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Hmm...
It occurs to me that this would be a useless contrivance on Earth, but NOT on Mars.
Mars has a lower gravity, but an equivalent angular velocity to Earth, making the "pumping" action due to the pole/equator head difference more pronounced. Mars has water in its polar regions which might prove useful in its rather water poor tropics. And while water would prove a problem to pipe all that way without freezing, methane gas would not. (This concept would work for a gas pipeline as well as liquid. Let methane carry the hydrogen and convert it to water on arrival.)
Maybe Percival Lowell had the right idea after all. It just needs some Martians to make it work.
However, this "Pipelines of Mars" discussion might be better suited for the Terraforming forum.
What if you angled the pipeline backward toward the equator opposite of Earths rotation to compensate for the coriolis force?
The water would no longer be pushed sideways into the pipe wall (lower C value in the equation), but the angled pipeline would require a longer length of pipe to reach the equator(bigger L value).
The energy savings of not fighting the Coriolis Force would be cancelled out by having to pipe the water farther.
I hadn't considered that possibility, Spacenut. Surely not?
Does anyone have any anecdotes or information on what the shuttle people's work schedules were between normal flights (and what they are doing now that there are no normal flights)?
The idea of thousands of people in a daily diddle loop is... disturbing. Someone, please dispell this notion.
The formula John Creighton gave for the local acceleration is correct. Just be sure to compensate for latitude when you do the calculation.
(That equation is: a = g - w r sin(latitude) )
Angular momentum, per se, does not figure into the equation, but inertial accelerations do. Centripetal/Centrifugal acceleration is what causes the variation in local acceleration, and consequently the head difference that pumps the water. Coriolis force is a cause of additional drag and energy loss.
With the difference in sea level, there should be a difference in gravitational acceleration, but it will increase toward the equator, and reduces the head difference that's moving the water (making the flow even slower).
Regarding the idea of using this to propel water to space:
You'll notice the interchangeable use of "energy" and "head" when describing the fluid energy equation. By dividing each term in the equation by the specific weight of water, you can convert every term to a distance value, or head (pressure head, elevation head, velocity head, pump head, etc.). This is the height of the column of water corresponding to that much potential energy (or alternately, the depth at which the pressure would correspond). It's also the height to which the water would rise at that point if you just opened a nozzle and let it fly. It will never go higher than that under its own power.
The elevation difference is only a few kilometers, and it won't spurt very high moving at one millimeter per second.
This effect will never allow you to pump anything to orbital heights, because the head doesn't correspond to an orbital height. Any "pipeline to space" idea will need to use something else.
BTW, Errorist, Graeme Skinner is quite correct. Judging from what I've seen of your posts, this sort of simple theoretical model is probably well within your capababilities. You really should try to work out the math for yourself first. That will allow you to defend yourself better against those who try to shoot you down for fun.
The world resists your theories, but remember: Math is Power! :laugh:
Bernoulli's Equation holds true whether you're raging against the establishment or not, but you need to learn it first.
I'd rather stab myself with a spork.
Don't you mean "runcible spoon", Trebuchet? :laugh:
I had a professor once who insisted that if there was a fluid head difference (potential energy gradient) between two ends of a uniform level pipeline, no matter what the continent-spanning length of it might be, a fluid could be induced to flow from one end all the way to the other. He said that all head losses (losses of flow energy) were velocity dependent, so at some point the flow velocity would fall below the point where friction, viscosity and other velocity-dependent losses were strong enough to prevent the flow. Similar flows were already observable in ocean bottom currents which - though it might take thousands of years - trickled from the pole to the equator propelled by nothing more than a slight head difference.
In short, Errorist, his claim was that your claim was theoretically possible, provided you don't care how fast the flow is moving.
Unfortunately, the expected flow velocity is hardly fast enough to keep the water at a stable temperature all the way from the poles. It would heat up to within a few degrees of equatorial temperatures along the way if you ran your line along the surface. You'd need pumps just to get the water to the equator in your lifetime, much less while it still had a chill on it.
It will pump water, but you can forget this as a heat exchange mechanism.
The applicable equation is Bernoulli's Equation adjusted for external work and potential losses, also called the Fluid Energy Equation. It goes like this:
P1 + rho1 * a1 * h1 + alpha * rho1 * v1 ^ 2 + W =
= P2 + rho2 * a2 * h2 + alpha * rho2 * v2 ^ 2 + Q
where
P1 & P2 are the pressures on each end of the pipeline,
rho1 & rho2 are the fluid densities on each end,
a1 & a2 are the local accelerations (gravity + centripetal force) on each end,
h1 & h2 are the elevations on each end,
v1 & v2 are the flow velocities on each end,
W is the total pumping work added to the fluid over the entire pipe,
Q is the total loss in potential energy over the entire pipe,
and
alpha is a constant correction factor for non-uniform flow across the pipe's cross section.
The basic idea is that the energy on one end of the pipe is the same as the energy on the other end of the pipe. This equation can be found in any Fluid Mechanics textbook, as well as equations for computing W and Q.
If you plug appropriate values into this equation, assuming W = 0 and Q = C L v^2 (where L is the pipe length and C is some system-dependent constant describing the energy losses per unit length), you see that v has to be very small before any of the other terms become larger than Q, because L is so freaking huge. And nothing will move until the other terms sum to more than Q. Without a lot of big pumps, you're probably looking at a flow velocity of a few millimeters per second. It might outrace a snail - maybe, with a really big pipe.
The Chief Administrator of NASA makes $158000 per year.
The US Vice President makes $190000 per year.
The LSU Chancellor makes $350000 per year.
The US President makes $400000 per year.
O'Keefe, already an unusually well-paid public servant, stands to become a spectacularly well-paid academic. I'd have taken the chancellorship, too. It makes me rather sorry for the rank and file at NASA, though. Odds are, their pay scales are not as impressive.
It was a high pitched sound and ear piercing if you twisted the end of the conduit towards your ear. It worked with ten foot piece as well as the two foot piece that was left over. In either case you had to blow moderately and not to hard and so it seemed it had to reach a predetermined velocity for it to work.
This will sound odd, but have you tried swinging the lengths of tubing around overhead like a sling? This will give you a relatively simple means of controlling the flow rate through and around each tube.
I don't recall the name of the children's toy, but I do recall that it operated in roughly that fashion and had a fairly wide range of pitch.
PS: Before I ran across this post, I had completely forgotten about this simple, tunable sound transducer. I was looking for something like this recently. Thanks.
If you are repeating your question, then you obviously DON'T understand.
What's wrong with that?
I also wonder about that macro-scale tubing. There used to be a popular child's toy that did the same thing. Why does it yield that pitch, which is a function of the flow velocity rather than a harmonic of the tube length?
What's making that sound? It's a perfectly legitimate - and potentially useful - question.
Regarding sound on the microscopic scale:
Sound does not exist on this scale. Indeed, it isn't even usefull to think of the molecules as being in any particular state, gas, liquid, solid whatever. The relevant laws (such as the gass law, fluid dynamics) do not apply on these scales, as the intermolecular forces completely overwhelm them. The reality of this scale is a group of realtivly small molecules moving surounded by a group of bonded, but still constantly moving/flexing carbon atoms.
Four statements, none of which are necessarily wrong, but none of which necessarily support each other, either. The dots must be connected for this to be a useful argument.
Macro-scale descriptions won't even work on the macro-scale if the assumptions you use don't match the system you're describing. Pre-supposing sound doesn't exist in any model of nanoscale phenomena can tempt one to neglect acoustic potential energy. Assuming there is no ordering to the motion of molecules in any system at that scale can tempt one to neglect mass transport phenomena and a host of other effects. Yet these effects can not only readily exist at the nanoscale but can "swamp" the net effects of other intermolecular interactions. You can set up a system that won't have them, but not by ignoring them.
Errorist might even find them in his corrugated tubing.
I hope O'Keefe gets the chancelorship at LSU.
I don't know if Zubrin would be a good or bad choice for NASA administrator. On the one hand, most of the better NASA administrators have had an agenda, a mandate from their supporters, or both (Faster-Better-Cheaper, straighten the books, put a man on the moon, etc.). NASA needs focus, and needs it badly. Zubrin could supply that.
On the other hand, he's Robert Zubrin! :laugh:
I'm uncertain if a loudmouthed spitfire can develop the effective cat-herding strategies necessary to make it in the upper echelons of NASA. One might do better to look for another candidate, one with the requisite focus but without a history of blanket criticisms, minor insults to former employers, etc. Zubrin's got skill and enthusiasm, and he's a true leader. I admire the man greatly. I'm also happy to see him with his own company, because he'd probably have suffered greatly from submission to the bureaucratic politics of NASA.
NASA needs someone at home in the environment it offers. Zubrin isn't that guy.
Give the administrator's job to the current director of the Kennedy Space Center. Between the hurricanes and the fires, I'm sure they need a vacation right about now. :;):
It's important to separate "Mars Direct, The Design" from "Mars Direct, The Mission Architecture".
The current design won't work, but design may be too strong a word for a collection of sketches and manufacturer's specifications gestimated together into a glorified Powerpoint presentation. Though advanced beyond the vaporware stage, it's an unfinished product, no more able to fly to Mars than a model ship is meant to sail to Hawaii.
However, the design is just a sample of how to use the design approach. The important innovation isn't some sketchy, unfinished mass estimates that don't even provide a means for the crew to avoid appearing naked on international television. (The analysis of Mars Direct only ran so deep. If fuel wasn't accounted for, clothes weren't either.) It's the combination of in situ propellant production, a separate ERV and other approaches that, if used in a properly designed system, could produce the kind of mass savings necessary to make a Mars mission possible for less than a tenth of previous estimates.
Anyone who says that Mars Direct provides no useful inspiration is as crazy as someone who expects to run out and hop in the working model tomorrow.
Sure, let 'em ship food. It's good practice for sending the pharmaceuticals and other manufactured goods later.
Traditionally, it's been the menfolk who rush out to the unknown desert frontier where they have no mates. They then start getting desperate, at which point the womenfolk follow after and take their pick.
I don't know if the sight unseen, mail-order bride scenario would be particularly appealing in the absence of a groom able to pay a bride's way. A family looking for prospective in-laws would do better to look for a productive and/or secure spouse from Earth (male or female), and an available lady would do better to make her own way.
By the time this becomes an issue, I think that recruiters would do as well to devote time to entire families as well as singles. Families with children bring their own singles - you just have to wait longer for them.
I just had a mental image of long lines of smoke-belching tractors, blackening the pristine snow downwind of their exhaust stacks.
Drat! :bars:
Don't tell me one of the one of the world's greatest living adventurers had a point! :bars2: I don't want to hear it!
Whatever happened to ignoring the ramblings of old men! Where is progress for Progress's sake! Hasn't the world's largest expanse of unspoiled land been beyond our grasp long enough! Who cannot see the virtue of showing man's innate power over nature!
I want McMurdo Station to be another Cairns! :realllymad:
*cough!* *wheeze!* Where's my inhaler! *snort!*
I mean, um... Hmmm... Perhaps the environmentalists are merely waiting expectantly?
That electric current oven sounds interesting.
Did you know that - contrary to popular misconception - it isn't microwave resonance that heats food in a microwave but electric current? Most food conducts electricity, so like any conductor it develops electric charge under microwave radiation (just like a metal antenna) and those charges flow. That's also why glass, ceramic and paper containers don't get very hot above the fill line in a microwave - they don't conduct electricity, so they don't heat up.
Imagine just sticking a couple of paddles up against the food, shouting "clear!" and jump-starting your dinner. That would be better than a microwave.
if all the countries around the world cooperated properly then we'd have manned missions flying every week
And when that happens, I'm sure that I will lose all reservations about international cooperation on individual space missions...
Of course, there is hope as pointed out by Spacenut:
Military, government, education and space-industry leaders will gather in Denver today for the Colorado Space Rendezvous, an event aimed at spurring collaboration in the state to pursue important space contracts and projects.
It's important to note that this event is statewide only. It's not national, or international. However, given the apparent gradually decreasing efficiency of progressively large organizations, perhaps a national or international organization would be less desirable.
I'm no statistician, but as I recall, elementary risk assessment can be done any number of ways depending on how you expect your investment to behave.
The "time value of money" method is simple, and useful if you know the investment's behavior over time. Cumulative reliability estimates, and zero-sum matrices can help if you don't know what it's going to do over time but do know how likely it is to fail or how spectacularly it will do so.
If you had a whole bunch of investments of the same type, so that you could watch how they behave as a group, you wouldn't necessarily have to know enough details to predict how each individual investment will perform. You could just use an amortization matrix instead to make predictions using average behaviors.
Discussions of these methods can be found in any business statistics book.
I'm of mixed feelings on this.
When I reach 85 years old, I expect to be left alone to say whatever I want.
On the other hand, Edmund Hillary ought to shut the heck up and let them build the road.
If they built a road to the summit of Mount Everest, I'd hate to see the litter people would leave along the way. Of course, with regular cleanups, Mount Everest might be prettier than it is now. (No more candy wrappers, spent oxygen bottles, dead bodies, etc. left lying around.)
[...]in one test the increase was between 36% - 169%
269% of 0.3 mbars (the amount of CO2 in Terrestrial Air) is only 0.8 mbars. That's still breathable.
The small guys will come of w/ some innovative ideas that the big guys will impliment to reduce launch cost and thus have more money for R&D, profits, etc.
Usually it is the other way around. The big guys come up with the ideas and do most of the research, the little guys try and make cheap knock-offs.
It's not the little companies' fault that patents expire. :;):
Unfortunately for the little guys, the giant corporations hold most of the patents. The little companies generally try and compete by being more efficient. The can not compete on the big projects that require the most R&D and advanced technology, so instead they aim for the segment of the market that is easiest to enter: small low-cost launch vehicles.
Big corporations hold many of the relevant patents, it's true. Small companies have to pay to use them commercially, which drives up prices. Further, many small companies are forced to seek funding from sources by conceding portions of proceeds from their own patent development. However, it's gradually becoming clear that the technology represented by many of those patents is not adequate to the task, so it doesn't ultimately matter who owns them.
The current "small low-cost launchers" are nothing of the kind. They were quite innovative a few decades ago, but I would not recommend the average modern rocket to a start-up company wanting to specialize in launch vehicles.
If you want to start a new company, get a new product.
Question: Is human space exploration a niche market?
[...] improbable that a small private coorporation will be able to generate the resources to support the development of exploration program.
I agree we're reaching the limits of conventional rocketry, but I don't agree with this assertion.
The small guys will come of w/ some innovative ideas that the big guys will impliment to reduce launch cost and thus have more money for R&D, profits, etc.
I can't concur that the "big guys" will necessarily steal ideas from the "small guys". Such a theft would have to occur in the courts as well as the markets. Are there no trade secrets? Are there no patent laws?
By their nature the small guys will not produce the margins necessary to fund the rapid development of a robust launch system.
Nope, rapid development will not be forthcoming from the small business people. Profit margins do affect the rate at which money and man-hours can be poured into a project, and small businesses barely have any in comparison.
But that does not mean that no development will be forthcoming.
This, however, is what many of the Altspace folks are arguing; make a rocket on the cheap and and pull necessary revenue from the big guys. SpaceX and Microcosm are hoping to carve out a niche for institutional/military/medium industry launches and drive up launch frequency. If they can't do that they're sunk.
Although small companies do tend to be more efficient than larger companies, the difference isn't vast enough to give them the edge all by itself. However, given a uniquely innovative, sufficiently legally protected, and truly superior functional solution, a small business could become a big business over time. The big guys were small guys once, too.
If you had a small AltSpace startup, trying to compete directly with an aerospace collosus fifty times your size would be foolhardy. There has to be a barrier between you, some mouse hole to hide in while you grow bigger... Fortunately, such holes exist, in the form of patent monopolies and other legal protections. You can find your company's niche. All you need to get into it is some really good legal advice and the next big idea.
Climbing out again once you're there, that's the subject of a whole other post. :;):
Maybe I can make this simple enough for you Comstar:
You are a dumb person who has his head stuck in a fantesy world of yesteryear and who resists all challenges to your wild statements in an attempt to drum up exclamation point ridden yes-men support.
Ouch, GCNRevenger. Mixing a little bitter venom with our usually refreshing pessimism today?
You did say one thing that rang true, though. IMHO, it's the true cause of the current sorry economic state of affairs in space exploration.
Rocket technology has by and large reached a zenith too, engines have reached the limits of their fuels, materials are reaching their limits, and computer technology does not need to improve any more to fly them.
Rocket technology can take us no farther in our current direction. That's why we've made so little progress since the 1980's. That's why Mars Direct can't work. We are reaching the limits of this technology.
However, the proper response is not to rant about the limits of the old technology and how nobody using the old technology is able to innovate sufficiently to make it work. The proper response is to turn to new technologies that can still innovate and improve. Don't hitch your wagon to a falling star.
The main difference between motors using the Otto cycle, Diesel cycle, and the various turbine types is operating torque, which affects everything else about the motor design.
The efficiency of any heat engine cycle varies according to what pressure you run it at, and pressure determines the minimum torque needed to run a rotary motor using that cycle. Since each cycle works most efficiently at a different range of pressure, each engine type works best in a different range of torques.
For example, a diesel motor needs huge pressures and consequently huge torques, but an Otto motor can work at lower pressure and a turbine motor can operate at near zero pressure. Consequently, you will never see a model airplane using a diesel - those tiny little motors would burst apart before developing enough pressure to run a diesel cycle. But you can run them with a turbine or otto cycle motor. A turbine engine can't quite reach the same overpressure as an Otto cycle engine, so it's range of torques is smaller, but can run at even lower pressures. A turbine engine could even conceivably run on the surface of Mars without extensive vacuum modifications, though you wouldn't get much work out of it.
There is a theoretical smallest optimum size for a turbine engine using pressure differentials alone to drive the engine. Below that, a simple fan turbine can't reach a very high efficiency. However, fluid adhesion can drive a turbine as well, allowing turbines to reach sizes smaller than the smiley at the end of this sentence.
Totally not my field, but I'd think the diff between .38 and .5 is significant, engineering wise...
Wouldn't the booms or cables have to be longer, to get increased g-forces?
The difference is significant, but not so much that it can't be done. The main mass difference comes from maintaining reliability under the greater wear and tear, not from withstanding the greater load. Remember, everything on the ship has to withstand 3G's during launch anyway. However, over three years, 0.3G's can do more damage than 3.0G's applied over three minutes.