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Thermoacoustic refrigeration is certainly less efficient, though perhaps "energy hungry" is a better description than "power hungry".
The refrigerator has to run longer if thermoacoustic, but can be powered by other sources than electricity. The gas liquifier in the article, for example, is thermally powered. Sound energy is required, not electric.
Thermally powered... hmm... I wonder if that would make a useful reactor cooling system?
Well, yeah, but you don't want any of that catastrophic failure stuff.
Why use a design where that's a possibility?
Small RTG's have proven highly reliable over years (even decades) of use, but have fairly low power output for their weight. Gas cooled and liquid cooled nuclear reactors can have very high power outputs, but are relatively unreliable on timescales of more than a few months.
Small RTG's can be strung together like batteries to yield higher outputs. The additional weight required to assemble a radiatively cooled (ultimately air cooled on the Martian surface) nuclear pile of this type may be well made up for in the increased reliability over a more compact, actively cooled reactor. Such a pile would not be subject to risk of meltdown, and need not be too much heavier than alternatives that require active cooling.
It's not nuclear power that bothers me. It's having to run your nuclear power supply so hot that you can't go near it to fix it and it melts if something goes wrong. If my powerplant breaks, I want it to just break, not send me running for my life.
I also have a question: What are the prospects for in-situ construction of a nuclear pile on Mars? What are the expected chances for finding useable radioactives on Mars?
After all the beating this idea took today, I'm not sure if I still need to say that I went back over my calculations and found out that I was off by a factor of two _before_ accounting for efficiency...
So I won't.
The sabatier reactor makes a lot of power, but cannot provide sufficient power for the needed production of oxidizer.
(Curses, foiled again!) :bars3:
And how long do you think that propane/oxygen will last compared to an RTG?
*shrug* About as long as a solar powered rover, I guess, only with more available power.
The Sabatier reaction, used for on site propellant production in the Mars Direct plan, releases a great deal of usable energy. Even accounting for the energy use required to keep the process going continuously, a properly designed propellant plant based around a Sabatier reactor could produce enough power to run both itself and the ERV during the in-situ propellant production phase of a mars mission.
That estimate does not require energy input from a full nuclear reactor (5kW, lithium cooled, etc.). A set of RTG?s would still be required to start the Sabatier reactor and to maintain the ERV indefinitely after the Sabatier reactor shut down. However, the mass of the RTG?s needed would be an order of magnitude less than a full nuclear reactor. Additional hydrogen feedstock would be required, but not so much that it would outweigh a one to five ton nuclear reactor. RTG?s have a better success record in space applications than full nuclear reactors and last longer. (For comparison, the maximum lifetime of the longest operating RTG on a satellite ? the one on the Pioneer X probe ? hasn?t been determined after thirty years. The longest lasting full nuclear reactor on a satellite didn?t make it to six months, with the average being closer to one month.) Current RTG technology is already adequate for on site propellant production.
In short, using the Sabatier reactor for power, employing the hydrogen fuel already along for the ride, can eliminate the need for a full nuclear reactor in an ERV.
Why don't we forget about those meager little RTG's and solar panels and send a rover that runs on propane/oxygen?
[...] can this device separate the various Martian gases by fractional cooling? [...]
Actually, thermoacoustics offers another technique besides fractionation by evaporation & condensation: thermoacoustic mixture separation (also being investigated by the folks at Los Alamos):
[http://www.eurekalert.org/features/doe/ … 092402.php]http://www.eurekalert.org/features/doe/ … 092402.php
Note that no physical state changes (or the energy needed for them) are required using this technique. Thermoacoustic separation is a new transport phenomenon (like diffusion or osmosis), discovered in 1998. It can be used for fractionation by producing a concentration difference between two ends of a tube containing a gas mixture. Given a long enough tube and a loud enough sound source, this difference in concentration can approach 100%. It requires no moving parts and is very forgiving in terms of temperature and pressure. The degree of temperature control necessary for fractional distillation in the Martian environment would not be necessary.
Thermoacoustic heat engines are quite versatile. It is even possible to set up a cycle in which they can act as continuous operation compressors, lacking any moving parts more complex than a backflow valve.
Long tube lengths for thermoacoustic separation and thermoacoustic heat engines don't take up excessive space, because the tubes can be coiled like the tubing of a tuba or french horn. The tubing can be made of plastic instead of the metal used by these researchers, which saves mass.
This looks like a very versatile technique.
One difficulty I've had with the Mars Direct scheme is the fact that, in the fuel production stage, no one has ever provided a satisfactory answer for how the carbon dioxide reactant will be separated from the atmospheric intake. Nor, apparently, has anyone taken the initial fuel production experiment to its logical conclusion and actually liquified the fuel gas generated by Dr. Zubrin's original Sabatier reactor experiment.
These folks at Los Alamos have provided us with two related technologies that can deal with both of those shortcomings.
CME
Hello all.
Check out this link:
[http://www.lanl.gov/projects/thermoacou … Wollan.pdf]http://www.lanl.gov/projects/thermoacou … Wollan.pdf
as well as other thermoacoustic devices describes at the Los Almos National Laboratory website:
[http://www.lanl.gov][http://www.lanl.gov]www.lanl.gov
They?ve built a device which can reduce gases to cryogenic liquids using no moving parts, without any inherent requirement for pressurization. It uses a heat source to power a sound source, but an electric transducer would serve for a smaller unit. Either method could be adapted to Martian conditions.
Because there are no moving parts, the mechanism required for gas extraction is much simpler than methods requiring compressors, has significantly higher reliability, and requires significantly less power input despite needing more energy over time.
I suspect that the possible power savings are sufficiently high that such a system could extract gases from the Martian atmosphere without need for a nuclear power source.
Hello GCNRevenger.
I should clarify.
I am not fundamentally opposed to all possible instances of any use of hydrogen fuel, thermal rocket propulsion, or any combination of the two. You can, if you're willing to put in enough power, heat hydrogen to temperatures in excess of 700K -- the point at which its performance in a rocket engine becomes superior to any chemical propellant. Mechanically, one can make such a propulsion system operate without a meltdown. That's not my point.
I've got no problem with nuclear power, either. As long as it doesn't leak or disintegrate, a well shielded nuclear reactor is just one more heat source. Most of what I've said can be applied to resistojets, heat beds, or any other type of thermal rocket. That's not my point either.
My point is that there are better alternatives.
My principle difficulty with hydrogen as a propellant is the amount of power you have to put into it to make it work as a superior propellant, when there are other propellants that will yield similar performance at a fraction of the heat flow.
Two excellent examples are methane and ammonia. Both have much higher molecular weights than hydrogen in their stable, room-temperature forms. Fortunately, thermal rocket engines don't run at room temperature. Methane and ammonia have relatively low specific heats -- closer to that of water than hydrogen -- and break down into much lighter molecules with relatively low molecular weights -- closer to that of hydrogen than water -- at temperatures in excess of 1300K. And methane and ammonia require less than a third and less than a fifth, respectively, of the energy hydrogen requires to get to that temperature. That means that if you were really interested in pouring in enough power to make a methane (or ammonia) thermal rocket's exhaust velocity comparable to that of a hydrogen thermal rocket, you could do it and still have some power left over. You could produce higher thrusts using methane or ammonia as your propellant, at similar exhaust velocities, with a greater chance that your engine's heat exchanger would still be in one piece at the end of the day.
Thanks for your time.
CME
Hello all.
I must contradict a misconception:
Hydrogen is not always the fuel that gives the most bang for the buck. For a thermal rocket propulsions system (like NERVA or a resistojet), in which the propellant is heated by the transfer of thermal power through heat exchanger, hydrogen can be one of the least desirable propellants to use.
Hydrogen has the highest specific heat of any known substance. This means that it can absorb considerable heat energy with only a small change in temperature. While it is true that hydrogen flows through a nozzle at a given temperature faster than any other gas at that temperature, getting the hydrogen to that temperature is problematic.
For example, a conventional chemical rocket engine burning hydrogen and oxygen propellant releases water as its exhaust. It can attain an operating temperature of about 4700K using the energy of that chemical reaction. (Any hotter and the water breaks back down into hydrogen and oxygen, taking energy away from the reaction.) At this temperature, it can attain an exhaust velocity of about 4.5 km/s. A thermal rocket having hydrogen exhaust only needs an operating temperature of 700K to reach an exhaust velocity of 4.5 km/s (the same as the H2/O2 rocket). However, reaching this 700K for any given thrust requires almost as much thermal power as burning the same amount of hydrogen and oxygen. In a chemical rocket engine, all this heat comes directly from the chemical reaction, but in a thermal rocket engine it has to come from contact with a heat exchanger (such as a nuclear reactor core). Thermal energy doesn't flow against an increase in temperature, which means that the heat exchanger has to be hotter than the fuel. And heat exchangers have specific heat, too -- likely much lower than that of hydrogen. So, if the hydrogen flow gets shut off without shutting off the heat source, the heat flow from the heat exchanger stops, causing heat to build up in the heat exchanger at the same rate it was being transferred to the propellant. That equates to applying nearly the same thermal power as you get from an oxy-hydrogen torch, over every part of the heat exchanger's surface simultaneously.
Under that circumstance, meltdown could take place in as little as a few seconds. Modern nuclear reactor controls are quite good, and could probably prevent a full meltdown even under these conditions in a properly constructed nuclear thermal rocket. But there would be extensive cracking and other thermal damage by the time the control rods got inserted from one end of the reactor to the other, which could result in release of nuclear material.
There are design features that could be incorporated into a thermal rocket to address this safety problem. However, only two of them do not drastically increase the mass of the thermal rocket engine:
1) Do not use hydrogen as a propellant (or anything else with an obscene specific heat),
and/or
2) Do not use nuclear thermal power as a heat source.
You may chose one, the other, or both. Either is effective.
Contrary to some opinions, neither of these is a show-stopper for thermal rocket propulsion. There are other propellants besides hydrogen, and there are other heat sources besides nuclear power.
Thanks for your time.
CME
Hello CC.
There are a lot of plastics that will be just as difficult to work with as you say. However, polyethylene and polypropylene are not among them.
Neither of these plastics evaporate readily in vacuum, so they can be worked with in the open. Both have relatively low melting points -- around 100C. Rather than pressing them, they can be pooled, drawn or blown like glass.
Special shapes with exact tolerances will require heavy molds, though. And some sort of press will be needed to work the plastic, but to form melted liquid, not solid blocks of plastic.
Polyethylene withstands cold very well. It's brittleness temperature (the temperature at which its strength is reduced by half) is -90C. Polyethylene is also resistant to sunlight and very strong. (High density versions compare favorably to aluminum and kevlar.) It's a common material for children's playground equipment.
Polypropylene is not so good in cold, and it eventually breaks down and turns brittle in sunlight. It's brittleness temperature is just 0C. But it has a unique property: It is almost immune to thermal stress. Changes in temperature do not crack or warp it. Polypropylene pipe can be used for liquid nitrogen, and polypropylene dishes are safe in hot dishwashers where polyethylene dishes would be deformed by the heat.
Polyethylene is useful enough to justify taking some with us when we go to Mars. However, if you absolutely must chose between the two, choose polypropylene. It can be made on Mars directly from the propane byproducts of a Sabatier Reactor, using a second catalyst chamber. This eliminates the need to take a block of it with you from Earth.
CME
Maybe only one in two or three men is capable of going through a three year mission in a steel can with a mixed sex crew and not "oppressing the fairer sex," but I don't care if it's only one in a hundred. If you find him, he's the one. And frankly, the womenfolk are not likely to be selected for their frailty in such situations.
Not all men will do it, and not all women will put up with it. If we just pick from those, that still leaves us a huge pool.
CME
Wouldn't the bends (decompression sickness) be a problem with running around naked outside? The pressure is low enough that all gases -- not just nitrogen -- would start to come out of solution in your body.
I for one wouldn't want my kids to see me carried in with an embolism.
CME
Hello Scott. Hello Clark.
I've had some good experiences with the idea of using surveys as decision making tools. I've also had experiences which point out possible pitfalls of this method.
For example, one of the best bosses I ever worked for often employed surveys as a preliminary to a vote for making group decisions. She would send out a formal blank survey to everyone by e-mail (about fifteen people) explaining the situation and asking for everyone to submit written suggestions, then use those suggestions as the basis for a vote.
I got to see some of those surveys at intermediate stages, and I can assure you that this method would never have worked with a simple "one person, one vote" voting scheme, nor do I believe the resulting morass of suggestions would have been at all helpful in a simple bureaucratic review. The trouble is, it was a very rare thing that anyone making suggestions ever limited themselves. No matter what was being done, if people had a choice between their own best interests or efficiency or the common good, self-interest won out nearly every time. The situation was particularly bad if scarce resources were up for distribution. Then it seemed that everyone had to try to swim up and take a bite.
The way my boss avoided information overload was, once all the opinions were in, she would remove suggestions which were inherently unworkable (I never heard back from her about our "Mickey Mouse for Mayor" campaign, for example... a minor disappointment, but I lived), compile a list of all distinct suggestions, and then redistribute that list for the vote. All voters were strictly required to prioritize the list and return it to her as part of their day's assignment. Then it was just a matter of adding points. Whatever the top priorities were, those entries got the most points, and whatever got the most points from everyone combined was considered the most favored solution.
It worked most of the time. I only saw the system break down once, when not one person could agree on a common suggestion out of dozens submitted. Then she fell back on bureaucratic dictatorial authority and made the call for us. With all the bickering required for not two people in fifteen to have a single idea in common, having someone around with the power to put us together and make us look like a group was a godsend.
Clark, I used to work in a marketing department at a hospital. The policy there was that every clerical task had to have an associated list of procedures, in writing, for performing the job. The ideal was that in an emergency you could pull in anyone passing by in the hall to perform clerical duties, freeing some of the nursing staff. (There were rumors circulating that some departments were already doing this, but that's a whole other letter.... ) Perhaps extensive use of detailed procedures and cross training could alleviate some of the danger of groups seizing power by a monopoly on vital skills.
Even so, no one could have replaced the doctors, and they knew it.
Hmm...
CME
Hello Clark.
You wrote:
However, how does the binding arbitration help or even address the situation I have outlined? How does it deal with the centers of power that undermine the basis of the system that makes binding arbitration work?
How can a government enter into "binding arbitration" with a group that wishes to undo the will of the people, yet is also dependant upon these people for exsistence? The system only works if the people can be replaced- how does the system work when the people are not replacable?
And the answer is, ultimately, that I have no answers to any of the questions you ask. These methods alone are not long term solutions. They are acts of desperation.
People also jump out of burning buildings as acts of desperation. How would that address the problem of survival? How would that deal with the fire undermining the structure of the building? How can a person throw themselves from one impending doom to the next?
I have no answer for that, either. I only know that both things happen, and seem quite similar in the amount of forethought given to each.
They happen often enough that we can reasonably expect them, regardless of whether or not they are reasonable.
CME
Hello Clark and Scott.
Clark, "binding arbitration" is generally exactly what occurs in those circumstances. The government puts pressure on both sides to resolve the situation, but their primary interest is in maintaining the services and not in who gets burned.
As for the idea of shooting and torturing people to make them do what you want, world history demonstrates that this often works in the short term. Actually giving the employees what they want -- the long term solution -- yields less immediate results when you've procrastinated so long someone finally turns off the air. By then it's too late to say "tomorrow".
Scott, many bureaucracies hold meetings as well, though the audiences vary in scope. Alas, the passing of policy memoranda throughout the organization is not unknown, there, either.
However, in most bureaucratic heirarchies, policy memos are not policy drafts/proposals/surveys, but "final" ultimatums issued from specific points in the command chain. Do individual people unrelated to the origination of the policy have full authority to suggest changes of the Los Harcones policy drafts, and what criteria are employed to say which suggestions will be implemented? Does Los Harcones have an equivalent to the memo/ultimatum common in bureaucratic heirarchies?
CME
Hello Clark and Scott.
Clark, the best form of central government for dealing with potential strikes and revolts among essential personnel is a dictatorship. For example, here in the United States of America, it is illegal for railroad and electrical power plant employees to strike. If they try it, the government immediately sends in its own negotiators for binding arbitration, and if that doesn't work the companies are authorized to fire and replace everyone. In time of war, military force is authorized. This is very helpful for the preservation of social order. Whenever a strike or revolt is threatened, the threatened companies simply lock out all of their employees and holler "STRIKE!" In comes the government, and the whole messy matter is cleared up in no time, with none of the messy business observed in other industries where the workers' unions decide who goes on strike and who doesn't.
Very clean, very orderly.
Scott, some of the most prevalent problems with bureaucratic heirarchies stem from their inefficiencies in passing information from one point to another within their own structure. Does the Los Horcones community have typical and/or unique methods of passing information within its structure, and are there any problems common with them?
CME
Hello Scott.
If the description on the website is to be believed, it appears I am in error regarding Comunidad de los Horcones. It's government is not bureaucratic, and therefore is unlikely to follow the same information transmission behaviors. (Perhaps they will add my misconception to their list. )
However, I wonder: do they have a Dilbert Problem unique to their own model?
CME
It seems that every time someone a discussion of potential government forms for Martian colonies, two contrasting notes appear: 1) Drastic economic shortages will be a fact of life in the first Mars colonies; and 2) Let's use forms of governance favored by societies enjoying the luxury of economic plenty. Something must be done to remedy or reconcile this.
Regarding Walden Two as a model for government, the social management style Dr. Skinner expounded on has actually seen extensive use in several places in the business community. Bureaucratic decision making structures follow similar mathematical models whether in business or government. The results of those experiments (directed at running businesses with measurable economic outputs rather than societies with less tangible outputs, but still indicative) lead me to believe that a society based strictly on the methods described by B.F. Skinner will quickly come to resemble the well known group from another fictional tale:
Dilbert.
Beware of any kind of government that both requires a lot of interference and refuses to tell you how it's going to work from one day to the next.
Regarding the economics of a Mars base, I think we have a lot to learn from the poorer cultures of the world. For example, the national economy of Argentina has collapsed over the past few years. But Argentinian economics has not. Barter has replaced money-driven economies in many places, and it often not the bare minimum "I want that and I'll give you this for it" that one might expect. Since there's so little money to work with, many of the Argentine people are trading in markets and clubs that apply modern economic principles to the barter system, printing trade tickets, establishing exchange rates, etc. These barter clubs are more like Sam's and Walmart than a barter session with your next-door neighbor. And they are building a sort of currency/money system as well. Barter Club vouchers are currently a harder currency than the Argentine peso and stand to replace it for many purposes if the national economy does not recover.
I suspect that the first Martians will look not to the US Federal Reserve Board but to the Argentine Barter Clubs for their first economic plans.
CME
Look here, Phobos:
http://www.niac.usra.edu/studies/
This is a list of some studies NASA is funding, and Edwards's elevator is among them. The studies are listed alphabetically by principle investigator's name.
Shaun, I merely meant that the pranksters who make these crop circles often sign their work.
I'm able to roughly visualize the methods used to lay out the circles, but I'm having some difficulties understanding the methods some of these artists used to add their initials and even signatures to the work when completed. The precision required to add those letters is very mysterious to me.
CME
I'm afraid it may take a little more than lining your cap with gum wrappers.
http://space.com/busines....31.html
It turns out the reason there have been no research results is that there is no research.
CME :angry:
I am not disturbed in the slightest that results from this have not come in exactly on the appointed hour of the appointed day.
If the expected result is small enough, and the researchers conscientious enough to keep trying, it can take almost that long to go through enough different variations to determine _that you are not observing anything at all._ If the apparatus has to be rebuilt for significant readjustments (a distinct possibility), every time you tweak a variable could delay you for weeks. Even if there is something to see, you might be months working on the optimum method of reproducing that.
The fact that they've asked for an extension to the end of the year does suggest hope. If there was absolutely _nothing_, not even background disturbances to sort out, they should have a null result by now and have everything they need to make an announcement today. However, if drawing out the grant money to the last cent is as important as results, that's a big incentive to extend the experiment to the end of the year, regardless of its result. I consider both scenarios equally likely at this point. It's just a question of what their priorities are.
CME