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Maglev launch, Peak Oil, Iwreck & mo' revisited
TIRED ARGUEMENTS I keep hearing the same themes over and over such as "we can't launch from sea level because of Earth's dense atmosphere" (or "lower taxes brings greater economic growth and prosperity so government revenues should be infinite at a tax rate of zero for that matter") . As of this posting "we"'ve already sank $U$356.5 billion into a failed Mideast experiment that should be written off as a lost. The anti-business, pro-speculation class, pro-monopoly Bureaupublican Reich wingers (at least they know what they're for) obviously don't understand economics. http://nationalpriorities.org/index....per&Itemid=182 Or maybe Lawrence Kudlow wants America's supply of snow white to be cut off before Three-Piece Suit Larry falls off the wagon again? WHAT WE CAN DO - ALTERNATIVES TO LEO -- SYSTEMS Enough of the "bad attitudes" (what we can't do); How about what we can do? A search for "evacuated tube" returned no results. How about a system such as the following: http://www.google.com/search?hl=en&q...cuated+tube%22 or even Josh Storrs Hall's Space Pier: http://discuss.foresight.org/~josh/t...struction.html WHAT WE CAN DO - ALTERNATIVES TO LEO - SYSTEMS - MOST PRACTICAL OPTIONS I think that using an evacuated tube and placing as much of the tube at or near sea level as possible would be cheaper than the pier. I like JP Aerospace's idea too -- if they can make it work. Unfortunately, they aren't even telling us what their propulsion system is. http://www.jpaerospace.com/ Another idea, make use of helium to support a portion of the pier or evacuated tube system. Where towers are needed, perhaps they can be used for other purposes (telescopes, communications, solar chimneys, replace weather balloons, etc.) http://www.enviromission.com.au/ http://vortexengine.ca/ If we are going to start on the ground and eject at 70,000 ft. to 100 km (approx. 328,000 ft), why stop at orbital speeds? When the payloads reach the climb phase should it already be at orbital speed? This may be hazardous if power goes out or other failures occur. There seems to be a problem with the StarTram analysis (although the problem may be I skimmed instead of reading which would require engineering expertise a BBA isn't likely to have). If an object comes out of the tube merely at orbital velocity, wouldn't it be necessary to use fuel to get to a decent altitude. Then there is the drag along the way. Perhaps the air in front can be ionized into a plasma (an idea proposed by NASA as part of its own blimp-to-orbit idea) to reduce drag. If anyone can find a link to an online resource on this, it would be appreciated. WHAT WE CAN DO - ALTERNATIVES TO LEO - SYSTEMS -- MATERIALS Josh Hall mentioned diamond, why not more practical materials such as carbon fiber/epoxy or a pressurized shell of PBO fiber? http://www.google.com/search?num=100...rized+shell%22 WHAT WE CAN DO - ALTERNATIVES TO LEO - SYSTEMS - COST ESTIMATES I find the cost estimates a bit difficult to believe. I would think that even the StarTram would end up costing $600 billion. If done by such state-chartered bureaucracies as Helliburton they will probably overcharge us by $6 trillion and waltz off with $5.4 trillion plus the reasonable profit already included in the $600 billion. WHAT WE CAN DO - ALTERNATIVES TO LEO - SYSTEMS - NECESSITY OF CONSTRUCTION With cheap access to space it would be easy to launch the infrastructure to mine NEAs (Near Earth Asteroids), the Moon, other moons (Deimos and Phobos) and crank out solar furnaces which could be attached to space stations with elevators or rotating tethers (to provide an additional boost to objects launched into orbit from the tube/pier). WHAT WE CAN DO - NECESSARY CONPLIMENTARY CHANGES ON EARTH It should be possible to convert to an electric economy. Heat homes with "geothermal" electric and buildings with solar. Perhaps we can put magnetic induction systems in the most heavily traveled sections of roadways, electrify rail lines, and build grade-separated (elevated) PRT (personal rapid transit) systems to dramatically reduce the need for hydrocarbon fuels. As for fuel cells, we'd probably need to go into space anyway to get the platinum needed to build them (not to mention that to get hydrogen from water one must put energy into the water). WHAT WE CAN DO - CONPLIMENTARY LEO TO PLANETS PROPULSION SYSTEMS - USE M2P2 AND GO FOR SPEED WITH HUMAN CARGO Perhaps various ideas can be combined such as using M2P2 (Mini-Magnetospheric Plasma Propulsion) after a tether boost from LEO. The tricky part is slowing quickly upon approach of Deimos or Phobos. It has been suggested that the same tricks ships with sails use to fight the wind can be used. Perhaps in time maglev systems (or tethers) in space can be used to slow approaching vessels. When it comes to human cargo, I think that with these technologies the light and fast approach (a few weeks max) may be best once there are doctors on at least one of Mar's moons -- just put someone in a suit or canister under sedation and send him/her on the journey. WHAT WE CAN DO - CONPLIMENTARY LEO TO PLANETS PROPULSION SYSTEMS - OTHER USES FOR M2P2 Other possible uses for M2P2 I can think of would be to power cyclers and move asteroids (which according to astrophysicist Fred Adams of the University of Michigan and NASA's Gregory Laughlin (and Dr. Benny J. Peiser's who spends most of his time trying to find ways to keep asteroids from Earth and also reviewed their work) in turn could be used to move the Earth). If it can be used to power tethers (would take ingenuity at the very least I suppose) that would be great too. http://www.ess.washington.edu/Space/M2P2/ http://www.space.com/scienceastronom...ve_010207.html THE FOURTH PANET SHOULD NOT BE THE FOCUS I have my "biases". I am inclined to think that the fastest and cheapest way to get to the fourth planet (whose name I dare not speak or write) (and the Moon as well) is by its moons and NEAs, unless perhaps you want another junket that gets little of lasting value accomplished. The fourth planet should not be the focus, except when it comes to marketing. |
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Bill Haught wrote:
[snip[ I feel your pain. Why not just put a capsule on a Delta IV Medium? http://www.orbitersim.com/Forum/Defa...=posts&t=12177 THE FOURTH PANET SHOULD NOT BE THE FOCUS I have my "biases". I am inclined to think that the fastest and cheapest way to get to the fourth planet (whose name I dare not speak or write) (and the Moon as well) is by its moons and NEAs, unless perhaps you want another junket that gets little of lasting value accomplished. The fourth planet should not be the focus, except when it comes to marketing. The problem with the fourth planet is its sheer size. The fifth planet is much smaller, and it's pretty much the same in terms of composition, water ice covered by a thin layer of dessicated crust. http://cosmic.lifeform.org/?p=166 -- The Tsiolkovsky Group : http://www.lifeform.org My Planetary BLOB : http://cosmic.lifeform.org Get A Free Orbiter Space Flight Simulator : http://orbit.medphys.ucl.ac.uk/orbit.html |
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On Mon, 8 Jan 2007, Bill Haught wrote:
I keep hearing the same themes over and over such as "we can't launch from sea level because of Earth's dense atmosphere" (or "lower taxes brings greater economic growth and prosperity so government revenues should be infinite at a tax rate of zero for that matter") . As of this posting "we"'ve already sank $U$356.5 billion into a failed Mideast experiment that should be written off as a lost. The anti-business, pro-speculation class, pro-monopoly Bureaupublican Reich wingers (at least they know what they're for) obviously don't understand economics. They don't need to. They understand greed, gimme and forkover. It's better the world be destroyed than to allow unrealized profits. |
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The US government needs to change the role of NASA from a projects
oriented agency to a mission oriented agency dedicated to reducing the momentum costs and establishing the technical conditions for commercial space launch using assets currently owned by the government. This would put NASA in the same role in the space age, as NACA had in the early days of the air age. The aerospace community should focus its attention on reduction of momentum costs, just as electronics engineering community has focused its attention on the reduction of feature costs. The US government also needs to establish property rights on celestial bodies and regions of the solar system and give the ability to private individuals and companies to develop resources across the solar system and bring them to market. The US government also needs to give tax credits and preferred tax treatment to aerospace investments. Once these conditions are met, the private sector will respond to these opportunities by creating the necessary technical infrastructure to cash in on the opportunities created there. As momentum costs drop the nature of profitable aerospace activities will change, just as falling costs for computing equipment caused a change in computing activities. As these activities become feasible, the services provides are global in nature - creating a global paradigm. Here is the sequence of events that we have gone through and will go through; 1) High cost small sub-orbital transport resulting in ICBMs. The presence of nuclear tipped ICBMs has changed the nature of warfare and created a global incentive, a global paradigm, that seeks to avoid global thermonuclear war. 2) High cost small orbiting payloads - resulting in automated information-satellites, navigation, sensing, communication - these provide global services, GPS, global communications (TV, telephone, radio) and global sensing (weather, intelligence, environment) - changed the nature of information networks and rise of international business. 3) High cost large cislunar payloads - manned space travel through cislunar space. High quality images of Earth from space gave rise to the concept of the entire Earth as a single place. This gave rise to the environmental movement and the demise of rabid nationalism. Terror wars and similar movements are very much a REACTION to the rising global culture. Immediate opportunities exist in enhancing the capacities of infosats. Improved GPS and improved communications as well as improved sensing provide immediate commercial opportunities. Comsats for example, like Telstar - were point-to-point - later satellites like, Sirius and XM - were one-to-many. Future satellites, will have many-to-many capabilities - like the Iridium system. Ultimately, there will be a wireless broadband capacity using space assets that will generate tens of billions of dollars each year in profit. This communications capacity will be used for a variety of purposes, most importantly going forward, will be tele-robotics. People will be able to work anywhere and live anywhere else - and report to work via broadband wireless activation of humaniform tele-robotic systems. Terrestrial solar power systems are the first way we will tap into off-world resources. Sunlight arrives from deep space onto the surface of Earth. Future opportunities exist in expanding launch infrastructure to support large satellite launches to support solar powersats. Lightweight, low cost, solar panel elements combined with low cost phased array microwave - provide a first generation solar powersat. An unmanned fully reusable multi-staged launcher built around existing engine sets and technology, launched from adequate facilities at sufficiently high launch rates - have the potential to reduce costs to 1% that of the space shuttle. Other types of power transfer involving solar pumped lasers also appear feasible using conjugate optics. Here's how conjugate optics works to transfer power - at all wavelengths, microwave to UV. 1) A weak probe beam is generated at the receiver. 2) This beam traverses the distance between the receiver and power transmitter 3) The probe beam interacts in a nonlinear medium with the power beam to produce a dynamic hologram 4) the hologram causes a portion of the power beam to form a phase conjugated beam to the probe beam 5) The power beam travels back precisely along the same track as the probe beam that illuminates the conjugate optical lens. 6) The power beam arrives precisely at the receiver powering it. Now, if there is an intervening distortion or scattering in this setup - phase changes are produced in the probe beam that are communicated to the optics which cause a change in the conjugate beam so that the returning power beam STILL arrives at the receiver unchanged.well formed. http://en.wikipedia.org/wiki/Nonline...se_conjugation As I mentioned, this system works with any wavelength of 'light' - including microwaves. In the end, a space based powernet will emerge, and provide clean energy worldwide.on demand. Beyond that, this powernet will be expanded beyond Earth to support industrial activities in space. Laser based propulsion systems are being developed. A laser based power delivery system on orbit will form a natural infrastructure supporting global ballistic transport using laser based power delivery. This will include the creation of vehicles sporting 'propulsive skins' that consist of millions of pore sized rocket nozzles controlled by a digital signal processor so as to create a wide range of propulsive effects. http://www.me.berkeley.edu/mrcl/rockets.html http://www.eng.rpi.edu/mane/lightcra...t2fullsize.jpg A laser propelled jet has already been flown farther than Robert Goddard flew the first liquid propelled rocket. http://www.nasa.gov/centers/goddard/...r_goddard.html Once we have laser powersats - augmenting maser powersats - we will have the capacity to bring about a fundamental shift in the way transport takes place on our planet - and beyond. Ballistic transport and orbital transport has the potential to be commonplace when a network of solar pumped lasers combines with low-cost laser powered propulsive skins. Of course, the same technology that deliveres precisely controlled amounts of colored inks in a color inkjet printer can be adapted to provide controlled amounts of propellants in a propulsive skin rocket array. Thus, laser energy can be augmented with conventional rocket fuels to provide a very capable system. Specific impulses starting at 400 sec Isp, with fuel based systems can rise to as high as 2,500 sec Isp with laser based systems, and even to infinity with jet based systems and laser light sails. http://www.jpl.nasa.gov/releases/2000/lasersail.html Powersats operating close to the solar surface, and using large lasers and optics to beam terawatts of laser energy across the solar system - has the potential to develop celestial bodies throughout the solar system industrially. Such systems also support low-cost solar system wide transport. Large optics projecting terawatts or even quadrillions of watts interplanetary distance will be adapted to support early interstellar probes and missions using laser light sails. One use of extreme propulsion using very large quantities of solar pumped laser photons is the movement of asteroidal bodies throughout the solar system. A natural consequence of this capacity it to bring a small population of rich asteroids into orbit around Earth and then populating those asteroids with remotely controlled factories driven by populations of workers living on Earth - to produce large quantities of goods that are then distributed by direct deorbiting to customers on Earth and in cislunar space. As the industrial capacity grows ever more sophisticated systems will grow to include space colony sized pressure vessels which will support off-world production of food and fiber which will be distributed throughout human space - including Earth's surface. Ultimately, the Earth will become a residential park supported by orbiting off-world industrial activity, fed by captive asteroids. This same capability will also be used to protect Earth from asteroidal impact, as well as be used to engineer changes in Earth's orbit to protect the biosphere from changes in the sun's activity. http://www.usatoday.com/news/science...2-15-orbit.htm |
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"William Mook" wrote in message
ups.com... The US government needs to change the role of NASA from a projects oriented agency to a mission oriented agency dedicated to reducing the momentum costs and establishing the technical conditions for commercial space launch using assets currently owned by the government. This would put NASA in the same role in the space age, as NACA had in the early days of the air age. The aerospace community should focus its attention on reduction of momentum costs, just as electronics engineering community has focused its attention on the reduction of feature costs. With real interest rates at practically zero and 1% of the population having perhaps 50% or so of the nations wealth due to Reich wing tax cut and spend, do we need NASA for this? Then too, we don't really have free trade (which is part of the problem). The US government also needs to establish property rights on celestial bodies and regions of the solar system and give the ability to private individuals and companies to develop resources across the solar system and bring them to market. Like they did with a swath of North America? How did the U.S. government get all that land by divine right? "Ask any child what he knows about Shays's rebellion, and he will answer, "Oh, some of the farmers couldn't pay their taxes, and Shays led a rebellion against the court-house at Worcester, so they could burn up the deeds; and when Washington heard of it he sent over an army quick and taught them a good lesson" -- "And what was the result of it?" "The result? Why -- why -- the result was -- Oh yes, I remember -- the result was they saw the need of a strong federal government to collect the taxes and pay the debts." Ask if he knows what was said on the other side of the story, ask if he knows that the men who had given their goods and their health and their strength for the freeing of the country now found themselves cast into prison for debt, sick, disabled, and poor, facing a new tyranny for the old; that their demand was that the land should become the free communal possession of those who wished to work it, not subject to tribute, and the child will answer "No."...." http://mutualist.blogspot.com/2005/0...tim.html#links The US government also needs to give tax credits and preferred tax treatment to aerospace investments. More sensible treatment regarding the third factor of production would be better. http://groups.google.com/group/sci.s... 62adc32d4e7a9 Here is the sequence of events that we have gone through and will go through; Future opportunities exist in expanding launch infrastructure to support large satellite launches to support solar powersats. Lightweight, low cost, solar panel elements combined with low cost phased array microwave - provide a first generation solar powersat. An unmanned fully reusable multi-staged launcher built around existing engine sets and technology, launched from adequate facilities at sufficiently high launch rates - have the potential to reduce costs to 1% that of the space shuttle. I wonder about trying to produce the solar panels here on Earth -- toxic materials and impending water shortage. A laser propelled jet has already been flown farther than Robert Goddard flew the first liquid propelled rocket. http://www.nasa.gov/centers/goddard/...r_goddard.html Another alternative. I think the more aggressive infrastructure project I've suggested earlier in this thread is worth the cost. It would force the issue. Variable launch costs would be so low it would be foolish not to go all out. Once we have laser powersats - augmenting maser powersats - we will have the capacity to bring about a fundamental shift in the way transport takes place on our planet - and beyond. Ballistic transport and orbital transport has the potential to be commonplace when a network of solar pumped lasers combines with low-cost laser powered propulsive skins. Still like solar chimneys if we need more electricity generating capacity first. Or start by using lasers to power space planes during hours when power demands aren't so high. Powersats operating close to the solar surface, and using large lasers and optics to beam terawatts of laser energy across the solar system - has the potential to develop celestial bodies throughout the solar system industrially. Such systems also support low-cost solar system wide transport. Large optics projecting terawatts or even quadrillions of watts interplanetary distance will be adapted to support early interstellar probes and missions using laser light sails. Does have a reliability advantage over M2P2. This may be necessary or more practical when dealing with human cargo. One use of extreme propulsion using very large quantities of solar pumped laser photons is the movement of asteroidal bodies throughout the solar system. A natural consequence of this capacity it to bring a small population of rich asteroids into orbit around Earth and then populating those asteroids with remotely controlled factories driven by populations of workers living on Earth - to produce large quantities of goods that are then distributed by direct deorbiting to customers on Earth and in cislunar space. I thin that for this purpose M2P2 is ideal, except for when the velocity gets rather close to the point where they end up in Earth orbit, at which time we may want to switch to a more controllable system. |
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![]() "kT" wrote in message ... Bill Haught wrote: The fifth planet is much smaller, and it's pretty much the same in terms of composition, water ice covered by a thin layer of dessicated crust. For the clueless I think he means minor planets / planetoids between Mars and Jupiter. Why not Deimos and/or Phobos? Since we can Move the Earth ( http://www.space.com/scienceastronom...ve_010207.html ) how about using a small asteroid to move a bigger one to a more desireable location? The difficulty of course may be finding a combination of various tricks involving orbital mechanics (I mean sling-shots and stuff) and bodies in the right locations to use such schemes. Instead of looking for asteroids in the right orbits perhaps such opportunities can be created? First we should perhaps have missions to find asteroids and minor planets closer to the Sun than Earth, unless suitable ones are known. Suitability (different orbits required, likely water supply problem) to set up camp on may be different from snagging asteroids into Earth or Moon orbits and their Lagrange points. Perhaps we can crash an asteroid into a larger one or a planetoid and quickly mop up the water and put it in a basin, then cover it. Other ideas? If one is really lucky one might (I suppose be able to) put an asteroid in orbit (probably not realistic). The advantage would be that it could be coated to reflect radiation thereby preserving water. |
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