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#1
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Remember how we were going to have the Endeavour rescue Shuttle on 39B
ready to go in case Atlantis got marooned in orbit? Well, guess what? Maybe we don't need to do that after all: http://www.space.com/news/081219-sn-...x-impacts.html If something does go wrong with Atlantis, we had better hope we can do one quick turnaround on pad 39A. Pat |
#2
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On Sun, 21 Dec 2008 15:19:31 -0600, Pat Flannery
wrote: If something does go wrong with Atlantis, we had better hope we can do one quick turnaround on pad 39A. ....IIRC - and Jorge can confirm/deny this - we've done thought exercises on this in the past over on .shuttle, and IIRC the quickest "safe" turnaround was ~4 days. Of course, there's quite a few x-factors here, such as when in the mission the need for a rescue occurs, how much pad refurb can be done while the rescue vehicle is being moved from either the VAB or the other pad, and how much can either be slapdashed or skipped over altogether in order to get the rescue shuttle launched in time. ....Also, here's one I think we discussed, but I can't recall the answer right off, is whether a Progress resupply could be launched to Hubble orbit on short notice. This goes back to all the talk about "What If?" in the weeks following Columbia, and the n00b/Press questions about "why couldn't they just throw up food/water/fix-a-flat kits/etc until another shuttle could be launched?" OM -- ]=====================================[ ] OMBlog - http://www.io.com/~o_m/omworld [ ] Let's face it: Sometimes you *need* [ ] an obnoxious opinion in your day! [ ]=====================================[ |
#3
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On Dec 21, 5:21�pm, OM wrote:
On Sun, 21 Dec 2008 15:19:31 -0600, Pat Flannery wrote: If something does go wrong with Atlantis, we had better hope we can do one quick turnaround on pad 39A. ...IIRC - and Jorge can confirm/deny this - we've done thought exercises on this in the past over on .shuttle, and IIRC the quickest "safe" turnaround was ~4 days. Of course, there's quite a few x-factors here, such as when in the mission the need for a rescue occurs, how much pad refurb can be done while the rescue vehicle is being moved from either the VAB or the other pad, and how much can either be slapdashed or skipped over altogether in order to get the rescue shuttle launched in time. ...Also, here's one I think we discussed, but I can't recall the answer right off, is whether a Progress resupply could be launched to Hubble orbit on short notice. This goes back to all the talk about "What If?" in the weeks following Columbia, and the n00b/Press questions about "why couldn't they just throw up food/water/fix-a-flat kits/etc until another shuttle could be launched?" � � � � � � � � � � � � � � � � OM -- � �]=====================================[ � �] � OMBlog -http://www.io.com/~o_m/omworld� [ � �] � � � �Let's face it: Sometimes you *need* � � � � [ � �] � � � � �an obnoxious opinion in your day! � � � � � [ � �]=====================================[ boy not having a rescue shuttle and rushing ares? hopefully ares that disgrace of a bad idea will be killed by the new obama adminstration before then |
#4
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OM wrote in
: On Sun, 21 Dec 2008 15:19:31 -0600, Pat Flannery wrote: If something does go wrong with Atlantis, we had better hope we can do one quick turnaround on pad 39A. ...IIRC - and Jorge can confirm/deny this - we've done thought exercises on this in the past over on .shuttle, and IIRC the quickest "safe" turnaround was ~4 days. Of course, there's quite a few x-factors here, such as when in the mission the need for a rescue occurs, how much pad refurb can be done while the rescue vehicle is being moved from either the VAB or the other pad, and how much can either be slapdashed or skipped over altogether in order to get the rescue shuttle launched in time. More like 7, I think. But still possible. Both single-pad and dual-pad plans were considered for 125/400 the first time around, and dual-pad won out since it would take less labor on short notice, and there wouldn't be much impact on Ares I-X. Now that the slip has increased the impact of dual-pad ops for 125/400, single-pad is being reconsidered. ...Also, here's one I think we discussed, but I can't recall the answer right off, is whether a Progress resupply could be launched to Hubble orbit on short notice. This goes back to all the talk about "What If?" in the weeks following Columbia, and the n00b/Press questions about "why couldn't they just throw up food/water/fix-a-flat kits/etc until another shuttle could be launched?" No. Progress can't launch to 28.5 from Baikonur, Kourou has no handling facilities for Progress, and no deal is being negotiated. |
#6
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nasa should keep 2 ads operational till hubble service mission is
complete. lets say they dont, shuttle has a problem and the rescue mission fails for any reason. the lack of a second pad will be blamed, and nasa gets slammed as careless.......... |
#7
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On Dec 22, 2:24*am, "Brian Gaff" wrote:
The problem with the progress idea is pressurisation. I do not think there are facilities to unpressurise it on orbit unless its connected to a docking port. It kind of makes it hard to dock a Progress or a Soyuz to a stranded shuttle orbiter when they use two different types of docking mechanisms. Rigging up tethers to an unmanned vehicle, never mind depressurizing it are the least of the problems to consider in this scenario. As Jorge has pointed out, launching a Progress or a Soyuz down into a 28.5 degree inclination and at the Hubble altitude is well out of the Soyuz launcher's capability. -Mike |
#8
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#9
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![]() John Doe wrote: I terms of depresurization, if there are truly no operable valves to depressurise a progress in space, couldn't they just use a space hammer and a long nail to punch a hole in the pressure vessel ? As soon as the air starts shooting out, the Progress will start moving around from the thrust of the escaping gas. You might be able to store stuff in the unpressurized section of the Progress that replaces the Soyuz reentry module though (the pressurized section is a modified Soyuz orbital module), but it's not designed to go into that orbital inclination. So you would have to give the Russians a lot of advance notice (months) to even attempt it. On the other hand you could stick a grapple fixture on it for the Shuttle's RMS to grab and lower it into the cargo bay after rendezvous. But payload would be very limited to that high of a orbit at that low of a orbital inclination. We're pretty much counting on Atlantis working right or a very quick turnaround for pad 39A. Worth it? Hard to say. Recent Shuttle flights have been going very well as far as ascent damage goes. So the HST repair mission's overall risk is pretty low, but certainly not nonexistent. On the other hand, HST is getting long in the tooth and needs replacement...the recent failure of the communications system luckily occurred a few weeks before - not a few weeks after - the planned repair flight. It really does need to be replaced with the new generation Webb Space Telescope*, as we can learn a whole lot from having operated HST over the past 20+ years and its basic technology is getting pretty dated, having come from the late 1970s-early 1980s. For starters, we can grind the mirror correctly next time around. * http://webbtelescope.org/webb_telescope/ Pat |
#10
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![]() wrote in message ... On Dec 22, 2:24 am, "Brian Gaff" wrote: The problem with the progress idea is pressurisation. I do not think there are facilities to unpressurise it on orbit unless its connected to a docking port. It kind of makes it hard to dock a Progress or a Soyuz to a stranded shuttle orbiter when they use two different types of docking mechanisms. Rigging up tethers to an unmanned vehicle, never mind depressurizing it are the least of the problems to consider in this scenario. As Jorge has pointed out, launching a Progress or a Soyuz down into a 28.5 degree inclination and at the Hubble altitude is well out of the Soyuz launcher's capability. What about a Progress or Soyuz launched from Guyana? http://spaceports.blogspot.com/2007/...ch-guyana.html http://www.msnbc.msn.com/id/17421968/from/ET/ From the above article by James Oberg: Although the purpose of the new launch pad is mutual profit through commercial payload delivery to space, Russian officials make no secret of their long-range goal for the facility. It is human space flight - more Gagarins, on Russian-European spacecraft - using a new access highway to space that bypasses existing political bottlenecks in Kazakhstan and in Florida. Of course, wishful thinking on the part of the Russians wouldn't be enough. You'd have to have a Progress or Soyuz nearly ready to launch in order to make this work. Plus there are all othe other problems like how to grab Progress (you'd want a grapple fixture for the RMS to snag) and how to depressurize it and open the hatch. Jeff -- "Many things that were acceptable in 1958 are no longer acceptable today. My own standards have changed too." -- Freeman Dyson |
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