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Questions regarding my Earth-to-LEO infrastructure biases
What do you think are the current (or at least most near-term) TECHNICALLY
feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. Given developments in maglev technology I would think that this aspect wouldn't be a problem. What about using carbon fiber/epoxy or pressurized PBO fiber shells or other materials instead of diamond for a space pier? What about evacuated tube systems? Would use of high velocity gas ejectors and MHD systems to minimize air infiltration and maintain a vacuum be currently doable technology? If not how far out is it compared to fully reusable rocketry, laser/maser powered space planes or other Earth-to-LEO schemes? If a space plane was maser powered I would think that would necessitate a transfer of cargo at high altitude from one plane to another designed for high altitudes (if even this would work). My "wild" ideas can be found he om or http://groups.google.com/group/sci.s...a8361600615baf -- I am a reasonable conservative who likes to write about politics and culture. Since the media is biased I get all my news from Fox News, Rush Limbaugh and Jay Leno monologues. -- Jon Swift |
#2
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Questions regarding my Earth-to-LEO infrastructure biases
In article ,
"Bill Haught" wrote: What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. OK, what we need then are rockets that launch pretty much daily. That's it -- the high cost (and poor reliability) of rocket launch stems mainly from the fact that it's so rare. Things like space piers, space elevators, etc., that assume a huge launch rate in order to economically justify themselves, often fail to notice that the same huge launch rate would dramatically lower the cost of rocket launch too. But this points out the chicken & egg problem: rocket launches are rare because they're so expensive, and they're expensive because they're so rare. Such problems do eventually crack, but it takes either a lot of patience, or a lot of pushing (or both). Folks like Elon Munsk are doing their best to push from the supply side. The government could push from the demand side, say by setting up an orbital fuel depot and paying for the delivery of large amounts of water. From the commercial demand side, space tourism seems like the most likely bet -- though that will start out suborbital, it will involve a high flight rate, and I'm hopeful that customers will demand longer/higher/faster flights all the way to orbit. Best, - Joe |
#3
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Questions regarding my Earth-to-LEO infrastructure biases
"Bill Haught" wrote in message om... What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. How can you discuss "low cost" LEO launch vehicles and "hand wave" the "economic arguments"? Given developments in maglev technology I would think that this aspect wouldn't be a problem. You underestimate the state of the art in maglev technology. What about using carbon fiber/epoxy or pressurized PBO fiber shells or other materials instead of diamond for a space pier? I personally think this space pier idea is folly. What about evacuated tube systems? Would use of high velocity gas ejectors and MHD systems to minimize air infiltration and maintain a vacuum be currently doable technology? If not how far out is it compared to fully reusable rocketry, laser/maser powered space planes or other Earth-to-LEO schemes? If a space plane was maser powered I would think that would necessitate a transfer of cargo at high altitude from one plane to another designed for high altitudes (if even this would work). My "wild" ideas can be found he om or http://groups.google.com/group/sci.s...a8361600615baf It's pointless to talk about ideas like these since, in the near term, they're simply not going to be pursued in any meaningful way. Instead, look at the companies building real hardware. Look into the economic viability of something like a fully reusable, liquid fueled rocket powered, TSTO. Note that the cost of fuel for a liquid rocket engines is a *very* small part of total launch costs. The US launch industry would be doing very well if it could get the costs down to some small multiple of fuel costs using existing liquid fueled rocket engine technology. Jeff -- "They that can give up essential liberty to obtain a little temporary safety deserve neither liberty nor safety" - B. Franklin, Bartlett's Familiar Quotations (1919) |
#4
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Questions regarding my Earth-to-LEO infrastructure biases
Jeff Findley wrote:
Instead, look at the companies building real hardware. Look into the economic viability of something like a fully reusable, liquid fueled rocket powered, TSTO. Note that the cost of fuel for a liquid rocket engines is a *very* small part of total launch costs. The US launch industry would be doing very well if it could get the costs down to some small multiple of fuel costs using existing liquid fueled rocket engine technology. That's going to be tough. Even capsule development costs are very high. I would go even further and notice that people are lining up for Soyuz rides to the ISS at $20 million dollars a seat. Even if putting a six person capsule on the Delta IV or Atlas V comes in at 20 million a seat, I would run with that. We are already turning away paying passengers. Cost reduction can only come from stage and a half or SSTO, with the engines being reusable and the tankage and residuals remaining in orbit. -- 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 |
#5
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Questions regarding my Earth-to-LEO infrastructure biases
Bill Haught wrote: What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. A rotovator, with a tip speed of about 4km/s, except that makes it cheaper to get to High Earth Orbit than Low Earth Orbit |
#6
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Questions regarding my Earth-to-LEO infrastructure biases
Jeff Findley wrote:
"Bill Haught" wrote in message om... What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. How can you discuss "low cost" LEO launch vehicles and "hand wave" the "economic arguments"? I was thinking largely in terms of the political end of the arguements. Instead, look at the companies building real hardware. Look into the economic viability of something like a fully reusable, liquid fueled rocket powered, TSTO. Note that the cost of fuel for a liquid rocket engines is a *very* small part of total launch costs. The US launch industry would be doing very well if it could get the costs down to some small multiple of fuel costs using existing liquid fueled rocket engine technology. Jeff Which would require designing a rocket that is a vast improvement over the ones we have now which burn up on first use. |
#7
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Questions regarding my Earth-to-LEO infrastructure biases
Joe Strout wrote:
In article , "Bill Haught" wrote: What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. OK, what we need then are rockets that launch pretty much daily. That's it -- the high cost (and poor reliability) of rocket launch stems mainly from the fact that it's so rare. Things like space piers, space elevators, etc., that assume a huge launch rate in order to economically justify themselves, often fail to notice that the same huge launch rate would dramatically lower the cost of rocket launch too. Things with the high fixed costs, lower variable costs (hopefully even with maintenance) would force the launch rate issue. But this points out the chicken & egg problem: rocket launches are rare because they're so expensive, and they're expensive because they're so rare. Such problems do eventually crack, but it takes either a lot of patience, or a lot of pushing (or both). Folks like Elon Munsk are doing their best to push from the supply side. Like the Federal Reserve back in 1932 -- it's like pushing on a string. The government could push from the demand side, say by setting up an orbital fuel depot and paying for the delivery of large amounts of water. If they do something like that they should pay for water obtained in space. From the commercial demand side, space tourism seems like the most likely bet -- though that will start out suborbital, it will involve a high flight rate, and I'm hopeful that customers will demand longer/higher/faster flights all the way to orbit. Best, - Joe There is one way to recover the 50% or so of the wealth the top 1% stole by various means you don't hear about on Reich wing mainscream media. Come take a trip on our suborbital planes, before the Islamic fundies fly a jumbo jet into the building you work at. |
#8
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Questions regarding my Earth-to-LEO infrastructure biases
Alex Terrell wrote: Bill Haught wrote: What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. A rotovator, with a tip speed of about 4km/s, except that makes it cheaper to get to High Earth Orbit than Low Earth Orbit I like this one too. It would take a number of payloads launched into space and in-space assembly work though. The mass of the tether is something like two orders of magnitude of the payload (if using Spectra). As I recall, Tethers Unlimited wanted to use a space plane to reach a tether made out of Spectra 2000. In order to reach their proposed tether a space plane better than an experimental plane (Boeing, I think) was working on would be needed. Perhaps focusing on Earth to LEO or HEO over shooting payloads to other planets would help. If I remember right 4 km/s is half orbital velocity. That would lighten the demands on rocketry making fully reuseable systems more acheivable from what I keep hearing. How about a 100 km tower? Could carbon fiber or something else be used so that payloads can be lifted from a tower? I assume that use of nanotubes/nanoscrolls is a ways away. Here is another idea, following the basic logic (integrate various ideas and systems into a full-scale storm-the-beaches program) of one of my long postings that has received no meaningful comments. A StarTram or space pier-like system that is shorter and operates at say 30gs could be used to send up the tether in sections to be assembled in space. An inflatable ship for the assembly work could be launched too. Capacity is likely to be lower (at least the launch rate). With a high enough launch rate (that is probably difficult to acheive with tethers) one would need a lot of towers anyway (unless of course you use planes or rockets) which is the way you probably want to go (or would at least make you satisfied). |
#9
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Questions regarding my Earth-to-LEO infrastructure biases
Alex Terrell wrote: Bill Haught wrote: What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. A rotovator, with a tip speed of about 4km/s, except that makes it cheaper to get to High Earth Orbit than Low Earth Orbit I like this one too. It would take a number of payloads launched into space and in-space assembly work though. The mass of the tether is something like two orders of magnitude of the payload (if using Spectra). As I recall, Tethers Unlimited wanted to use a space plane to reach a tether made out of Spectra 2000. In order to reach their proposed tether a space plane better than an experimental plane (Boeing, I think) was working on would be needed. Perhaps focusing on Earth to LEO or HEO over shooting payloads to other planets would help. If I remember right 4 km/s is half orbital velocity. That would lighten the demands on rocketry making fully reuseable systems more acheivable from what I keep hearing. How about a 100 km tower? Could carbon fiber or something else be used so that payloads can be lifted from a tower? I assume that use of nanotubes/nanoscrolls is a ways away. Here is another idea, following the basic logic (integrate various ideas and systems into a full-scale storm-the-beaches program) of one of my long postings that has received no meaningful comments. A StarTram or space pier-like system that is shorter and operates at say 30gs could be used to send up the tether in sections to be assembled in space. An inflatable ship for the assembly work could be launched too. Capacity is likely to be lower (at least the launch rate). With a high enough launch rate (that is probably difficult to acheive with tethers) one would need a lot of towers anyway (unless of course you use planes or rockets) which is the way you probably want to go (or would at least make you satisfied). |
#10
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Questions regarding my Earth-to-LEO infrastructure biases
Alex Terrell wrote: Bill Haught wrote: What do you think are the current (or at least most near-term) TECHNICALLY feasible low cost Earth to LEO solutions? Let's hand-wave the politics and economic arguments in this thread. A rotovator, with a tip speed of about 4km/s, except that makes it cheaper to get to High Earth Orbit than Low Earth Orbit I like this one too. It would take a number of payloads launched into space and in-space assembly work though. The mass of the tether is something like two orders of magnitude of the payload (if using Spectra). As I recall, Tethers Unlimited wanted to use a space plane to reach a tether made out of Spectra 2000. In order to reach their proposed tether a space plane better than an experimental plane (Boeing, I think) was working on would be needed. Perhaps focusing on Earth to LEO or HEO over shooting payloads to other planets would help. If I remember right 4 km/s is half orbital velocity. That would lighten the demands on rocketry making fully reuseable systems more acheivable from what I keep hearing. How about a 100 km tower? Could carbon fiber or something else be used so that payloads can be lifted from a tower? I assume that use of nanotubes/nanoscrolls is a ways away. Here is another idea, following the basic logic (integrate various ideas and systems into a full-scale storm-the-beaches program) of one of my long postings that has received no meaningful comments. A StarTram or space pier-like system that is shorter and operates at say 30gs could be used to send up the tether in sections to be assembled in space. An inflatable ship for the assembly work could be launched too. Capacity is likely to be lower (at least the launch rate). With a high enough launch rate (that is probably difficult to acheive with tethers) one would need a lot of towers anyway (unless of course you use planes or rockets) which is the way you probably want to go (or would at least make you satisfied). |
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