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It turns out that one CAIB recommendation is adding schedule
pressure to STS. Florida Today reported at: "http://www.floridatoday.com/columbia/columbiastory2A13038A.htm" that the new launch criteria will limit launching to four periods during 2004: "roughly March 11 to April 6; May 19 to June 28; July 18 to Aug. 26 and about a three-week period between mid-September and mid-October". There are also two three-day periods in November 2004 and January 2005, but if NASA can't get shuttle ready to fly by October (it has already given up on the first one or two 2004 periods), then it probably won't be able to launch until February 2005, according to the report. - Ed Kyle |
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In article ,
ed kyle wrote: It turns out that one CAIB recommendation is adding schedule pressure to STS. Florida Today reported at: "http://www.floridatoday.com/columbia/columbiastory2A13038A.htm" that the new launch criteria will limit launching to four periods during 2004: "roughly March 11 to April 6; May 19 to June 28; July 18 to Aug. 26 and about a three-week period between mid-September and mid-October". There are also two three-day periods in November 2004 and January 2005, but if NASA can't get shuttle ready to fly by October (it has already given up on the first one or two 2004 periods), then it probably won't be able to launch until February 2005, according to the report. Okay, this is probably a really dumb question; but how easy would it be to change the orbit of the ISS to put it in something that is more convenient to reach from the Cape? Forget the politics, etc., just the mechanics? Nick |
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Herb Schaltegger wrote:
[snip] I also thought the ISS Orbital Plane was chosen specifically to benefit the Russians and their higher latitude of launch sites. |
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In article , stmx3 wrote:
Herb Schaltegger wrote: [snip] I also thought the ISS Orbital Plane was chosen specifically to benefit the Russians and their higher latitude of launch sites. Yeah, but the criteria set by the original poster for this thread specified that he wasn't interested in going into the politics, just the math (and science) behind such a change. -Dan |
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Dan Foster wrote:
In article , stmx3 wrote: Herb Schaltegger wrote: [snip] I also thought the ISS Orbital Plane was chosen specifically to benefit the Russians and their higher latitude of launch sites. Yeah, but the criteria set by the original poster for this thread specified that he wasn't interested in going into the politics, just the math (and science) behind such a change. -Dan Ooops. Forgot. |
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In article ,
Dan Foster wrote: I also thought the ISS Orbital Plane was chosen specifically to benefit the Russians and their higher latitude of launch sites. Yeah, but the criteria set by the original poster for this thread specified that he wasn't interested in going into the politics, just the math (and science) behind such a change. Indeed I was just pondering the math. (pondering the feasibility of, for example, someone building a special one-time use second-stage type unit that could be used ... though given how slow an operation it would have to be, perhaps there isn't much technology sitting on the shelf that could burn that slow, for that long .... Another thought though, that is raised though ... what about moving the US launch site .... Are there more northerly launch sites that would have better operating windows? Nick |
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In article ,
Dan Foster wrote: In article , stmx3 wrote: Herb Schaltegger wrote: [snip] I also thought the ISS Orbital Plane was chosen specifically to benefit the Russians and their higher latitude of launch sites. Yeah, but the criteria set by the original poster for this thread specified that he wasn't interested in going into the politics, just the math (and science) behind such a change. -Dan Yeah, what Dan said! Leaving politics aside, moving ISS to the current orbital plane was such a technical mess . . . Since a major chunk of ISS is legacy Space Station Freedom hardware (all the U.S. elements, the ESA Columbus module, NASDA Kibo module, etc), it was all baselined for launch from KSC into more or less a 28 degree orbit. Changing the plane to satisfy Russian Baikonur constraints resulted in MAJOR shuttle payload hits; that meant (means!) elements have to be launched stripped-down and not fully operational, then outfitted on-orbit. That means adding flights to launch equipment and hardware which had been baselined for ground-based installation and checkout. That imposes increased testing (and possibly reliability/maintainability) requirements and adds lots of time to orbital assembly - lots more on-orbit rack-moving, connectors to be mated and verified, etc. Since the modules you're launching are not fully outfitted, you have lots of new operational constraints, too. For instance, deletion of the ECLSS ARS rack from the launch of the U.S. Lab module meant that all the procedures established for module entry and activation had to be redone: from verifying internal cabin atmosphere prior to hatch opening (which was to be done with the ARS GC/mass spectrometer and MCA) to software loads [the ARS rack had (has?) an MDM that also controlled equipment in other racks] to power-up procedures. The list goes on and on. All those things had to be changed for just about every system and every procedure due to the seemingly simple change to orbital inclination. -- Herb Schaltegger, B.S., J.D. Reformed Aerospace Engineer "Heisenberg might have been here." ~ Anonymous |
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