many long lasting colonies. No commodity that can be found on Earth will likely be worth shipping back to Earth. So what does Mars have that Earth does not, martian geology. Just like the new world the colonies will not be funded by mundane rare commodities but by unique luxury goods. Anything that could be fashioned into jewelry from martian 'rocks' will be worth orders of magnitude more than the identical item of terrestrial origin. Anything that has a unique make up and an appealing appearance will be worth shipping back to Earth. Martian granite and marble will be more valuable than platinum. It will be shipped back to Earth to floor the most exclusive hotels and the most expensive mansions.
I think the biggest danger entailed with using nuclear is the potential of budget cuts. There will be a significant number of people who will appose any program using nuclear propulsion. We will also likely also face international pressure as some other countries will view the program as a possible weapon, especially if it is assembled in orbit. To be honest the chances of anything on this scale getting funding soon are low and nuclear propulsion could cut the chance in half. I think this will continue to be the case until we are able to mine the radioactive materials off Earth.