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#101
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Invid Fan wrote:
The fact the colonies created enough wealth to buy imports means they were profitable. An unprofitable colony would have the parent nation sending needed goods for free or at reduced prices. Only if they buythings at non-subsidised costs. -- Sander +++ Out of cheese error +++ |
#102
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#103
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On Tue, 21 Dec 2004 16:51:25 +0000 (UTC), in a place far, far away,
Sander Vesik made the phosphor on my monitor glow in such a way as to indicate that: There is no "we" about colonization. It is an individual decision and also an individual responsibility. A colonist who can't support himself is not a colonist - he's a welfare recipient living in a very expensive housing project. Care to look up at which point the US was able to produce everything it needed? Whether it's capable of producing it is irrelevant. The point is that it's capable of paying for it. |
#104
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Henry Spencer wrote:
In article , Christopher M. Jones wrote: Ooo, ooo, orrrrr. Maybe, just maybe, Mars! The very same Mars with a massive ice sheet on one pole and permafrost deposits (or at least some form of Hydrogen) just a few meters below most of the surface of the entire planet... Of course, dirty cryogenic permafrost is not the easiest stuff to mine. And we are probably talking about mining, not about scooping it up with a backhoe -- permafrost at those temperatures is hard as rock. Yes, I am well aware of that. It's not an easy problem by any means, but comparing the difficulty of getting the process going vs. the results its a pretty big win at pretty low input cost, especially when compared to other alternatives throughout the Solar System. I was mainly commenting on the difference in ease of processing local materials for propellant production on Mars vs. on Phobos. On Mars there are many very robust, relatively low-cost pathways to propellant manufacture, with permafrost mining and atmospheric processing represinting a route that can produce large quantities of propellant with fairly low initial capital investment using entirely local materials. The comparable processes on Phobos are less easy, less straightfoward, and have a higher entrance barrier (on Mars you can begin very easily by brining along Hydrogen, processing CO2 from the atmosphere and producing LOX/CH4 from mostly, but not entirely, local materials, there is no similar "back door" to in situ resource utilization on Phobos). For example, I don't think many people have fully though out the difficulties of excavating Phobos. If we just so happen to be tremendously lucky then there will be a lot of loose, high-H2O content material on the surface (snow, basically). More likely, it will be embedded in regolith that may or may not be hard packed and may or may not be frozen together in permafrost formations. Even if the ice is packed (together with other materials) only as loosely as, say, your average Earthly dirt, that could still be problematic. The amount of force necessary to excavate is dependant only on material properties, but the amount of force available for excavation is often dependent on weight. And on Phobos there isn't a whole lot of weight to be had, especially in that we won't be able to make the equipment itself very weighty. Very likely excavation equipment on Mars will be fairly awkward contraptions weighed down, or perhaps anchored, in place so that they can apply mechanical forces into the surface. Then you get into issues involving the efficiencies of the propellant production process, which favor the Sabatier process pretty heavily over electrolysis. Anywho, desnarkify my original comments and the message is still perfectly accurate, independent of other factors it will almost certainly be easier to utilize in situ resources on the Martian surface than on Phobos. Then of course, you have to consider exactly what must be known before relying on such resources. You need fairly positive knowledge of what resources exist at a particular site, not just somewhere in the vague vicinity -- not information you can easily get from orbit, you have to actually put a probe with suitable instruments down there. And before relying on extraction and processing, you really need a pilot run to make sure your process will actually work, and won't plug up with dirt or wear down to a wreck or corrode to junk within a week. (Simulation on Earth won't necessarily tell you these things -- there are too many details it can't get exactly right because they aren't known very well.) Interestingly enough, the list of preliminaries you need to attend to is remarkably similar to what you'd have to do to exploit Phobos. Quite, but see above on the difficulties. Again, Mars still has the lead in this regard because of the "back door" approach. We can ease into fullscale 100% in situ resource utilization in stages. The first stage would be a technology demonstration and exploration of atmospheric CO2 usage along with the Sabatier process and Hydrogen that has been brought along. This step can be completely robotic and can be performed at fairly low cost, much less than the cost of the simplest robotic lander mission. This would provide the data needed to tweak the design of an Earth Return Vehicle scaled for a manned mission so that we can be fairly confident of its operation. The first full-scale Earth Return Vehicle fueling via in situ propellant production (though also with brought Hydrogen feed stocks) would provide the proof that the system was workable before astronauts would ever leave Earth and put their lives in the hands of the reliability of the system (or, if it failed, it would provide useful data to improve so that it could be made to work). Then, the first manned Martian mission(s) would be able to do the work necessary to take advantage of local Martian water sources. Locating prime spots, investigating different methods of extraction and processing, etc. Which will then put them in a position to begin propellant production using entirely Martian feedstocks. The comparable process with regard to Phobos is slightly more "front-loaded" and may turn out to take more effort to get into on any level. Though the lesser delta V requirements on Phobos do to a large extent help make up for these deficiencies. The one exception is if all the materials you want are from the Martian *atmosphere*. You probably still want a pilot run, but the resources are actually reasonably proven and in a fairly convenient form. It's unfortunate that there is practically no water vapor in Martian air. Not to mention the substantial advantage that a pilot run on Mars can be done entirely robotically. Plus, Mars also contains carbon dioxide. In fact, the Martian atmosphere is almost entirely Carbon Dioxide. It just so happens that with Hydrogen, Carbon Dioxide, the proper equipment, and a bit of power you can manfucture both Oxygen and Methane. Which just so happen to make really quite nice propellants. At some sacrifice in niceness, you can make CO and LOX from the atmosphere alone. They don't perform as well but they aren't bad. The conversion is very simple; the right sort of solid-electrolyte electrolysis cell does it directly, and is not bothered by moderate impurities. A major bonus is that the electrolysis cell will also run backwards as a fuel cell -- this has been demonstrated -- which lets you tap off a bit of your LOX/CO for keep-alive power at night. In an enormous bit of luck all of this stuff on Mars just so happens to be in exactly the same place, Mars, that a Martian exploration mission would visit, namely Mars. Yes, that is the place that *a* Martian exploration mission would visit. One. Program cancelled after first expedition returns. (Maybe the second if you're lucky.) No question, if you're convinced that the whole thing is going to die after one or two missions, then getting to the Martian surface is top priority. However, a *campaign* of exploration would naturally want to go to Phobos and Deimos *as well*, and would be willing to adjust the order of events if this turned out to have practical advantages. I do not assume a single mission or a campaign but really a process of exploration and colonization. I will respond to your points (and others' points) here later in an omnibus response analyzing the advantages and disadvantages of Mars vs. Phobos as an early target for manned exploration taking into consideration different exploration goals. |
#105
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Henry Spencer wrote:
I wrote: Even the very thin atmosphere at orbital altitudes can circularize... Unfortunately, once it's achieved circularization, it then starts quite briskly lowering the orbit... Addendum, something I forgot: the *hard* part is not circularization, but initial capture into an orbit with a low perigee. Purely gravitational capture doesn't generally get you down that low. Capture by drag very quickly circularizes the orbit and then drops it into the planet, unless the atmosphere somehow vanishes almost overnight. [snip interesting stuff] There is also the additional bit, which you pointed out, I think, that Phobos and Deimos are most like outer belt asteroids. Taken together the odd circumstance lead to some interesting likelihoods, in my opinion. We already know that the bodies in the Solar System are not today where they were when the Solar System formed. I think we can conclude that Mars almost certainly had a very large number of encounters with asteroid bodies throughout its history. Also, we can likely conclude that it had a large number of encounters with outer belt type asteroids. Although these are borderline speculative conclusions without additional corroborating information. As for circularization, what about ordinary tidal interations? It seems increasingly likely that Mars had a more substantial atmosphere (which also contributes to tidal forces) and likely a substantial covering of water for geologically significant periods of time. I wonder if these forces along with the occasional light touch of Mars' upper atmosphere might have done the trick. I imagine that the combination of a Martian atmosphere in decline and the regular Solar cycle could have helped circularize at least Phobos' orbit without causing it to crash. I'd be interested to see what sorts of dynamics studies have been done on this problem and what sorts of things have been pretty definitely ruled out and which have not. |
#106
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Paul F. Dietz wrote:
Another thought: if you have a moon in some possibly eccentric orbit, and it's shattered into many pieces by an impact, those pieces should (through evolution of their orbital elements and collisions between the fragments) reaccrete into a body on a much more circular orbit. Perhaps this happened to Phobos and Deimos, possibly more than once. I think we have been learning recently (from the origins of Earth's moon and especially from studies of the Saturnian system, for example) that cataclysm is very much an operating principle of the Solar System, and very much more prevalent than we had previously thought. We know now, for example, that the Saturn ring and shepherd moon system is rife with incredibly dynamic and cataclismic processes. |
#107
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Sander Vesik wrote:
There is no "we" about colonization. It is an individual decision and also an individual responsibility. A colonist who can't support himself is not a colonist - he's a welfare recipient living in a very expensive housing project. Care to look up at which point the US was able to produce everything it needed? Sander, you're confusing being able to support yourself with being able to produce everything one needs. Presumably, you can support yourself but (also presumably) you cannot produce all that you need. Do you appreciate the difference? Jim Davis |
#108
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Christopher M. Jones wrote:
The comparable processes on Phobos are less easy, less straightfoward, and have a higher entrance barrier (on Mars you can begin very easily by brining along Hydrogen, processing CO2 from the atmosphere and producing LOX/CH4 from mostly, but not entirely, local materials, there is no similar "back door" to in situ resource utilization on Phobos). For example, I don't think many people have fully though out the difficulties of excavating Phobos. If we just so happen to be tremendously lucky then there will be a lot of loose, high-H2O content material on the surface (snow, basically). Unless I'm mistaken, you can't get snow in the earthly sense on Mars. Not even if you had a source where it might come from (and there isn't). -- Sander +++ Out of cheese error +++ |
#109
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Henry Spencer wrote:
wrote: Even the very thin atmosphere at orbital altitudes can circularize any orbit given enough time. The much higher drag at the perihelian lowers the aphelion... Unfortunately, once it's achieved circularization, it then starts quite briskly lowering the orbit. Another cause of circularization is tidal drag. For this to work in a reasonable amount of time on such small moons, it would probably require them to dissipate a lot more tidal energy than a solid rock would. But perhaps not more than a rubble pile would. -- Keith F. Lynch - http://keithlynch.net/ Please see http://keithlynch.net/email.html before emailing me. |
#110
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Sander Vesik wrote:
Christopher M. Jones wrote: If we just so happen to be tremendously lucky then there will be a lot of loose, high-H2O content material on the surface (snow, basically). Unless I'm mistaken, you can't get snow in the earthly sense on Mars. Not even if you had a source where it might come from (and there isn't). If you couldn't tell, I was noting that the probability of snow *density* water-ice deposits on *Phobos* was rather low (though the same is true on Mars). Snow is definitely out of the question. But impacts of icy bodies might create similar density water ice deposits, though there's little reason to assume that later non-ice impacts would not thoroughly mix the ice with regolith. And, worse yet, pack it. |
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