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I think that problems of air quality have been too quickly skimmed over in this discussion, making it sound as though the Martian atmosphere could just be pumped right into the greenhouse on one end and have tasty vegetables come out the other side (although I do like Robert’s idea of using a catalytic converter to treat the air in the greenhouse). In addition to needing the same diligence in balancing the O2:CO2 ratio as is given to the crew’s air supply, the greenhouse is going to need some means of eliminating poisons like carbon monoxide and salt aerosols. There will likely be a slight but continuous flow of these through the greenhouse as they are tracked in by the crew, diffuse in through the plastic envelope, etc. Over time, if not removed, they will build up over several growing seasons, killing off the plants.
That kind of slow buildup is often hard to monitor, since the effects of low level poisoning in plants accumulate over time and are likely to start long before the indicator light on the gas sensor starts blinking.
In addition to mechanical monitors, I seriously recommend that we bring along canaries to monitor the gas levels in Martian greenhouses.
[http://www.ces.ncsu.edu/depts/hort/gree … ress2.html]http://www.ces.ncsu.edu/depts....s2.html
Tomatoes are susceptible to everything. Anything but perfect air quality seems to give them incurable epinasty. It’ll be just awful to try to grow them under the expected conditions on Mars, where almost any failure of the air conditioning system could slash yields and possibly wipe out the whole crop.
They’re perfect canaries.
If a Mars Reference mission profile used a transit habitat that could soak in Mars orbit – without a crew – for the entire duration of the surface stay, it would remove both the necessity of landing the entire hab on the surface after the outbound leg of the journey (using a smaller capsule instead for the landing), and the necessity of lofting an entire new transit habitat up from the Martian surface along with the ERV (just re-use the old one sitting in space, propelled using the ERV upper stage). This would substantially reduce the fuel and staging requirements on the ERV, which could then be an even smaller and simpler vehicle.
There would be four essential mission equipment components: A transit habitat, a surface habitat, a rover, and an Earth return propulsion stage. A descent module from the transit habitat would also be required, but I believe that anything big enough to bring the rover to the surface can be made big enough to bring the crew along inside the rover, reducing the role of the descent module to that of a deorbit stage and heat shield for the rover vehicle. The return stage would require a docking maneuver to mate it with the transit habitat, but could use the same docking port as the rover. This is an extra rendezvous over what would be required for a Mars Direct mission profile, but would easily knock fifty tons off of the return stage’s lift-off weight. The extra mission equipment component - a surface habitat – could be incorporated into either the return stage or a sufficiently large rover, and would not require a separate rendezvous to reach it.
In this scenario, the surface habitat would have to be sent over with the return stage, but would not have to be lifted with it. Likewise, the rover and descent capsule would not have to bring down the entire transit hab with them to reach the surface.
[...] I like TransHab construction, but it as with all pressurized space modules, you can't assemble them "incrimentally" from small launches; its unclear that even the ESA ATV could deliver an unfurnished one, and that would require extensive ISS docking port/node modification.
Then there is still the issue of getting science gear up there, which even if it can fit in suitcase sized chunks, you can't get very many of them up there at a time without more payload capacity (Progress 1-2 times a year, ESA ATV 9mo-1yr), and you can only get a few back a year via Soyuz.
Hmm...
I know that all of this applies to the current ISS and Transhab designs, but it does raise questions.
Could a station or other orbital assembly craft be designed for assembly from small packages in LEO?
Is the three-storey Transhab really the smallest inflatable structure that can be used for human habitation? If not, can a smaller version fit on Zenit booster?
What gear (science and otherwise) can be designed to fit in suitcase-sized chunks? What can't?
What absolutely must arrive already assembled? What can be built on site if you can just get it in the docking port?
In short: How unfurnished is unfurnished?
Holy Cow! It's a spin drive!
I had always thought that spin drives would prove impractical because of conservation of energy concerns. However, if the requisite energy really can be stored by _stable_ nucleon spin pairing in large nuclei, all you have to do is figure out how to tap it once you've put it in.
If this really can be scaled up, this is very cool.
Very cool indeed.
Why does the seawater have to arrive distilled and ready to go? Why not create a set of large inland saltwater reservoirs to serve as evaporating ponds? The only difficulty would lie in dealing with the excess salt, but if continuous flow could be arranged over a wide enough area, there’s no need to evaporate the brine down to the point where it couldn’t be pumped back out.
I don't know about you folks, but all those working instruments and other spare parts in one place -- high in the gravity well -- practically make my mouth water.
We should cannibalize the thing.
[http://www.newmars.com/forums/viewtopic.php?t=2078]http://www.newmars.com/cgi-bin....=4;t=82
What about an unmanned stationary probe to drill for water in likely spots?
Drilling to the depths necessary to reach even the highest expected water table on Mars is likely to be a very complicated endeavor. The sandy surface layers expected will require pressurizing a wet bore hole to keep the bore hole from collapsing and trapping the shaft during drilling, which will in turn require bringing something to wet the borehole with. All known drilling methods (including the use of sonic bits) require moving parts and lots of power. The depths expected will require a long shaft, which must be stowed and deployed by an automated probe. Everything coming out of the >100m bore hole (at least a ton of sand, rock fines, and wetting agent for every 100m) must be processed and exhausted by the drilling rig without getting it covered in the stuff. Everything coming out of the bore hole must be analyzed, in at least a cursory fashion, to monitor the drilling progress.
That's probably at least a half-ton of wetting agent, drilling rig and other systems sent to Mars for a single borehole. Taken altogether, none of that is particularly worthwhile for geological prospecting when all one has to do is find a spot where the rocks you want happen to be exposed right at the surface. Mars is an entire planet, and you should be able to find exposed native rock somewhere on it. I also do not regard the search for extraterrestrial life to be sufficient justification for such an undertaking, since the probability of successful detection would be low without striking water, and the sampling methods needed to look for biological activity amid a ton of dessicated rock fines would hinder the drilling. A deep drilling rig would only be worthwhile if, in addition to all the requirements mentioned above, another arbitrary requirement were imposed:
If it finds water, the probe must leave the well in suitable condition for later use, and remain usable for any necessary redrilling or reconditioning.
I believe that the only rational justification for sending a probe capable of drilling deeper than 100m is to scout out water for use in manned exploration. I also believe that it will be an eventual necessity, and should probably even precede the first manned excursion along with the ERV. That way, the first crews on Mars can re-use the drilling rig upon their arrival.
I also think it would look better not to have the first thing we send to our Mars base be the escape pod.
Modern guidance systems are relatively good, given enough fuel for course corrections. Probably good enough to bring one lander down on top of another -- again, given enough fuel. But fuel will be limited, and safety requires that the Hab not come down close enough to the ERV that the ERV would be in its backwash.
That means a separation of at least a few hundred meters between the Hab and ERV upon landing, possibly several kilometers. A substantial surface trek is in store for every member of the crew who wants to go home, regardless of how close the landing is. So, if you've got to cover the ground anyway, why not use a mobile Hab that can make a whole mission segment out of the traverse instead of a simple "final trek"? It could add substantial scope to the mission.
Sample data from the Viking landers back in the 1970's shows that the regolith is chemically reactive. However, just being reactive doesn't mean it's reactive enough to use as a compact fuel source.
Hmm... Perhaps the martian dust could be used in a fuel cell.
Do you have a reference for this? I'd like to read it.
I don't know if they are fossils or not.
As for the methane, at what rate should it be breaking down? A constant rate, or does it have a half-life? That would help determine either a) The rate of replenishment or b) How high the levels must have been in the past to have diminished to their present level.
And no, I don't know that the smaller grains are silica sand. I just used something with a known density for comparison to show how the blueberry density could be estimated.
No.
In fact, I would dearly love to rule it in. However, all I can tell you about is size and approximate relative density.
The size distribution is fairly sharply limited to 5mm. The separation of sizes during saltation should leave the largest particles on top, and there just aren't any larger than 5mm. This suggests that something prevented the growth of hematite blueberries larger than 5mm.
As for the density, the average density of solid hematite is 5.3 g/cc, while the average granular density of silica sand is 2.6 g/cc. Solid hematite grains are twice as dense as solid silica sand grains. So, according to the chart in the article, the smallest grains of solid hematite we should see always on top of a windblown mix of sand and hematite are those whose size is at least 25 times that of the average sand grain. Anything smaller than that would be mixed in evenly with the rest.
I’ve done a little preliminary analysis of some of the soil sample micrographs, looking for a size distribution pattern in the hematite blueberries at Eagle crater. The following mosaic is a good example of some soil micro-photos by the Opportunity rover:
[http://marsrovers.jpl.nasa.gov/gallery/ … 2R1_br.jpg]http://marsrovers.jpl.nasa.gov/gallery...._br.jpg
and this non-micrograph picture of the “Berry Bowl” site was interesting as well:
[http://marsrovers.jpl.nasa.gov/gallery/ … 0R1_br.jpg]http://marsrovers.jpl.nasa.gov/gallery...._br.jpg
It’s been noted that the size distribution of these hematite concretions is not uniform or balanced. There appears at first glance to be a distinct upper and lower limit to their size throughout the Eagle Crater site, with the average size of the globules being closer to the upper limit than the middle of the range.
I think that there is indeed a consistent upper limit to the size of the hematite blueberries, which is on the order of about 3mm but actually varies significantly from sample to sample. The largest blueberries exceed 5mm but those are quite rare. The average is between 2mm and 3mm, despite the fact that the median value is usually closer to 1.5mm.
There is an observable lower limit in several of the samples, but not all. Further, this lower limit is not consistent from sample to sample. I think we can attribute this to two effects: 1) resolution limits and other artifacts in the images which make my sampling technique of sliding a ruler around my screen unable to discern the smallest particles, and 2) size separation of particles due to saltation in the soil samples.
This link is an article discussing size separation of particles in a collection of vibrated (or windblown) granules:
[http://jfi.uchicago.edu/~jaeger/group/p … Nature.pdf]http://jfi.uchicago.edu/~jaeger....ure.pdf
The graph at the beginning of the article is very interesting, as it indicates what would be necessary for large particles (like the hematite blueberries) to separate and rise within the surrounding sand grains as the soil is blown along the surface. This data suggests that the largest blueberries would rise to the top of the windblown sand over time as they were carried along, with the smaller blueberries remaining buried, thus segregating them according to size and concentrating the larger blueberries on top. It also suggests that the blueberries are either significantly heavier than the smaller particles that comprise the rest of the windblown sand or (an intriguing possibility) a dozen times lighter than the surrounding sand.
How large this difference in density is may provide an additional clue to the composition of the little spheres. For example, if they are porous, their distribution will vary slightly from that of solid hematite granules.
Hmm...
It's interesting to note that two other bodies in the solar system, besides Mars, have atmospheric methane concentrations which are out of chemical equilibrium: Earth and Titan. Both have known chemical processes at work which should oxidize or reduce methane quite quickly in geologic terms, yet both have methane. Maybe Mars, Earth and Titan all derive their methane from the same source.
As for the hematite "concretions" found in Eagle crater, I have a hypothesis: I suspect that these globules were not formed by diagenesis _or_ seeded deposition from aqueous solution, but are rather a Martian equivalent of terrestrial stromatalites, and were formed by isolated colonies of iron-oxidizing chemosynthetic bacteria for which hematite was a waste product of their metabolism. Judging from known examples of iron-metabolizing bacteria, methane is also a likely waste productof their metabolism. Similar extremophiles are known to exist on Earth, so why not Mars?
This hypothesis could explain the observed upper limit to the size of the hematite blueberries found on Mars. Deposited concretions need not necessarily have such a limit.
Are there any suggestions for testing such a hypothesis? For example, would a globular stromatolite be porous in comparison to a deposited concretion? What are the distinctive characteristics of a stromatolite, created by living bacteria, compared to a concretion created by inanimate processes?
A Zenit booster only lofts 5 tons to LEO, as opposed to 20 tons for a Delta. How am I supposed to get my spaceship from my backyard to the moon if SeaLaunch puts the Beoing's Delta Division out of Business?
The hab/rover vehicle would have to leave Earth orbit being as big as a house, but it need not reach Mars that way. The extra mass required to make the RV off-road worthy would have to be made up by a smaller final mass. Ultimately, this is a proposal to use an even smaller hab than Mars Direct, but that can be alleviated by relying on the ERV for habitation as well, and by discarding expendable cabin sections.
In the Mars Direct mission profile, crew transit between the Hab and ERV is a necessary portion of the mission. This makes the rovers used by the crew a vital mission component. So, why not combine it with another vital mission component, the crew hab?
A pressurized passenger vehicle similar in size to a modern recreational vehicle (with bigger tires and a broader wheelbase, please! ) could be incorporated into the hab during the outbound trip, then disconnected and driven off the lander as a mobile base. Constructing the hab in in this fashion could allow large portions of the crew cabin to be discarded before the descent to the surface, saving propellant. Using the rover as the primary living space for the entire crew would enable a mission profile with longer surface forays over greater distance. The ERV crew cabin -- not that of the Hab vehicle -- could be used for additional living space, allowing the crew to remain close to the vehicle that they must spend their time setting up to take them home rather than spend time with a vehicle that will ultimately be abandoned.
Power and fuel may be a prohibitive requirement, as the rover vehicle would be hauling around a substantial portion of the mission architecture with it. However, the extra fuel may well prove worthwhile if the mission range could be greatly extended with a matching reduction in the propellant required for landing.
Methane is only a sign of life if it is present in sufficient concentration that it would be out of chemical equilibrium without a source.
Is the methane in Mars' atmosphere really at that high a concentration if it hasn't been detected by now?
I think we should try another tack.
Errorist, I believe your analysis of the mass-energy equation is insufficient to prove your point. Use of units is an adopted convention, and needn’t necessarily reflect reality, but it is the convention in which the mass-energy equation was derived. You can’t get rid of it without voiding a key assumption.
To really argue your point, it might be best to forget E = m c^2 and appeal directly to Mother Nature.
Nuclear fission and fusion, as well as antimatter annihilation, produce energy by the conversion of mass. Electron spin releases energy spontaneously (and without exhaustion – electron spin doesn’t run down) via quantum transitions. However, I think you’ll be more interested in processes that produce mass – or mass effects – from energy.
One example is Inertial Frame Dragging. This is one of the confirming observations of General Relativity, and is the effect used to explain a boost to the orbital precession of Mercury, Mars, and other planets. As it turns out, the sun’s rest mass alone cannot account for its gravitational field. A small portion is due to the energy of its internal reactions (energy creating gravity), and another small portion is due to its angular momentum (angular momentum creating gravity). It’s referred to as frame dragging because the contribution isn’t all in one direction. The energy of reactions contributes a new outward component (swamped by the mass contribution) and the angular momentum contributes a net sideways component. This sideways component of the sun’s gravity nudges the planets’ precession to such an extent that relativistic corrections are necessary for the orbital mechanics computations for a journey to Mars.
The implication is that energy creates gravity, just like mass.
Another example is the momentum of light. The impact of light on an object creates a slight thrust, as well as imparting other energy. Solar sails are supposed to take advantage of this for propulsion.
This implies that energy has momentum, just like mass.
Another example is the Sysiphus effect, seen in the sub-Doppler laser cooling used to cool atoms to absolute zero temperature. The laser light’s photons exchange momentum with the atoms, slowing their motion, but the recoil of photon impacts on the atoms should set a lower limit for how low their temperature can get. The lowest thermal energy attainable for each atom should be related to the energy of the photons slamming into it, but it isn’t. Instead, it looks like the atoms are able to undergo quantum transitions at lower energies than the photon energy, particularly when the reaction rate (the slamming about by photons) exceeds the rate at which the atom can emit photons of its own. This can create a net energy deficit on the scale of a single atom (i.e, lower temperature), even though the atom mainly only emits at its driving frequency (the frequency of the incoming light). The outgoing energy slightly exceeds the incoming energy for each atom, but only when it’s driven faster than it would normally emit. The difference in energy is related to the frequency of interactions between atoms and photons, and not to the total energy involved.
This strongly suggests than energy has quantum uncertainty, just like mass.
And then there’s pair production from gamma rays. Gamma rays of sufficient energy can transform spontaneously into free electrons and positrons. In this case, a massless photon forms two or more massive particles, just by virtue of having sufficient energy to do so. Furthermore, the resulting positrons and electrons are attracted to each other. If they contact another free particle, they can transform right back to a photon, but the transition can also happen spontaneously for a high enough energy electron, just like it can for a high enough energy photon. For an example, check this out:
[http://www.hep.princeton.edu/~mcdonald/ … e1202.html]http://www.hep.princeton.edu/~mcdonald/ … e1202.html
This implies that matter and energy are not just convertible but equivalent and interchangeable – that mass, fundamentally and of its nature, is a form of energy.
Maybe it's not energy after all, but angular momentum...
Or is angular momentum energy instead?
After all they both have the same units...
At any rate, GNC Revenger is right. The algebra of "E = m, therefore M = E", as derived from the mass-energy relation, is flawed because some steps are skipped.
E = m * c^2
E / c^2 = m
let E' = E / c^2
making the actual relation, as described by Errorist:
E' = m, therefore m = E'
which is a true relationship. A transform exists that allows derivation of E from m and vice versa. But that transform is not the actual energy all by itself. Nor, mathematically, is the mass.
The dimensional analysis is very important, too. Units have to be treated as variables during the solution of this formula in order to have any claim to mathematical rigor, and when you're trying to make a point based on math, rigorousness is vital.
For example:
Where this concept gets really cool is when apparently very different things are describable using the same units. Electron spin is often described as "having units of angular momentum", but that's hand waving, because energy and angular momentum both have the same units. In the mathematical sense, angular momentum = energy, with no need for a transform. Angular momentum just happens to be directional, a difference which isn't always relavent to the formula at hand.
Since the units are the same for angular momentum as for energy, the equation E = m c^2 mathematically allows the conversion of angular momentum to mass, too. This is actually observed in nature, too, as relativistic inertial frame dragging.
I feel obligated to point out that the actual equation is:
E = SQRT( ( a * m * c^2 )^2 + ( p * c )^2 ),
where E is energy, m is mass, c is the speed of light, p is momentum, and a is the relativistic correction factor:
a = 1 / SQRT( 1 - (v / c)^2 ),
where v is the velocity. (SQRT() is the square root operator that I can't make HTML give me...) (The whole universe can be thought of as being "off" by the relativistic correction factor. For example, m(v) = a * m is the formula for relativistic mass increase, L(v) = a * L is the formula for relativistic length contraction, E(v) = a * E is a good approximation for the energy formula above, etc.)
E = m * c^2 holds true for the special case of v=0. It's also about right when v is very small.
For a photon, E is not equal to m * c^2. E = p * c for a photon, because m = 0 for a photon in this convention.
That said, the argument still can't be put to rest just by saying "Aha! Photons have no mass! See!", because photons still have momentum. Without mass.
And you guys thought energy without mass was odd...
The elemental composition of the rocks in Opportunity's Eagle crater seems very similar -- almost identical -- to the elemental composition of the infamous ALH 84001 meteorite, which is the meteorite that sparked the "Life discovered on Mars" debate a few years ago. Most of their mineralogical differences can be entirely accounted for by thermal decomposition, such as might be expected in an asteroid impact sufficient to fling ALH 84001 into space from the Martian surface.
I would be willing to bet that all the magnetite found in ALH 84001 was originally hematite that got baked during the original ejection of the meteorite.
I would also be willing to bet that, in addition to the obvious "blueberries", the rocks at Eagle crater also contain microscopic hematite granules (just like those that presumably used to be in ALH 84001). I suspect the whole bunch of rocks formed in similar fashion.
What are the smallest hematite concretions Opportunity can see? What is their size distribution?
I think its time to go back and look more closely at the pictures from Opportunity's "microscope".
Iron-rich minerals deposit all the time on Earth. However, most of that recently deposited iron is not hematite. Most of the hematite ore found on Earth is found in formations dating from well before the cambrian period, so much so that geologists speculate that some event during this time caused a massive deposition of hematite in the world's oceans.
One such speculation is that the first introduction of oxygen by living organisms oxidized the iron in the oceans, depositing it all as rust and iron sulfides in a few million years. Another speculation is that iron-metabolizing microbes (similar to those known today) deposited the iron. However, all that is really known is that most of Earth's hematite formed relatively quickly, deposited in only a few geologic layers.
The satellite survey of the Meridiani area indicates that the hematite layer is very thin.
This means that Mars may have experienced banded iron formation just like Earth.
My guess is that it happened for the same reason.
You're proposing a business venture.
Can you please state your basic financial plan?
RE: Inflatable furniture, I'd have thought throw pillows for sure...
RE: SUV's, they're hardly the most reliable things on the planet (Earth!), but more importantly as a class they're hard to work on. Lots of modern cars are made to be repairable only with specialized equipment. While it's reasonable that the first crews would bring any equipment with them that was necessary to repair their vehicle, it's also reasonable that they would look for vehicles that didn't require much to repair them in the field.
Unfortunately, many other types of vehicle have the same difficulty: You need a garage to fix them. They are designed to exclude repair in the field.