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On Sun, 07 Mar 2004 09:11:49 +0100, in a place far, far away, Robert
Kitzmüller made the phosphor on my monitor glow in such a way as to indicate that: I can also think of a lot of ways how to implement docking in orbit. This does not mean that any of them are easy to implement, or cheap either. However you do it, it involves a huge number of components, which must work together perfectly. Well, they have to work well enough. I'm not sure that's the same as "perfectly." You make it sound much more difficult than it is. BTW: How are you going to do maintenence on the space tug? NASA has a hard time to maintain the shuttles engines, on earth... Shuttle engines are intrinsically hard to maintain, due to their extremely high performance. There's no reason a space tug engine would have to be such a finicky beast. |
#22
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In article ,
Robert =?ISO-8859-1?Q?Kitzm=FCller?= wrote: I can also think of a lot of ways how to implement docking in orbit. This does not mean that any of them are easy to implement, or cheap either. However you do it, it involves a huge number of components, which must work together perfectly. No, just well enough. Apollo's docking system did not work perfectly, but no mission was ever compromised by its foibles. BTW: How are you going to do maintenence on the space tug? NASA has a hard time to maintain the shuttles engines, on earth... Rocket Science Fallacy #101 is the belief that the shuttle engines are typical of rocket engines. They're not. DC-X's RL10s didn't need a hundredth of that amount of maintenance to do a dozen flights and maybe twice that many static tests. How best to do maintenance, when the tug needs it -- which shouldn't be all that often -- depends on the nature of the problem and also on the size of the tug. Typically, the best thing to do would be to swap out the affected module -- you'd build the tug modularized, to make this easy -- for a new one, and take the old one down to be fixed. -- MOST launched 30 June; science observations running | Henry Spencer since Oct; first surprises seen; papers pending. | |
#23
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Robert Kitzmüller wrote in message ...
Christopher M. Jones wrote: I can think of about a gazillion ways that this could be done well. [...] Anywho, the amazing thing about space tugs is that we have all the technology to do them on the shelf right now. [...] I can also think of a lot of ways how to implement docking in orbit. This does not mean that any of them are easy to implement, or cheap either. However you do it, it involves a huge number of components, which must work together perfectly. Sure, but we've already done all the work, all that we need to do is put it into practice. Look, this is not speculation at all, Russia has built plenty of space tugs, it's just never really used them as such. BTW: How are you going to do maintenence on the space tug? NASA has a hard time to maintain the shuttles engines, on earth... This is actually really easy. You make the engines replaceable and/or modular. Even so, since these aren't massive, first stage engines, they should have a long service life. The reboost engines on Mir or ISS are not replaceable, for example, though they have successfully gone through a large number of firings and refuelings. As I said, this is actually pretty straightforward stuff. We could do it now to a limited degree with what's on the shelf, we could do it in the near future well with a little bit more engineering and scaling up of certain components and aspects. |
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Sander Vesik wrote in
: Huh? Since when is the shuttle equiped with a fairly advanced nuclear drive? The shuttle does gross orbital changes by landing and re-launching into a different orbit. An orbit-only workstation/tug that is incapable of landing does not have this option and must make all orbital maneuvers using fuel it either already has or can be economically launched to it from the ground. Given the delta-v requirements for moving between, for instance, the ISS orbit and the orbit of the Hubble, the only practical way an orbital tug could service a large varity of orbits would be to use highly advanced propulsion systems. -- Coridon Henshaw - http://www3.telus.net/csbh - "I have sadly come to the conclusion that the Bush administration will go to any lengths to deny reality." -- Charley Reese |
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On Fri, 05 Mar 2004 01:55:48 GMT, "Greg D. Moore \(Strider\)"
wrote: You can do a lot more with a handheld HP than you could do with the Apollo computers. Actually, you can't. The HP has more compute power but it doesn't have the input capability the Apollo computers did. The Apollo computers used pilot inputs and instrumentation that the HP couldn't handle. Mary -- Mary Shafer Retired aerospace research engineer |
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#28
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(Derek Lyons) writes:
(Christopher M. Jones) wrote: It's not exactly like you or anyone else "tosses" their car away when they leave it in the driveway or in a parking space and go to work or watch a movie or eat dinner or go to sleep. It's still there when they get back. Think of it as a roving space station. Which has nothing to do with the discussion of expendables vs reuseables. I'm currently reading "Spaceflight Revolution" by David Ashford. In the very beginning of the book he recalls his first job interview (as an aerospace engineer). Here is a quote from the book: The conversation went something like this: "How did you come to this interview, my boy?" "I cycled sir". "I see. How much cycling would you do if your bike were scrapped each ride?" "Er, not much sir". "Quite right, my boy. Well, that is how it is with launching satellites. They are carried on converted ballistic missiles that can fly only once. Very expensive..." I'm sure you'll dismiss this as well, but it's interesting to note that this conversation took place in 1960. Isn't it nice to see that things haven't changed much in over 40 years? Jeff -- Remove "no" and "spam" from email address to reply. If it says "This is not spam!", it's surely a lie. |
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"jeff findley" wrote ...
(Derek Lyons) writes: (Christopher M. Jones) wrote: It's not exactly like you or anyone else "tosses" their car away when they leave it in the driveway or in a parking space and go to work or watch a movie or eat dinner or go to sleep. Which has nothing to do with the discussion of expendables vs reuseables. I'm currently reading "Spaceflight Revolution" by David Ashford. In the very beginning of the book he recalls his first job interview (as an aerospace engineer). Here is a quote from the book: The conversation went something like this: "How did you come to this interview, my boy?" "I cycled sir". "I see. How much cycling would you do if your bike were scrapped each ride?" "Er, not much sir". "Quite right, my boy. Well, that is how it is with launching satellites. They are carried on converted ballistic missiles that can fly only once. Very expensive..." I'm sure you'll dismiss this as well, but it's interesting to note that this conversation took place in 1960. Isn't it nice to see that things haven't changed much in over 40 years? You mean people are still trotting out the same old tired analogies? It's all in the numbers. How often are payloads how large need to be launched to orbits of what type/height? Now if you were to tell me that (expendables/reusables)* are _always_ going to be the 'right' solution regardless of the answer to the previous question then I'll laugh in your face. * pick one. |
#30
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jeff findley wrote:
I'm sure you'll dismiss this as well, Yes. Because it's another attempt by you to redefine what you are talking about rather than adress the issues I raise. D. -- Touch-twice life. Eat. Drink. Laugh. |
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