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#21
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![]() snidely wrote: Could be Delrin or "engineering plastic", which show up in model railroad kits for parts that would be too delicate in styrene. Now that you mention it, it did somewhat resemble Plastruct engineering model plastic. Intermountain seems to have a decent reputation in model railroading, fitting in to the "Lexus" price range compared to Athearn's "Toyota" price range, but not up to the "Daimler" price range of some craftsmen kits (I know, I shifted countries in that analogy). Maybe the boss is a space freak, too, eh? I found the story of where it came from: http://www.imrcmodels.com/iss/issinfo.htm "THE MODEL A project of the scope and character (of the International Space Station) requires that models be available as educational tools for all aspects of the planning, development, and utilization of the prototype. With this in mind and responding to the growing demand, Johnson Engineering of Houston, Texas and InterMountain Railway Company of Longmont, Colorado have cooperated in the development of a 1:144 scale model of ISS. The dimensions of the completed model are 30x22x20". It is injection molded in styrene plastic, and will be mass produced in several versions to meet the varying needs for such a model." They say it's styrene, I don't know if they changed the plastic, or if it's some sort of super styrene. Pat |
#22
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And there's no way that CEV will be cheap even if flown a thousand
times a year, if it flies on top of an expendable. Agreed. That's why you should fly it on the Stick rather than the EELVs. EELVs are fully expendable. Stick is fully reusable. |
#23
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![]() wrote in message ups.com... And there's no way that CEV will be cheap even if flown a thousand times a year, if it flies on top of an expendable. Agreed. That's why you should fly it on the Stick rather than the EELVs. EELVs are fully expendable. Stick is fully reusable. The stick is only planned to be partially resuable. Unfortunately, the part that is planned to be reusable (the SRB) doesn't save you much money over building it as an expendable. Jeff -- Remove icky phrase from email address to get a valid address. |
#24
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On 17 Oct 2005 11:26:57 -0700, in a place far, far away,
" made the phosphor on my monitor glow in such a way as to indicate that: What's lacking are companies that would be willing to do it as expensively as the use of a CEV would require. Then increase the flight rate. No such thing as a manned spacecraft that'll be "cheap" if only flown a few times a year. And there's no way that CEV will be cheap even if flown a thousand times a year, if it flies on top of an expendable. |
#26
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Or, to put it more simply, the supply curve that the CEV system would
have, would be so far up the graph that it never meets the demand curve. -kert |
#27
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In article ,
John Savard wrote: ...What's lacking are companies that would be willing to do it as expensively as the use of a CEV would require. ...are you claiming that there are ways, absent the development of far-future technologies such as a space elevator (or non-Newtonian propulsion!), to send personnel to the moon at prices that would be rational for even a *few* private companies to take advantage of? There's no fundamental reason why not. The only absolutely inescapable cost of doing so is fuel... and fuel is cheap. The fundamental cost of putting mass into orbit with LOX/kerosene is under $1.50/kg. Of course, most of that mass is vehicle; it'll be up around maybe $8/kg for payload. There will be some other operating costs, not large by comparison because rockets are so fuel-intensive. Call it $10/kg to LEO. Handily, the delta-V for TLI, landing, and return is about the same as for reaching LEO. So similar mass ratios apply, and we get a cost of around $1000/kg for payload to the lunar surface and return. That could be reduced significantly with refueling on the lunar surface, and perhaps further with lunar LOX exported to LEO, but I'll disregard those options. Figuring person plus spacesuit plus baggage plus odds and ends at 200kg, a return ticket is $200,000. Which is a lot for an individual and nothing much for a company. The trick is getting the overhead costs down to a small fraction of fuel costs. We are nowhere near achieving that; currently the overhead costs are utterly dominant and fuel costs are insignificant. It would take fully-reusable highly-developed hardware, greatly streamlined operations, and a high flight rate. There's not the slightest chance that NASA could do that. But there is nothing impossible about it. Of course, looking at prices in my local department store... if it weren't for the effects of the balance of payments deficit, perhaps the U.S. could just buy Shenzou rockets from China! Not that helpful, not on this scale. Cheap hardware, but it's still expendable... and it uses quite costly fuels, much more expensive than LOX/kerosene. (By the way, Shenzhou is the spacecraft -- the rockets are Long March.) -- spsystems.net is temporarily off the air; | Henry Spencer mail to henry at zoo.utoronto.ca instead. | |
#28
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Pat Flannery ) wrote:
: Eric Chomko wrote: : "Yes your honor, it was a model project back in grade school that made : quit school and use and sell drugs." : : : There's a South Park episode lurking in there somewhere. : (Cut to image of Kenny impaled on a solar array.) :-D Yes, South Park dares to go where no other cartoon will. SP makes the Simpsons look like Saturday moring cartoons. Eric : Pat |
#29
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Stick is fully reusable.
The stick is only planned to be partially resuable. Planned, yes. However, the simple fact is that the first solid stage is reusable, while the second stage goes to orbit, leaving large propellant tanks and the SSME available. The tanks would make a fine basis for a space station or an upper stage (or a propellant storage facility, hab modules for the lunar surface, raw materials for SPS, you name it); the SSME can be cut off and returned. It's only a lack of even moderate imagination that makes the 2nd stage expendable. |
#30
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Really. As the man said: Don't think inside the box. The box is not
your friend. |
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