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#21
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#22
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#23
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In article ,
ed kyle wrote: ...At four launches per year, each launch, capable of putting roughly three EELV-Heavy equivalents (75 metric tons) in LEO, would cost roughly $533 million - probably putting it below the recently increased price point per kg of EELV-Heavy... Note that the recent EELV price increases occurred solely and only because of lack of business. The prices will go *down*, not up, if NASA places a bulk order. -- MOST launched 30 June; science observations running | Henry Spencer since Oct; first surprises seen; papers pending. | |
#24
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On 01 Mar 2004 06:27:36 GMT, "Jorge R. Frank"
wrote: Scott Ferrin wrote in : On 01 Mar 2004 05:45:17 GMT, "Jorge R. Frank" wrote: Scott Ferrin wrote in : This week's AW&ST: "Pressed by Congress for cost estimates on Bush's Moon/Mars exploration plan, NASA releases some figures to back up its pretty but imprecise "sand chart" that purports to demonstrate there's no hidden cost "balloon" in the plan (AW&ST Jan. 26, p. 22). According to the Library of Congress' Congressional Research Service, NASA assumes it will cost $64 billion in Fiscal 2003 dollars to land humans on the Moon in 2020. That amount includes $24 billion to build and operate the proposed Crew Exploration Vehicle (CEV) through 2020, plus $40 billion in Fiscal 2011-20 to build and operate a CEV lunar lander. " That's about two-thirds the cost of Apollo, in current dollars. That sounds about right, considering that 1) we've done it before, but 2) everyone who did it the first time is retired or dead. What did *you* find wrong with the picture? Seventeen years. There's two possible responses to this: 1) The actual date for the first lunar return in the plan was a range between 2015-2020, and CRS automatically picked the most pessimistic. It could happen sooner. 2) Even if it is 2020, why hurry? The artificial deadline placed on Apollo helped force some design decisions that ensured that the program would be too expensive to sustain. The idea isn't so much to hurry but to not waste time. Look at any military procurement effort and you'll see that the longer you stretch it out the more costs skyrocket. There isn't really any new technology to develope so why stretch it out when you don't need to? So you can develope an engine that gets two more Isp and costs five times as much? I probably sound like a broken record (for those who remember records LOL) but until they bring launch costs down substantially, nothing significant is going to be affordable. If they were serious about going to the moon and mars the first order of business would be funding the developement of a CHEAP way to get pounds into orbit. As it is, it just looks like more vaporware for political purposes. |
#25
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In article , jeff findley wrote:
"Bruce Sterling Woodcock" writes: One should say that Challenger was an STS accident not a Shuttle accident... in other words, the launch vehicle failed, not the orbital vehicle. True. But there was the mission where one SSME was shut down, and the crew had to inhibit the sensors on the remaining SSME's in order to get into orbit. Arguably that's a launch vehicle failure, but oddly enough in that case, the launch vehicle *is* the orbital vehicle. Hmm. STS-9, pretty undeniably a) not a launch-vehicle failure b) close. -- -Andrew Gray |
#26
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In article , jeff findley wrote:
It's a system integration failure. It would have been o.k. for the ET to shed foam, if it weren't for the shuttle bolted to the side. The problem was studied, but it was assumed that the RCC was "tougher" than the tiles. That's an engineering failure *and* a management failure for not properly solving this system integration issue that surfaced on STS-1. Oh - AIUI, it didn't. The tile loss on STS-1 was due almost entirely, I believe, to SRB-related pressure waves. Falling debris was a problem early, though. -- -Andrew Gray |
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Kent Betts wrote:
"Scott Lowther" The ISS started as a US operation, but the Soviets have come on board in a big way. Yeah. Look how well THAT worked out. I am looking and I see that the Russians are now doing the crew changes and the cargo delivery. Crws that do little except maintain a hunk of junk. Had it been a *real* space station, without the State Department mucking it up with extraneous Russian crap, it'd be much better. Might actually be gettign some science data back. -- Scott Lowther, Engineer Remove the obvious (capitalized) anti-spam gibberish from the reply-to e-mail address |
#28
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On 01 Mar 2004 17:16:37 -0500, jeff findley
wrote: Miss one luanch in a year, and your per launch cost goes up significantly. Miss three launches, and your per luanch cost (for that single launch) is likely to be in the $2 billion range. Miss all four luanches, and your "per launch cost" for the year isn't even defined. By the same token, launch six SDVs (say, four lunar flights, JIMO, and a Pentagon NMD payload) and the costs come down further. You need to average costs over more than a year. Brian |
#29
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On or about Mon, 01 Mar 2004 21:20:29 GMT, Bruce Sterling Woodcock made the sensational claim that:
One should say that Challenger was an STS accident not a Shuttle accident... in other words, the launch vehicle failed, not the orbital vehicle. I don't know why this got drilled into my head so well, but your defination means Challenger *was* a shuttle failure, as I believe NASA refers to the entire stack as the "Shuttle", and the orbiter alone is of course the "Orbiter". Which begs the question why is it called the "Shuttle" Landing Facility and not the "Orbiter" landing facility? -- This is a siggy | To E-mail, do note | Just because something It's properly formatted | who you mean to reply-to | is possible, doesn't No person, none, care | and it will reach me | mean it can happen |
#30
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"LooseChanj" wrote in message om... On or about Mon, 01 Mar 2004 21:20:29 GMT, Bruce Sterling Woodcock made the sensational claim that: One should say that Challenger was an STS accident not a Shuttle accident... in other words, the launch vehicle failed, not the orbital vehicle. I don't know why this got drilled into my head so well, but your defination means Challenger *was* a shuttle failure, as I believe NASA refers to the entire stack as the "Shuttle", and the orbiter alone is of course the "Orbiter". Which begs the question why is it called the "Shuttle" Landing Facility and not the "Orbiter" landing facility? I thought NASA refered to the entire thing as "STS" and the orbiter itself is referred to as the shuttle, the orbiter, etc. This seems obvious when one considers that Atlantis, Endeavour, Discovery are called Shuttles, and they don't change names every time they get new SRBs and an external tank. But, this could be just a primitive form of the old Metaphysics question of replacing every board and nail in a ship. (Or the old joke: "I've had this same axe for 40 years! Replaced the handle three times and the head twice!") Bruce |
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