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![]() "Paul F. Dietz" wrote in message ... Dr. P. Quackenbush wrote: Your gravel would have to be delivered from low orbit with a velocity accuracy of about 10 ppm in order to hit the SPS unguided. I doubt a simple two stage rocket can achieve that; you're going to need accurate tracking and course correction. It only has to go straight up. GPS makes that easy. The orbital velocity of the SPS does the rest. Basic math. You apparently don't realize that what you just wrote is maximally idiotic. Try again, but engage your brain this time, ok? Paul Nope. 1986. Air Force simulated, Aerojet approved. |
#22
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#23
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Dr. P. Quackenbush wrote:
Nope. 1986. Air Force simulated, Aerojet approved. Look, dumb**** -- the particular trajectory you have proposed doesn't change the fact that the velocity at burnout has to be very accurate, unless you have course correction. Why did you imagine what you wrote was in any way an argument against what I wrote? It was a complete non sequitur. Paul |
#24
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![]() "Paul F. Dietz" wrote in message ... Dr. P. Quackenbush wrote: Nope. 1986. Air Force simulated, Aerojet approved. Look, dumb**** -- the particular trajectory you have proposed doesn't change the fact that the velocity at burnout has to be very accurate, unless you have course correction. Why did you imagine what you wrote was in any way an argument against what I wrote? It was a complete non sequitur. Paul OK, look here you stupid ****ing ****. You said this: Your gravel would have to be delivered from low orbit with a velocity accuracy of about 10 ppm in order to hit the SPS unguided. I doubt a simple two stage rocket can achieve that; you're going to need accurate tracking and course correction. I said this: Nope. 1986. Air Force simulated, Aerojet approved. Your "doubts" are doubtable. Doubtful, even. ****ing meaningless, in fact. Now **** off and get ****ed you ****. |
#25
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![]() "Dr. P. Quackenbush" wrote in message ink.net... Your "doubts" are doubtable. Doubtful, even. ****ing meaningless, in fact. Now **** off and get ****ed you ****. Paul is right. If you don't get your second stage velocity right, your cloud of gravel will miss the solar power satellite. If you don't get your second stage cutoff velocity exactly right, you'll need a final stage to do this. This isn't as easy as it seems. Jeff -- Remove icky phrase from email address to get a valid address. |
#26
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"Dr. P. Quackenbush" wrote:
"Paul F. Dietz" wrote in message ... John Savard wrote: Solar power satellites are dangerous and expensive - only an L5 habitat could make them economically. I'm not convinced. I've seen a conceptual design of a modular multi-gigawatt SPS that would be built with only terrestrial materials, yet would require launching only a few thousand tons into LEO. Nothing would need to be manufactured in orbit. Paul And I could take that thing out with a simple two-stage rocket and a bag of gravel. Welcome to the 21st century. You personally have one? Look, the transformers outside most *any* generating station are vulnerable to various shoulder-fired anti-armor weapons, and not easily or quickly replaced. Dams have certainly been wartime targets. What's your point? Does every source of power have to be totally impervious to attack, too? -- You know what to remove, to reply.... |
#27
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"Dr. P. Quackenbush" wrote:
"Paul F. Dietz" wrote in message ... Dr. P. Quackenbush wrote: And I could take that thing out with a simple two-stage rocket and a bag of gravel. Welcome to the 21st century. Your gravel would have to be delivered from low orbit with a velocity accuracy of about 10 ppm in order to hit the SPS unguided. I doubt a simple two stage rocket can achieve that; you're going to need accurate tracking and course correction. It only has to go straight up. GPS makes that easy. The orbital velocity of the SPS does the rest. Basic math. Fine for LEO, but 'pop-up' all the way to geostationary orbit (which is where most SPS proposals put them) is asking rather more. Nor are they moving as fast. -- You know what to remove, to reply.... |
#28
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Dr. P. Quackenbush wrote:
I said this: Nope. 1986. Air Force simulated, Aerojet approved. I know you said that. So ****ing what, asshole? I gave a *specific technical reason* why the idea was dubious, one you utterly failed to address. You're all hot air and empty head, dumb****. Paul |
#29
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![]() James Nicoll wrote: In article , jonathan wrote: Let me ask you, looking into the future what is our biggest problem facing us? Isn't it our global energy needs? In fifty years or so we need to replace oil with other sources. Coal liquifaction should see us well into the 21st century, assuming the whole world industrializes (centuries if they don't). And assuming global warming turns out not to be a problem. I also hear tell that there's this atomic power stuff from the pulps that looks promising and a certain amound of uranium and thorium in the Earth's crust, to the tune of about 10^30 joules worth or about equal to the energy in 160,000,000,000,000,000,000 barrels of oil. Humans use use about 10^13 watts but most of us are poor: multiply that rate by 20 and there's enough fissionables to last us about 160 million years. If we'd got started using atomic power in the late Jurassic, we'd just be running out now. And how much of that uranium and thorium is recoverable at a reasonable cost? Granite, basalt, etc. are pretty poor "ores", so the cost will be relatively high at best. And we are *not* going to turn the Earth's crust inside out and pulverize it just to get at the Uranium and Thorium. About 4/5th's of that crust also seems to be under water, which might complicate mining a bit. -- http://www.cic.gc.ca/english/immigrate/ http://www.livejournal.com/users/james_nicoll |
#30
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Richard Morris wrote:
Coal liquifaction should see us well into the 21st century, assuming the whole world industrializes (centuries if they don't). And assuming global warming turns out not to be a problem. Add mineral carbonation to sequester CO2, or use the coal to thermochemically produce hydrogen and sequester the CO2 at the processing plant. And how much of that uranium and thorium is recoverable at a reasonable cost? Granite, basalt, etc. are pretty poor "ores", so the cost will be relatively high at best. With breeding, an average unit of granite has 20 times the energy content of the combustion of the same mass of coal, and the cost of extracting the uranium & thorium from that rock would be a small fraction of the value of the energy produced. But before we did that, we'd mine the oceans for uranium. Uranium can be extracted from seawater (containing about 4 billion tons of U, a at 3 ppb) for less than $1000/lb, and which (with breeders) would contribute negligibly to the cost of energy. It's even possible that the cost could be brought low enough to make this source useable in advanced burner reactors. Paul |
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