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LAUNCH DAY ARTICLE: http://www.nasaspaceflight.com/content/?cid=5302 - will be updated throughout this launch attempt.
This is the live update thread for the launch. Should we have a successful launch, it will continue as the Flight Day 1 Live Update thread.
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Firstly, if you are guest, please note it is reccomended that you create yourself a login, as we protect the site's servers in the event of overloading by making it member only, see here: http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=10291&posts=4&start=1 (membership to the open sections of the site is free).
This is a live update thread, so we do not want any "woo hoo, go Atlantis" comments clogging up the updates. We have a cheerleading thread for your best wishes:
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=10978&start=1
We also have a seperate weather specific thread, for comments on the status of the pre-launch weather: http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=11028&posts=13&start=1
If you are in Florida for the launch and need tips on where to go for best viewing, we have a thread for that: http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=10458&start=1
All NASA TV video for the mission is available - for free - here: http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=10045&start=1
If you're learning about the Shuttle - and let's face it, we all are unless your Wayne Hale - you are encouraged to ask questions, but please keep them here: http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=10600&start=1
Moderators will delete - without notification - any posts that do not follow the above request.
God Speed Atlantis.
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Last night, via L2, our pad rats were saying they were two hours down on the timeline (S0007) at RSS retract.
This is not unlike previous, and we're waiting now for the go for tanking.
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Tanking expected to begin in one hour.
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Atlantis, under the lights, ready to get a little cold with the tanking..
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No NASA TV coverage of the launch for another 5 hours yet...so we're totally reliant on NSF for yet another great launch day coverage :)
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Atlantis at dawn.
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Everything nominal for on time tanking at six minutes past the hour (about 15 mins from now).
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T- 6 hours and counting.
:)
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Chilldown and slow fill. No issues being worked.
Bipod area and a dawn Atlantis.
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17 inch LOX Feedline (about to get rather cold!). Nice look at an IFR (Ice Frost Ramp) too.
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Chris Bergin - 6/12/2007 7:20 AM
17 inch LOX Feedline (about to get rather cold!). Nice look at an IFR (Ice Frost Ramp) too.
And one of the feedline brackets. (And the cable tray, etc.)
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Loving the work by the camera operator!
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Troubleshooting a communications asset. Still has redundancy.
Meanwhile...
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Chris Bergin - 6/12/2007 6:37 AM
Troubleshooting a communications asset. Still has redundancy.
Meanwhile...
So no constraint to launch?
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shuttlefan - 6/12/2007 12:38 PM
Chris Bergin - 6/12/2007 6:37 AM
Troubleshooting a communications asset. Still has redundancy.
Meanwhile...
So no constraint to launch?
Working the info on L2. LCC allows for 1 of 2. Preference is 2, hense troubleshooting. Technically no constraint to launch on the LCC.
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Bit of ground fog at the moment...
(bottom is one of the end of the runway cams at the SLF)
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About to head into fast fill (after 5 percent - if memory serves - loading). Slowfill = no issues.
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Great images from Tanking.
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Loving these images!!
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Problems with the ECOs. More shortly.
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Launch may be scrubbed shortly.
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Crap-O-la.. ECO sensors - remind me - those the fuel cutoff sensors in the tank that gave problems on 114?
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John2375 - 6/12/2007 2:50 PM
Crap-O-la.. ECO sensors - remind me - those the fuel cutoff sensors in the tank that gave problems on 114?
Yes and 115.
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It also was a problem with 115.
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Troubleshooting. Two of the sensors failed. Lots going on, but they are reccomending scrub. Standby...
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Oh.Such a good weather today.Hopefully problem with ECO's can be solved.
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I believe that the issues on 114 and 115 are still essentially unexplained anomalies (UA), although they have more data in this case with the orbiter wiring mods that were made.
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yeah it's GORGEOUS here in FL today.. and Mom was ready to watch in the SE sky up in New England to see it today too :( they better fix it.
If they can't and they scrub, what can they do to be sure it doesnt' happen at the next attempt?? And would that be a 24 or 48 hr. scrub? or more?
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Quotes and notes from L2 coverage are going into the main article, remember:
http://www.nasaspaceflight.com/content/?cid=5302
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I'm thinking they will stand down 24 hours, de-tank, and try again Tomorrow
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Chris Bergin - 6/12/2007 8:00 AM
Quotes and notes from L2 coverage are going into the main article, remember:
http://www.nasaspaceflight.com/content/?cid=5302
No one else is reporting this (SFN, Florida Today). You sure?
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John2375 - 6/12/2007 8:59 AM
yeah it's GORGEOUS here in FL today.. and Mom was ready to watch in the SE sky up in New England to see it today too :( they better fix it.
If they can't and they scrub, what can they do to be sure it doesnt' happen at the next attempt?? And would that be a 24 or 48 hr. scrub? or more?
They better fix it because...why? They are working on it, they have been working on the UA since spring 2005 when they first saw it. All we can do on the outside is observe.
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This site is always ahead, thatīs something I learned with time... :D
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SCRUB is what we're hearing on L2.
Crikey, and rollback (not official).
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ECO sensors again? This is beyond ridiculous.
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SCE2Aux - 6/12/2007 8:07 AM
ECO sensors again? This is beyond ridiculous.
You've got that right! :angry:
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Chris Bergin - 6/12/2007 2:04 PM
SCRUB is what we're hearing on L2.
Crikey, and rollback (not official).
I'm guessing they may want to swap these sensors out. If it's a rollback then launch won't be until next year and that's going to impact all the other launches... damn and all that hard work done on the ISS to relocate Harmony.
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What I canīt believe is that we had over 100 flights without this problem, and after RTF we have it now and then! Seems the problem is with the batch of sensors
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SCE2Aux - 6/12/2007 9:07 AM
ECO sensors again? This is beyond ridiculous.
I don't know why it's ridiculous. If this is related to the previous cases, it's still unexplained behavior, which makes it hard to "fix." If it isn't fixed, then I don't see why it couldn't happen again.
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Are they continuing to fill the external tank until it's full or have they suspended fueling?
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It must be disappointing enough for the astronauts for a 24/48 hour postponement. But a "come back after Christmas" must be a real kick in the pants for them :( And all the ESA people too. But, that's life in the space industry I guess.
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Bruce - 6/12/2007 2:14 PM
It must be disappointing enough for the astronauts for a 24/48 hour postponement. But a "come back after Christmas" must be a real kick in the pants for them :( And all the ESA people too. But, that's life in the space industry I guess.
And for Dan Tani's family. If this is a rollback then he is stuck in orbit over Christmas.
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On the NASA Launch and Landing page the countdown clock is still running.
So I guess this could mean they are still filling the tank - or the just are not as fast as this website
Thanks for the excellent coverage!
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Gary - 6/12/2007 7:15 AM
Bruce - 6/12/2007 2:14 PM
It must be disappointing enough for the astronauts for a 24/48 hour postponement. But a "come back after Christmas" must be a real kick in the pants for them :( And all the ESA people too. But, that's life in the space industry I guess.
And for Dan Tani's family. If this is a rollback then he is stuck in orbit over Christmas.
Heavy on "if". Rollback is far from certain.
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They are going to look at the sensors again during detank. Could be electrical connectors/paths at fault. Not sure how long that fix would be at the pad.
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Can this scrub be confirmed?
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Bejowawo - 6/12/2007 2:15 PM
So I guess this could mean they are still filling the tank - or the just are not as fast as this website
They stopped loading the tank a while ago.
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ok thanks.
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psloss - 5/12/2007 2:10 PM
SCE2Aux - 6/12/2007 9:07 AM
ECO sensors again? This is beyond ridiculous.
I don't know why it's ridiculous. If this is related to the previous cases, it's still unexplained behavior, which makes it hard to "fix." If it isn't fixed, then I don't see why it couldn't happen again.
Whoever made these sensors did a shoddy job, that's what is ridiculous: How hard can it be for supposedly smart people to make a sensor whose sole purpose is to work out whether there's liquid in the tank or not?
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SCE2Aux - 6/12/2007 2:23 PM
psloss - 5/12/2007 2:10 PM
SCE2Aux - 6/12/2007 9:07 AM
ECO sensors again? This is beyond ridiculous.
I don't know why it's ridiculous. If this is related to the previous cases, it's still unexplained behavior, which makes it hard to "fix." If it isn't fixed, then I don't see why it couldn't happen again.
Whoever made these sensors did a shoddy job, that's what is ridiculous: How hard can it be for supposedly smart people to make a sensor whose sole purpose is to work out whether there's liquid in the tank or not?
Careful. It might not even be the sensors. Could be electrical paths, GSE, orbiter aft. etc.
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dember - 6/12/2007 9:20 AM
Can this scrub be confirmed?
Good rule of thumb for newbies: this site is always ahead of the other news sites. There are actually people who work for NASA here, and a lot of the info here comes in real-time.
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SCE2Aux - 6/12/2007 9:23 AM
Whoever made these sensors did a shoddy job, that's what is ridiculous: How hard can it be for supposedly smart people to make a sensor whose sole purpose is to work out whether there's liquid in the tank or not?
There's a whole instrumentation circuit and so far they haven't been able to isolate the problem to a particular location in the circuit. In the meantime, they went through their sensor inventory, reverified the quality controls, and replaced sensors from suspect lots.
How do you know it's the sensors?
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SCE2Aux - 6/12/2007 9:23 AM
Whoever made these sensors did a shoddy job, that's what is ridiculous: How hard can it be for supposedly smart people to make a sensor whose sole purpose is to work out whether there's liquid in the tank or not?
It's safe to say that that we're all a bit frustrated at not having a launch today. But it's pointless to start laying blame or criticizing when we don't even know where the problem is yet.
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Why wouldn't they use another type of sensor (just as a backup) when they know they cannot fully trust those sensors currently used.
Another question, just for clarification: There will be another lauch attempt tomorrow or is this too early to tell?
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when it happened on -114, did they roll back or fix at the Pad??
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They have a short trouble shooting window to have a look before calling a stop to today, but scrub does look very likely.
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John2375 - 6/12/2007 8:35 AM
when it happened on -114, did they roll back or fix at the Pad??
On the pad.
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ok that's what I thought - so why is everyone saying "rollback!" if they coudl fix it there then maybe support a 1/2/08 launch?
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Bejowawo - 6/12/2007 9:35 AM
Why wouldn't they use another type of sensor (just as a backup) when they know they cannot fully trust those sensors currently used.
In part because they don't know that the sensor is the root cause.
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John2375 - 6/12/2007 8:40 AM
ok that's what I thought - so why is everyone saying "rollback!" if they coudl fix it there then maybe support a 1/2/08 launch?
What are the launch windows for this mission?
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Is it a confirmed scrub yet?
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John2375 - 6/12/2007 9:40 AM
ok that's what I thought - so why is everyone saying "rollback!" if they coudl fix it there then maybe support a 1/2/08 launch?
Because they may be able to see more data and/or analysis than we can. One of the things they did was add more instrumentation in the orbiter; that might help rule-in/rule-out things that they couldn't rule in or out during the last tanking with this issue on STS-115.
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Satori - 6/12/2007 8:42 AM
What are the launch windows for this mission?
The launch period is December 6 through December 13.
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If the managing editor says "Scrub", then it is official. He also reported hearing speculation on a possible rollback. These are from sources "in the know", not just people sitting in front of their computers making it up as they go. As stated previously, this site has direct access to people involved in NASA, and the L2 part of this site has actual, real-time information during the decision-making processes at NASA.
EDIT: redundant comment...
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How long is the launch window open for today?
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NASA just updated the Space Shuttle page
Approximately 16 minutes into fast fill, two ECO sensors failed to indicate wet. They are troubleshooting the issue. Currently, H2 is at 80% and O2 is at 50%. Tanking is continuing. We expect to have a status from leadership soon as to whether we continue or scrub. If we scrub, a briefing will follow that decision on NASA TV.
http://www.nasa.gov/mission_pages/shuttle/main/index.html
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launch window extends for 10 minutes.
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dember - 6/12/2007 2:43 PM
Is it a confirmed scrub yet?
As in PAO? Not yet.
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thanks Chris
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Harwood has put up a good historical background here:
http://spaceflightnow.com/shuttle/sts122/071206ecos/
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dember - 6/12/2007 2:58 PM
thanks Chris
Should be soon. It's now over the loop they are scrubbed.
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Officially scrubbed. 24 hour turnaround.
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Just put up a graphic on NASA TV...conference time TBD.
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Noted it in the article, but should here: One potential plan is to enter the aft, demate and remate the monoball electrical connections to see if bad electrical path.
Remember, it might not be the sensors themselves - especially when these sensors in question are hand picked.
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While it is of course disappointing with the scrub (especially when everything else was going so smooth), it's good to see NASA is making the right decision for the safety of crew and vehicle.
I know I had a bad case of go fever. ;)
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I was hoping for a launch today.
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Better we should have a case of "get it right" Fever that never breaks.
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Launch weather for tomorrow?
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Have the ISS crew been informed?
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dember - 6/12/2007 10:15 AM
Launch weather for tomorrow?
Yep.
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=11028
Gary - 6/12/2007 10:17 AM
Have the ISS crew been informed?
Nothing heard on the ISS audio feed.
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dember - 6/12/2007 10:15 AM
Launch weather for tomorrow?
The launch weather thread is here: http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=11028&posts=16#M220242
It gets updated frequently, so is better to check it directly. Quick summary at the moment: KSC chance for showers is up a little bit, 2 of 3 TAL sites still good, slight chance of rain off the coast at Edwards for AOA.
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Well, we almost had 4 for 4 launches on the first attempt this year. Chris, I would change the batteries in that rabbit's foot ;)
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Status update briefing shown as 10:30 am Eastern.
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What's the scheduled launch window for tomorrow if they get it all figured out?
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Now they are going to do this 10:30 am update as a status from the firing room...still busy, obviously...
Edit -- this may be PAO commentary or PAO interviewing someone...
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Gary - 6/12/2007 10:28 AM
ntschke - 6/12/2007 3:27 PM
What's the scheduled launch window for tomorrow if they get it all figured out?
Each day the launch window gets around 20 minutes earlier so expect it to be around 21:10 GMT.
FYI, here's Bill Harwood's chart for December:
http://www.cbsnews.com/network/news/space/122/122windows.html
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Mission Management Team Chairman LeRoy Cain concurred following a short briefing on the issue. The ice inspection team will proceed with an abbreviated vehicle inspection prior to offloading the LO2 and LH2 and recycle for a launch attempt tomorrow, at 4:09 p.m.
A press briefing is tentative scheduled for 3 p.m. An update is forthcoming on NASA TV. (nasa.gov)
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I'd imagine Launch Director Doug Lyons will be in on this briefing.
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ISS comms were down due to TDRS problems, now back online. Officially scrubbed today, turnaround meeting at 19Z earliest (2pm EST) and at that point they'll know if tomorrow is an option.
2 of the LH2 low-level cutoff sensors failed to show dry when they were simulated commanded.
(Those were MCC-Houston's words to ISS)
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PAO George Diller with LD Doug Lyons...
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"Hopefully it's just a connecter issue as that would be easiest to fix" (ISS ground)
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"If we'd have sent you to the Cape, we might have launched yesterday!"
(MCC-Houston's words to a certain member onboard ISS :> )
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I believe Doug Lyons noted that the preliminary indication is of an open circuit somewhere in the instrumentation (already reported on L2). Teams are going to regroup at noon local to evaluate options, report to the MMT, which will meet at 1400 local.
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rdale - 6/12/2007 4:37 PM
"Hopefully it's just a connecter issue as that would be easiest to fix" (ISS ground)
Let's hope so or else it will be another rollback to the VAB.
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They are still in stable replenish to facilitate an expedited inspection by the final inspection team (they are budgeting about an hour). After that, they will start draining and are working the 24 hour turnaround procedures to preserve that option. (Doesn't mean they have decided to try tomorrow.)
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Correction: the final inspection team has been out at the pad for a while, but they have budgeted approx. another hour before they will clear the pad to begin drain around 11:30 am local.
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Just repeating, but the post MMT briefing is scheduled for approximately 4 pm local.
(Edit -- changing NET to approx., as that's what George Diller said.)
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So the ET was filled up to 100% today then, or can they put it into stable replenish even when it's not full?
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shuttlefan - 6/12/2007 3:50 PM
So the ET was filled up to 100% today then, or can they put it into stable replenish even when it's not full?
Good question. We know they went to 80 percent. We know they stopped. Question is if - when they decided to use the opportunity to send the Ice Team out there - they then went and filled up, to bring the tank to stable replenish (I would guess so. I'll grab and ET guy and find out, but they are all rather busy, as I'm sure you can understand!)
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Hopefully they can get off the ground tomorrow.
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dember - 6/12/2007 3:55 PM
Hopefully they can get off the ground tomorrow.
Let's just hope the weather holds out..
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Since this has happened before, would it be possible for them to do a mini-tanking test when they get to the pad? just to see how the sensors are acting? Or would the be useless since odds are, tomorrow, they'll be just fine..
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ShuttleDiscovery - 6/12/2007 10:59 AM
dember - 6/12/2007 3:55 PM
Hopefully they can get off the ground tomorrow.
Let's just hope the weather holds out..
Given the situation, I'd say weather is far down on the list of concerns. I'd trade most poor weather conditions for this anomaly because in most weather cases they can come back tomorrow. It's still very much undecided (at least from the outside looking in) whether that's the case currently.
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Video STS-122 - Atlantis Status Update
http://www.space-multimedia.nl.eu.org/index.php?option=com_content&task=view&id=3181&Itemid=2
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Thanks for turning that around so quickly, John44.
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John2375 - 6/12/2007 10:05 AM
Since this has happened before, would it be possible for them to do a mini-tanking test when they get to the pad? just to see how the sensors are acting? Or would the be useless since odds are, tomorrow, they'll be just fine..
Well, if you mean WHEN THE TECHNICIANS GET TO THE PAD, no, because the pad has to be completely evacuated when the propellant is actually flowing. ;)
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If the issue is not with the sensors themselves, but rather with electrical connectivity, why would it not have been detected during the run-up to launch day? They seem to have the ability to test most, if not all of the electrical connections on the stack prior to actual use.
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Chris Bergin - 6/12/2007 9:52 AM
shuttlefan - 6/12/2007 3:50 PM
So the ET was filled up to 100% today then, or can they put it into stable replenish even when it's not full?
Good question. We know they went to 80 percent. We know they stopped. Question is if - when they decided to use the opportunity to send the Ice Team out there - they then went and filled up, to bring the tank to stable replenish (I would guess so. I'll grab and ET guy and find out, but they are all rather busy, as I'm sure you can understand!)
Yep, thanks in advance Chris!! :)
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Lee Jay - 6/12/2007 11:18 AM
If the issue is not with the sensors themselves, but rather with electrical connectivity, why would it not have been detected during the run-up to launch day? They seem to have the ability to test most, if not all of the electrical connections on the stack prior to actual use.
In the past cases, the behavior has been intermittent and seemed to only occur under cryogenic conditions. (In other words: test the sensors at ambient and they behave one way; then test the sensors during tanking at cryogenic temps and then they exhibit multiple behaviors.)
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While I want to see the shuttle launch as soon as possible, I'll be in Orlando over New Years and would absolutely LOVE to take kids to see our first shuttle launch while down there!
Is there a scenario with a Jan 2 launch date? Seems like any work would have to be done at the pad, not enough time to roll back?
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psloss - 6/12/2007 5:23 PM
Lee Jay - 6/12/2007 11:18 AM
If the issue is not with the sensors themselves, but rather with electrical connectivity, why would it not have been detected during the run-up to launch day? They seem to have the ability to test most, if not all of the electrical connections on the stack prior to actual use.
In the past cases, the behavior has been intermittent and seemed to only occur under cryogenic conditions. (In other words: test the sensors at ambient and they behave one way; then test the sensors during tanking at cryogenic temps and then they exhibit multiple behaviors.)
Yes. During the extensive troubleshooting activities between the first and second launch attempts of STS-114 they spent nearly two weeks trying to recreate the problems with the ECO sensor system in ambient temps with no results leading them to recommend going to cryogenic temps.
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TrueBlueWitt - 6/12/2007 4:24 PM
While I want to see the shuttle launch as soon as possible, I'll be in Orlando over New Years and would absolutely LOVE to take kids to see our first shuttle launch while down there!
Is there a scenario with a Jan 2 launch date? Seems like any work would have to be done at the pad, not enough time to roll back?
We'll be continuing with this thread through troubleshooting.
Right now it's NET tomorrow. Data being collected for the engineering community. Engineers will tag-up (Orbiter, ET Project etc). Go to MMT. Work the forward plan.
All depends on the location of the fault on how long the wait will be, and we're working on that info via L2. Will summarize here/article later on.
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Super George - 6/12/2007 8:02 AM
Chris Bergin - 6/12/2007 8:00 AM
Quotes and notes from L2 coverage are going into the main article, remember:
http://www.nasaspaceflight.com/content/?cid=5302
No one else is reporting this (SFN, Florida Today). You sure?
Hah, welcome to the site ;)
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DaveS - 6/12/2007 9:29 AM
psloss - 6/12/2007 5:23 PM
Lee Jay - 6/12/2007 11:18 AM
If the issue is not with the sensors themselves, but rather with electrical connectivity, why would it not have been detected during the run-up to launch day? They seem to have the ability to test most, if not all of the electrical connections on the stack prior to actual use.
In the past cases, the behavior has been intermittent and seemed to only occur under cryogenic conditions. (In other words: test the sensors at ambient and they behave one way; then test the sensors during tanking at cryogenic temps and then they exhibit multiple behaviors.)
Yes. During the extensive troubleshooting activities between the first and second launch attempts of STS-114 they spent nearly two weeks trying to recreate the problems with the ECO sensor system in ambient temps with no results leading them to recommend going to cryogenic temps.
This I understand, but I don't understand why cryo in the tank would affect electrical connectivity in the orbiter aft, or areas even further up-stream from there.
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Correct me if I'm wrong, but aren't the tanks used since RTF, up through this flight, tanks that were all or partially-built pre-RTF then modified with the RTF modifications? Also, hasn't the ECO sensor issue only been prevalent since RTF? If so, then perhaps there is some commonality with the mods and this issue.
EDIT: In particular, I'm concerned with the electrical trays and the bipod ramps, although I would expect them to have more effect on the O2 sensors than the H2...
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John2375 - 6/12/2007 10:05 AM
Since this has happened before, would it be possible for them to do a mini-tanking test when they get to the pad? just to see how the sensors are acting? Or would the be useless since odds are, tomorrow, they'll be just fine..
Tanking the vehicle puts thermal stress on the tank and is believed to be a factor in foam liberation from the tank. So NASA wants to perform as few tanking cycles as possible. Therefore there is no point in a separate tanking test; the actual tanking for the launch attempt constitutes the test.
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oh ok - that makes sense. I remember them doing mini-tanking tests for STS-38 and STS-35 because of the hydrogen leaks, but yeah, these days w/the thermal issues on the tank I can see why.
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What happens to the LOX and LH2 during the detanking? It is returned to the storage tanks and reused?
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Ray Todd - 6/12/2007 1:20 PM
What happens to the LOX and LH2 during the detanking? It is returned to the storage tanks and reused?
yes
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*Sigh* The Launch Prevention Devices strike again...
And so much for having 4 straight launches this year that took off on the first attempt.
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Where are we in the count? Have they recycled to T-11?
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Are these sensors actually used to determine when MECO should occur, under normal circumstances? (My recollection is that they are not a normal control point for launches, but are only a contingency for engine protection). If they are "contingency" sensors, how quickly does a true "dry" signal need to be acted on to protect the orbiter? Human speed, or quicker? Or if the consequences are less, like SSME damage but no orbiter effects, can they actually be ignored without threatening this mission (although possibly incurring costs for future)?
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punkboi - 6/12/2007 12:28 PM
*Sigh* The Launch Prevention Devices strike again...
And so much for having 4 straight launches this year that took off on the first attempt.
I'll take launch safety assurance over an first-try-four-times-in-a-row record any day.
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Joffan - 6/12/2007 12:33 PM
Are these sensors actually used to determine when MECO should occur, under normal circumstances? (My recollection is that they are not a normal control point for launches, but are only a contingency for engine protection). If they are "contingency" sensors, how quickly does a true "dry" signal need to be acted on to protect the orbiter? Human speed, or quicker? Or if the consequences are less, like SSME damage but no orbiter effects, can they actually be ignored without threatening this mission (although possibly incurring costs for future)?
I don't believe they're used in normal scenarios, but I could be wrong. I say that because there has been a case of 'low-level cutoff' (STS-93) in which the ECO sensors went dry a little early in the ascent, resulting in a slight underspeed for Columbia. It would take a small fraction of a section to send and execute the shutdown command. And there aren't 'contingency' sensors. They only need two, but they have four for complete redundancy incase one or two fail on the way uphill. And we're not talking slight damage to SSMEs in the case of ECO sensor failure. We're talking catastrophic engine failure that would quickly and easily lead to orbiter damage or even destruction, I believe.
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The placement of the sensors take into account the timing needed to shutdown the engines. Engine fuel depletion can cause many things, two of which are: an Ox shutdown where the metal of the engine burns and or an unloaded H2 turbopump, that goes from spinning at 36,000 rpm to infinity
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Also, in the case of sensor ECO, the first signal is ignored to guard against a premature shutdown due to sensor faults. This means that with two potentially failed sensors, there would be no redundancy left in this scenario.
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Joffan - 6/12/2007 12:33 PM
Are these sensors actually used to determine when MECO should occur, under normal circumstances? (My recollection is that they are not a normal control point for launches, but are only a contingency for engine protection). If they are "contingency" sensors, how quickly does a true "dry" signal need to be acted on to protect the orbiter? Human speed, or quicker? Or if the consequences are less, like SSME damage but no orbiter effects, can they actually be ignored without threatening this mission (although possibly incurring costs for future)?
Here is a very high level overview of how these ECO sensors work that I wrote for Interspacenews during the STS-114 timeframe.
http://www.interspacenews.com/interspace%20News%20Web%202/sections/In%20focus/ECO%20Sensors.htm
Bill Harwood wrote one for CBS/Spaceflight Now that is probably better to undersand than mine (since he writes much better than me) so if anyone knows where that link is feel free to post that here as well.
Mark Kirkman
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mkirk - 6/12/2007 12:46 PM
Bill Harwood wrote one for CBS/Spaceflight Now that is probably better to undersand than mine (since he writes much better than me) so if anyone knows where that link is feel free to post that here as well.
Mark Kirkman
I thought I had, a few pages back...
Yup, here at 8:59 AM:
Harwood has put up a good historical background here:
http://spaceflightnow.com/shuttle/sts122/071206ecos/
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JimO - 6/12/2007 12:51 PM
mkirk - 6/12/2007 12:46 PM
Bill Harwood wrote one for CBS/Spaceflight Now that is probably better to undersand than mine (since he writes much better than me) so if anyone knows where that link is feel free to post that here as well.
Mark Kirkman
I thought I had, a few pages back...
Yup, here at 8:59 AM:
Harwood has put up a good historical background here:
http://spaceflightnow.com/shuttle/sts122/071206ecos/
Sorry JimO, as usuall I am late to the party.
;)
Mark Kirkman
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Thanks for the answers guys. I guess the summary is: the ECO sensors wouldn't be used to determine actions in a perfectly nominal ascent, but if a tank runs dry early without engine cutoff, the rapid consequences could include loss of orbiter and crew.
(and Mark, your link leads back here...) (no longer... thanks again)
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When should we expect the next attempt to launch?
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Joffan - 6/12/2007 1:11 PM
Thanks for the answers guys. I guess the summary is: the ECO sensors wouldn't be used to determine actions in a perfectly nominal ascent, but if a tank runs dry early without engine cutoff, the rapid consequences could include loss of orbiter and crew.
(and Mark, your link leads back here...)
Sorry. I fixed it.
http://www.interspacenews.com/interspace%20News%20Web%202/sections/In%20focus/ECO%20Sensors.htm
Mark Kirkman
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Yegor - 6/12/2007 1:13 PM
When should we expect the next attempt to launch?
Just too soon to call, not enough data yet.
Tomorrow is very unlikely!!!
Mark Kirkman
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Yegor - 6/12/2007 1:13 PM
When should we expect the next attempt to launch?
Last time something like this happened (STS-114) it took about two weeks before the next attempt. But it all depends on how fast they can find a source for the problem and resolve it. We'll just have to sit back and let them work their magic.
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What about STS-115?
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Thank you very much for quick answers! :)
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dember - 6/12/2007 1:21 PM
What about STS-115?
STS-115 had so many delays I honestly can't remember what happened with the ECO sensors for that flight. I think it resolved itself but someone else will have to elaborate.
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Yegor - 6/12/2007 1:22 PM
Thank you very much for quick answers! :)
Our pleasure :) All part of the NSF community.
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dember - 6/12/2007 2:21 PM
What about STS-115?
In that case, they followed the procedure agreed upon after STS-114, which was to detank and then retank the next day. None of the circuits failed WET on the second attempt and they launched.
This situation isn't exactly the same as two of the LH2 ECO measurements are showing this behavior; in the previous launch attempt cases, only one measurement failed WET.
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I dont get how on one try the ECOs dont work and then next try they do. Seems a little odd. Such an important part needs to work 100% of the time. Running out of gas in a car is inconvinent. Running out of gas on the shuttle is deadly (the turbo pumps spin out of control).
Its like a PC. One day it acts up, you dont do anything to fix it, the next try its fine...huh? I remember thats what they did the last time the ECOs failed wet. Just try again and hope for the best.
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Would be nice if there was some sort of test they could run in the VAB BEFORE they rolled out and all that to find out before that the ECOs where toast. Makes me worry about the CEV Stick and the LEV Launcher, they will probably have the same sensors!
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Zoomer30 - 6/12/2007 1:37 PM
I dont get how on one try the ECOs dont work and then next try they do. Seems a little odd. Such an important part needs to work 100% of the time. Running out of gas in a car is inconvinent. Running out of gas on the shuttle is deadly (the turbo pumps spin out of control).
Its like a PC. One day it acts up, you dont do anything to fix it, the next try its fine...huh? I remember thats what they did the last time the ECOs failed wet. Just try again and hope for the best.
It's a pretty complex little piece of equipment. And some believe the problem isn't in the sensors themselves. Some think it's related to connections between the sensors and the orbiter avionics. Very, very complex.
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Zoomer30 - 6/12/2007 2:40 PM
Would be nice if there was some sort of test they could run in the VAB BEFORE they rolled out and all that to find out before that the ECOs where toast. Makes me worry about the CEV Stick and the LEV Launcher, they will probably have the same sensors!
They won't
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It would make it easier if they could run tests.
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Its like a light switch that one day you hit it and the light does not come on, the next day it works fine.
That article ECO SENSORS 101 explains the issue well. Reading that makes me wonder if we should even be flying with such a touchy and important item that has an issue that just cant be explained. From that ECO 101 article it seems the sensors could fail dry and shut the engines off way early, or fail wet and run out of fuel or O2. Run out of fuel and you have a oxygen rich issue, lots of fire risk. The other way and you have turbo pump cavitation, they go from normal speed to who knows how fast in the blink of an eye and come apart.
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MMT meeting to discuss 24 hours or longer on the turnaround.
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Zoomer30 - 6/12/2007 2:50 PM
From that ECO 101 article it seems the sensors could fail dry and shut the engines off way early, or fail wet and run out of fuel or O2. Run out of fuel and you have a oxygen rich issue, lots of fire risk. The other way and you have turbo pump cavitation, they go from normal speed to who knows how fast in the blink of an eye and come apart.
That's why they have four of them on both sides.
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dember - 6/12/2007 1:49 PM
It would make it easier if they could run tests.
They do run tests. They run tests several times during the launch countdown. You have to fill the tank to truly test these things out. That way they can run simulated dry commands and make sure they're functioning properly. It won't help you much to run tests when the tank is empty. You'll be making sure they'll show 'dry' when it's really dry. But you have to make sure it'll will also show 'wet' when it's loaded. It HAS to work both ways, and the only way to try it out is by filling the tank on launch day. If it works, great. If not, find the problem, fix it and try again.
This sort of thing happens, people. This is how they've approached this sort of problem before and, just like all the others, they'll get it fixed for STS-122. Let's quit questioning/criticizing their methods and let them do their jobs. For all we know, they could try tomorrow and everything could work fine. Just sit back and enjoy the ride.
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psloss - 6/12/2007 1:53 PM
Zoomer30 - 6/12/2007 2:50 PM
From that ECO 101 article it seems the sensors could fail dry and shut the engines off way early, or fail wet and run out of fuel or O2. Run out of fuel and you have a oxygen rich issue, lots of fire risk. The other way and you have turbo pump cavitation, they go from normal speed to who knows how fast in the blink of an eye and come apart.
That's why they have four of them on both sides.
It's also why they have four instead of the required two. If something goes wrong with one, or even two, sensors, they have complete redundancy to pick up the slack.
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Added some more: http://www.nasaspaceflight.com/content/?cid=5302
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One positive here (in a back-handed kind of way) is that the SIM DRY signal identfied a real issue wth sensors #3 and #4, as evidenced by their behaviour on de-tanking.
This means to me that if the Shuttle team does decide to have another try tomorrow, and the sensors show good in the tests, we can have a high level of confidence in that result.
(ETA: I'm counting the whole signal path as part of the sensor here).
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Up beanie and waiting patiently....
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http://www.cbsnews.com/network/news/space/current.html
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It looks like the afternoon briefing is going to slip, no new time as yet (MMT is still in progress).
I am sure nobody is surprised.
Mark Kirkman
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Does the flight crew have any input on the final decision of whether to try again tomorrow or not?
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ECO sensors still acting strange even now. Engineers are concerned, as LH2 ECO #1 went WET for no reason within the last hour.
Really not sure how the FD is thinking this is looking good for tomorrow, but we'll see what the MMT say.
MMT on a break, about to head back in.
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MSNBC is reporting that the decision is going to be to resume the count for an attempt tomorrow acording to "anonymous sources".
http://www.msnbc.msn.com/id/22120058/
Anyone else hearing this?
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MMT will decide that and they are still meeting. That would have been prior to the new ECO issue, also.
"Anonymous sources" will be engineers etc..the same sort of thing we work off. You can't go naming sources.
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NASA TV posted this briefly a few moments back. NET 5 pm Eastern, but probably emphasis on the NET.
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Beanie Cap removed from top of external tank. Atlantis' Postponement meeting scheduled for NET 5:00 PM EST.
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Briefing now NET 5:30 pm Eastern...
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The "beanie cap" removal....is that a sign the RSS will be rolled back?
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Bubbinski - 6/12/2007 4:55 PM
The "beanie cap" removal....is that a sign the RSS will be rolled back?
No...and FWIW, they switched to a live pad shot on NASA TV...
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Not sure if these can go here, so mods feel free to delete if they aren't..
NASA TV had a nice promo of Columbus.. Grabbed some snaps:
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Cool video. Back with a live shot at the pad... heading into sunset:
EDIT: They've either opened the iris on the camera.. or something..
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Ford Mustang - 6/12/2007 5:04 PM
Not sure if these can go here, so mods feel free to delete if they aren't..
NASA TV had a nice promo of Columbus.. Grabbed some snaps:
It was nice to see - John44 has it on his site...
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psloss - 6/12/2007 9:49 PM
Briefing now NET 5:30 pm Eastern...
I reckon it'll be later, as MMT is still meeting and has a way to go yet.
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Beanie Cap now back atop the ET, not lowered onto it, though..
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Chris Bergin - 6/12/2007 5:19 PM
psloss - 6/12/2007 9:49 PM
Briefing now NET 5:30 pm Eastern...
I reckon it'll be later, as MMT is still meeting and has a way to go yet.
Just passing along the updates as I see them on NASA TV...which just showed the GOX vent arm being swung back over to the tank.
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And now they are showing a graphic with NET 6:00 pm Eastern...
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Chris Bergin - 6/12/2007 5:19 PM
psloss - 6/12/2007 9:49 PM
Briefing now NET 5:30 pm Eastern...
I reckon it'll be later, as MMT is still meeting and has a way to go yet.
NET 6:00 PM EST.
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NET 6:30pm and could be later.
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Chris Bergin - 6/12/2007 3:48 PM
NET 6:30pm and could be later.
So where are we? Are the teams currently performing the 24 hour scrub-turnaround procedures while waiting for the MMT to conclude?
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Even when she's grounded, Atlantis is a beautiful bird... (taken about an hour ago during an unexpected photo opp organized by KSC PAO).
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Lee Jay - 6/12/2007 5:50 PM
Chris Bergin - 6/12/2007 3:48 PM
NET 6:30pm and could be later.
So where are we? Are the teams currently performing the 24 hour scrub-turnaround procedures while waiting for the MMT to conclude?
That was the last report. The launch team is preserving the option of tanking tomorrow, but I think some people are inferring (incorrectly) that means they will tank tomorrow. Haven't seen a report of any decisions out of the MMT yet.
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collectSPACE - 6/12/2007 5:51 PM
Even when she's grounded, Atlantis is a beautiful bird... (taken about an hour ago during an unexpected photo opp organized by KSC PAO).
AWESOME photo. Got a high res shot of that around anywhere?
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Bit of tangent, but watching them manually "re-white balance" OTV 070 for the extreme light changes brings back memories of an old, pre-CCD camcorder.
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If anyone has an answer.. I'm currently wondering if they are going to turn the Xenon lights on??
Also, photos from the photo-opp about an hour ago now in the KSC Hot Pics gallery.
http://mediaarchive.ksc.nasa.gov/search.cfm?cat=4
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el_nino - 6/12/2007 4:58 PM
AWESOME photo. Got a high res shot of that around anywhere?
Thanks! E-mail or PM me about the high-res...
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from nasa.gov
http://www.nasa.gov/images/content/122586main_ECO_charts1.JPG
http://www.nasa.gov/images/content/122588main_ECO_charts3.JPG
http://www.nasa.gov/images/content/122589main_ECO_charts4.JPG
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NET 7pm.
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Briefing NET 7:00 PM EST.
EDIT: You got me, Chris. :laugh:
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Briefers are on the way over now should start soon.
Mark Kirkman
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No launch attempt tomorrow.
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erioladastra - 6/12/2007 11:51 PM
No launch attempt tomorrow.
Tanking Test instead, right? (EDIT, doesn't look like it).
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Now they are telling the folks at the Press Site that the briefing will be no earlier than 7:30 pm EST.
P.S.
Briefers probably diverted to the LCC cafeteria before heading across the street to the Press Site... :)
Mark Kirkman
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MMT tomorrow to decide on new launch date. NET Saturday, may be later.
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Chris Bergin - 6/12/2007 4:55 PM
MMT tomorrow to decide on new launch date. NET Saturday, may be later.
If tomorrow is a definite no-go, would they have time to top-off cyro before a hypothetical Saturday attempt?
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Briefing is now listed as 7:30 pm EST (No NET)
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Lee Jay - 7/12/2007 12:58 AM
Chris Bergin - 6/12/2007 4:55 PM
MMT tomorrow to decide on new launch date. NET Saturday, may be later.
If tomorrow is a definite no-go, would they have time to top-off cyro before a hypothetical Saturday attempt?
Depends on whether they have decided to perform a tanking test or not. They can't perform a tanking test if the RSS is around the vehicle.
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Lee Jay - 7/12/2007 12:58 AMIf tomorrow is a definite no-go, would they have time to top-off cyro before a hypothetical Saturday attempt?
AFAIK they have 3 consecutive attempts before having to refill the APUs...
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GioFX - 7/12/2007 1:13 AM
Lee Jay - 7/12/2007 12:58 AMIf tomorrow is a definite no-go, would they have time to top-off cyro before a hypothetical Saturday attempt?
AFAIK they have 3 consecutive attempts before having to refill the APUs...
Not the APUs(Auxillary Power Units)! The Power Reactant Storage and Distribution(PRSD) system storage spheres beneath the payload bay.
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DaveS - 7/12/2007 1:14 AMNot the APUs(Auxillary Power Units)! The Power Reactant Storage and Distribution(PRSD) system storage spheres beneath the payload bay.
Yep sorry, i misunderstood the question!
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What is the percent of KSC weather prohibiting the launch Saturday?
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Justin Wheat - 7/12/2007 1:17 AM
What is the percent of KSC weather prohibiting the launch Saturday?
40% according to the L-1 day Wx forecast. And there's a dedicated launch weather thread with all this info already!
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Appears that they are going to rollback the RSS. So that'll rule out a tanking test tomorrow.
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DaveS - 6/12/2007 6:12 PM
Lee Jay - 7/12/2007 12:58 AM
Chris Bergin - 6/12/2007 4:55 PM
MMT tomorrow to decide on new launch date. NET Saturday, may be later.
If tomorrow is a definite no-go, would they have time to top-off cyro before a hypothetical Saturday attempt?
Depends on whether they have decided to perform a tanking test or not. They can't perform a tanking test if the RSS is around the vehicle.
Theoretically, couldn't they do what they did with the second STS-114 attempt tomorrow, tank and see how the sensors perform and then if they work, proceed with the rest of the countdown. I remember some folks calling STS-114's second attempt sort of a tanking test embedded into a real launch count. ;)
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shuttlefan - 7/12/2007 1:21 AM
Theoretically, couldn't they do what they did with the second STS-114 attempt tomorrow, tank and see how the sensors perform and then if they work, proceed with the rest of the countdown. I remember some folks calling STS-114's second attempt sort of a tanking test embedded into a real launch count. ;)
It wasn't a tanking test, it was a real launch countdown from the get go. Embedding a tanking test into the launch countdown was just one of the many ideas thrown around at the time.
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I bet these guys will be shattered (loooooong day).
48 hour scrub turnaround confirmed. NET Saturday.
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Leroy Cain now talking about the tanking test option "when they are ready."
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"What we did, fundamentally, was to keep all our options in front of us." "We need some more time."
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They are keeping the option of flying on Saturday open, too...
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psloss - 7/12/2007 12:43 AM
"What we did, fundamentally, was to keep all our options in front of us." "We need some more time."
Given what the ET guys were saying earlier, Leroy's made totally the right call.
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Doug Lyons recapping the events of the day; as already noted here, they continued tanking even after the SIM test failure early in fast fill.
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They initially postured for a 24-hour turnaround and are now transitioning into the 48-hour turnaround procedures. They are intending on topping the LH2 side of PRSD.
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Just completed pad safing, as Doug Lyons said.
40% chance of KSC weather prohibiting launch on Saturday.
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Leroy Cain saying that with the signature seen today, the path between the point sensor box and the MDM has been "exonerated." Current thinking (as reported) somewhere between the PSB and tank. Doesn't have the signature of a sensor failure.
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As noted in the opening, they are also looking at operational (in-flight) workaround procedures for dealing with the situation seen today with the new voltage measurements.
The haven't used the voltage measurements during ascent, but have been thinking about it. Now the flight control team is trying to see if and how they could use that.
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They are "taking the next step" in utilizing the weight of the data collected since the STS-114 campaign and the new data.
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Will be interesting to see if they can go to a LCC of 2/4 ECOs. NASA Safety would need to approve this, I believe?
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Good question from Bill Harwood to Leroy Cain -- in the current plan, they are not going to go into the aft. However, that is only where they are tonight.
(And "breaking the flight configuration" wouldn't support the option to attempt on Saturday.)
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No plans to go into the aft, yet (of course, if they did it would be a three/four delay, so a NET Saturday meant not going into the aft anyway). Might decide to at tomorrow's MMT.
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There's ex-astro Sam Gemar (w/ HDNet) again...
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No one's asked about ECO#1 yet.
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Craig Covault asking a configuration management question -- does OV-104 or the tank have a different config? Leroy Cain said that OV-105 and OV-103 (on STS-118 and STS-120, respectively) have already flown in the config that OV-104 is in (which flew a "hybrid" config on STS-117). Can't rule out the possibility that wiring config is a contributing cause.
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Interesting...Doug Lyons says that there's a study on doing a LH2 ECO sensor R&R in the winter months in the vertical while mated. (Maybe at the pad.)
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Briefing over. First wild guess on tomorrow's briefing time is 5 pm Eastern.
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Ok, we'll keep this thread active through tomorrow as they work the evaluations.
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Based on what Leroy said, I would be surprised if 48 hours is doable. If the Program accepts the 2 or 4 (or some other ratio) for failed wet sensors, it will still take a little time (presumably days, but maybe even weeks or more) to get the Flight Control Team and the Crew on the same page as to what the ascent procedures would be for the numerous cases in which this would be a factor (and there are a lot of cases to examine, mostly abort related).
While there has been some simulation on this for the ascent flight control team it is no trivial thing to get the procedures formalized and documented to the level you want before you go fly.
I may be wrong but at this point the ascent flight procedures with the ECO mod are not nearly mature enough.
I can see them getting there (i.e. to 2 of 4 decision) I am just saying that I dont believe they can do that in the 48 hour time frame!!!!
Mark Kirkman
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Gary - 6/12/2007 7:24 PM
mkirk - 7/12/2007 1:20 AM
While there has been some simulation on this for the ascent flight control team it is no trivial thing to get the procedures formalized and documented to the level you want before you go fly.
I'd also assume this is something you would want to throw at the crew and misson control in the sims a few times so everyone knows the signature of a ECO sensor issue and a (nearly) empty tank.
It does sound like its an option that's under evaulation but hasn't actually borne fruit yet.
I honestly don't know if this was presented in any of the Ascent Integrated Sims for 118 or subsequent training flows. Even if it did get worked in those I still think it would take the Program past Saturday to get everyone onboard with the new philosophy and to have the procedures and flight rules properly documented. (reference my previous post)
Mark Kirkman
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mkirk - 6/12/2007 8:27 PM
I honestly don't know if this was presented in any of the Ascent Integrated sims for 118 or subsequent training flows. Even if it did get worked in those I still think it would take the program past Saturday to get everyone onboard with the new philosophy and to have the procedures and flight rules properly documented. (reference my previous post)
Do you think it would be possible to get that through an organization the size of the SSP in a week's time? (i.e., before the end of the December window)
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Looks like a set of Xenon lights are on... Wondering when RSS moves to MATE position, if anyone knows.. I've been away for most of the briefing..
[small]Also, if this isn't supposed to go here yet, please delete[/small]
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psloss - 6/12/2007 7:29 PM
mkirk - 6/12/2007 8:27 PM
I honestly don't know if this was presented in any of the Ascent Integrated sims for 118 or subsequent training flows. Even if it did get worked in those I still think it would take the program past Saturday to get everyone onboard with the new philosophy and to have the procedures and flight rules properly documented. (reference my previous post)
Do you think it would be possible to get that through an organization the size of the SSP in a week's time? (i.e., before the end of the December window)
I would hate to speculate much further than what I already have. The team is great at doing the seemingly impossible, and right now the leader ship is outstanding...so we will just have to wait and see.
My main motive for the previous couple of posts was to point out the enormity of what has to take place. Going with a flight rationale of 2 of 4 ( or something similar) based on the real time use of the new instrumentation is not as simple as it may have sounded to some of the listeners to the briefing.
Mark Kirkman
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Thanks Mark and everyone else. Your insights and answers make this all so much more interesting for armchair spectators like myself.
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"I would hate to speculate much further than what I already have. The team is great at doing the seemingly impossible, and right now the leader ship is outstanding...so we will just have to wait and see. "
It is no different than pulling together the solar array repair EVA on 10A. We can do it. It won't be easy but it could be done.
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erioladastra - 6/12/2007 8:06 PM
"I would hate to speculate much further than what I already have. The team is great at doing the seemingly impossible, and right now the leader ship is outstanding...so we will just have to wait and see. "
It is no different than pulling together the solar array repair EVA on 10A. We can do it. It won't be easy but it could be done.
Preaching to the converted on a pro-NASA, pro-Shuttle site like this. :cool:
Awesome coverage here again.
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Ford Mustang - 6/12/2007 7:33 PM
Looks like a set of Xenon lights are on... Wondering when RSS moves to MATE position, if anyone knows.. I've been away for most of the briefing...
No specific time specified. I imagine they'll start whenever everything is finally ready for the rotation to begin, and only those on the pad will know that.
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Just so everyone knows, there is a live streaming view of the pad at this link. It is Camera 060, and it should be a very interesting view for the RSS retract later on. Xenons are on too, so its very easy to see everything.
rtsp://163.205.10.22:8080/encoder/cif.rm
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Michael22090 - 6/12/2007 9:36 PM
Just so everyone knows, there is a live streaming view of the pad at this link. It is Camera 060, and it should be a very interesting view for the RSS retract later on. Xenons are on too, so its very easy to see everything.
rtsp://163.205.10.22:8080/encoder/cif.rm
Thanks for that link. If they rotate the RSS while I'm watching, then I'll record it via cam record, as I can't think of any other way to record it.. All my other options are out! :(
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psloss - 6/12/2007 6:13 PM
Craig Covault asking a configuration management question -- does OV-104 or the tank have a different config? Leroy Cain said that OV-105 and OV-103 (on STS-118 and STS-120, respectively) have already flown in the config that OV-104 is in (which flew a "hybrid" config on STS-117). Can't rule out the possibility that wiring config is a contributing cause.
You have sensors that are known to work when tested individually, a point sensor box that works when tested individually, how can this be anything but some sort of signal path problem?
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Read through the thread, great catch up and really great work with the news, even when some other sites were saying different things, though it's the norm for this site to be on top of the game. Great to have these threads live, but also as a catch up for those of us who were at work with no net access. Thanks again.
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Andy L - 6/12/2007 10:05 PM
Read through the thread, great catch up and really great work with the news, even when some other sites were saying different things, though it's the norm for this site to be on top of the game. Great to have these threads live, but also as a catch up for those of us who were at work with no net access. Thanks again.
Well said.
Just shows how it all has to come together for launch, as this was a very smooth processing flow until this happened. Shows how well they did to get three launches off on the first attempt prior to this.
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RSS is moving...
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mkirk - 6/12/2007 7:27 PM
I honestly don't know if this was presented in any of the Ascent Integrated Sims for 118 or subsequent training flows. Even if it did get worked in those I still think it would take the Program past Saturday to get everyone onboard with the new philosophy and to have the procedures and flight rules properly documented. (reference my previous post)
Mark Kirkman
The Booster console team apparently already has prepared a fairly mature draft of the FR's for handling ECO votes when they are known to be 'fail wet' (based on the new instrumentation). They're probably reviewing all sim and analysis experience as we type, and will prepare their pitch tomorrow morning. If they can demonstrate that their decision tree or flow chart representation, needed for fast look-up during time-critical ascent, actually correctly responds to all possible permutations, they ought to be able to get it approved at the MMT.
I don't think the crew is deeply involved -- these FR's are all for MCC calls, and the crew just has to be aware of the range of keyboard inputs or switch throws they may be called upon to make.
I served as Neil Hutchison's panel secretary in 1979-1980 when he kicked off the very FIRST 'Shuttle Ascent Flight rules' panel meetings, and I documented the rationales, reasoning, and disagreements for the record and for wider distribution. Then I was on Neil's 'Silver Team' -- the very first shuttle Ascent Shift -- that made it all work on April 12, 1981, at the OMS/RCS Propulsion console. For all our prep, what a bold leap into the unknown THAT morning was.
And no, NONE of us was watching TV of the liftoff. We had our data screens to concentrate on.
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Correct me if I am wrong, but from what I have read the ECOs really only get "used" in a non normal ascent. Like an engine shutting down, which would throw off the fuel consumption figures, or a leak of some sort.
So really the only times it would have been used would have been STS -51F (the Challenger ATO) and the Columbia Chandra mission. If memory serves the ECOs did their job on that day, with engine 3 leaking hydrogen all the way up, the engines used up the oxygen and the ECOs called for an very slight early MECO.
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I am really glad they delayed till Saturday. I have three finals tomorrow, no way I could see it.
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Sorry to say this, but weakening the ECO fuel gauges flight rules is not what these rules are for. I see here a clear push to get the shuttle off the pad in December. The proper way to do it would be to stand down and check the complete wiring from ECO to point sensor box, even if this involves opening the engine compartment.
Reading the front page article of nasaspaceflight.com, also ECO #1 looks buggy (sensing briefly WET, when the tank is empty), so there seems to be a generic problem. This is a safety issue and I cannot believe that people are even thinking launching as-is, when 3 of 4 sensors are behaving strangely.
Sad to see again, that schedule goes over safety.
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avollhar - 7/12/2007 3:41 AM
...when 3 of 4 sensors are behaving strangely.
Well, one works fine, so I say GO! No, seriously, you are right - it is a bit of a mystery to me as well, why NASA and people around here are again in a GO fever. Of course there is schedule pressure, but I thought that schedule should not have any influence on critical safety decisions any more.
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mr.columbus - 7/12/2007 9:48 AM
No, seriously, you are right - it is a bit of a mystery to me as well, why NASA and people around here are again in a GO fever. Of course there is schedule pressure, but I thought that schedule should not have any influence on critical safety decisions any more.
I agree. If an engine running dry will behave badly - as many people here have indicated - and this is the reason for the ECO sensors being there in the first place, they should work.
Are the ECO sensors the last line of defense or are there other systems?
When into the flight start the computers accepting data from the sensors? I would think only well into the flight, because a dry signal at T+60 seconds would clearly be wrong and a resulting shutdown probably as worse as a dry running engine.
Analyst
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Analyst - 7/12/2007 10:00 AM
When into the flight start the computers accepting data from the sensors? I would think only well into the flight, because a dry signal at T+60 seconds would clearly be wrong and a resulting shutdown probably as worse as a dry running engine.
Analyst
They're armed at a specific velocity which is different for the various abort modes. Usually that velocity isn't reached until about 8 minutes into the ascent.
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Analyst - 7/12/2007 4:00 AM
Are the ECO sensors the last line of defense or are there other systems?
When into the flight start the computers accepting data from the sensors? I would think only well into the flight, because a dry signal at T+60 seconds would clearly be wrong and a resulting shutdown probably as worse as a dry running engine.
Mark Kirkman (mkirk) wrote a good overview of the ECOs, which I think has already been linked in this thread; but here it is again:
http://www.interspacenews.com/interspace%20News%20Web%202/sections/In%20focus/ECO%20Sensors.htm
Excerpt:
During a normal launch the shuttles computers are monitoring the orbiters velocity for the shutdown cue. For STS-114 the desired MECO velocity target is 25,819 feet per second (this is equivalent to 17,603 miles per hour) at the point of zero engine thrust. The shutdown process takes about six seconds during which time the shuttle is still accelerating. So in order to achieve a zero thrust target of 25,819 fps, the actual MECO command will be sent at a velocity cue of 25,800 feet per second. For normal ascents the engine cutoff sensors have no role in shutting down the main engines. Velocity is the only shutdown cue. In fact the GPCs will not even accept a shutdown command from the ECO sensors unless they have been armed.
The command to arm the ECO sensors is issued only if one of the following conditions applies:
- Two engines have failed, or
- A flight specific arming mass has been reached. This mass is usually the total mass of propellant remaining in the external tank that provides the shuttle the ability to perform a Transoceanic Abort Landing (TAL) should the sensors issue a cutoff command immediately upon arming. For STS-114 this mass is about 32000 pounds of propellant remaining.
L2 plug: if you review the STS-93 ascent video, you can hear that event called out on one of the booster console's loops.
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I would suggest you read Bill Harwood's current report:
http://www.cbsnews.com/network/news/space/current.html
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When can we expect RSS retract?
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avollhar - 7/12/2007 8:41 AM
Sorry to say this, but weakening the ECO fuel gauges flight rules is not what these rules are for. I see here a clear push to get the shuttle off the pad in December. The proper way to do it would be to stand down and check the complete wiring from ECO to point sensor box, even if this involves opening the engine compartment.
Reading the front page article of nasaspaceflight.com, also ECO #1 looks buggy (sensing briefly WET, when the tank is empty), so there seems to be a generic problem. This is a safety issue and I cannot believe that people are even thinking launching as-is, when 3 of 4 sensors are behaving strangely.
Sad to see again, that schedule goes over safety.
I couldn't agree more. I was staggered to see Leroy Cain in "launch in December at all costs" mode. He is deferring to the current safety risk assessment but there is obviously a huge management attempt to ease flight rules that already have been relaxed once before.
IMO there is a clear indication of a wiring fault with one of the sensors that failed, which was stuck on wet, that reset to a dry indication some hours after detanking. If that is a fault due to cryogenic cooling causing an open circuit in wiring or connectors, then it should be fixed before flight unless it is the only faulty sensor.
The whole sensor system in the ET seems to be troublesome and pretending to ignore this is not the way to operate flight critical hardware.
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montmein69 - 7/12/2007 11:09 AM
If 2 of 4 are failing .... how do you know that the other 2 are right ?
What is the "new instrumentation" procedure ? (which way to get the correct data ?)
What they said at the briefing was that the new instrumentation allows them to tell whether a sensor has failed in the WET state or whether it is reporting a normal WET condition. Before the new instrumentation was fitted, they could test this before launch by simulating a DRY condition but not after T-0.
Without the new instrumentation, they had no way of telling if any sensors fail after they've finished the pre-flight checks, so they need some redundancy to make sure that the cut off can will happen in the event of LH2 exhaustion. Now, with the new instrumentation, they can tell if any sensors subsequently fail.
They might use this mechanism to permit a launch with two failed sensors on the basis that they would know if a third fails. If the third does fail, they've lost the safety ECO function but could choose to do a manual shutdown as a precaution to protect the vehicle and crew. The cost would be that they would then have an abort condition which would mean a TAL, AOA or ATO, none of which would get Columbus attached to the station and two of which would create delay in getting Atlantis back to KSC (considerably so in the case of a TAL!).
They can trade crew safety against the risk to the programme (due to an abort) but the cost is there in one or the other. Those are no doubt the issues they will be working through today.
Mark
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nice day at the pad
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Very Nice!
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ETEE - 7/12/2007 7:23 AM
I couldn't agree more. I was staggered to see Leroy Cain in "launch in December at all costs" mode.
I couldn't agree less with this interpretation of what Leroy Cain said last night. The way I parsed what he said last night was that they are approaching the current situation making minimum assumptions, and they have made zero decisions other than passing on an attempt today.
I don't understand the blind jumping to the conclusion that IF the program deliberates whether they can proceed that somehow implies that they will proceed.
Evaluating one's options doesn't seem rash to me, because there's no commitment, no decision.
What is the basis for the assumption that they can't fly in December? If you make that assumption, what is it based on?
If you are questioning their philosophy of considering all their options, what is the basis for that?
ETEE - 7/12/2007 7:23 AM
IMO there is a clear indication of a wiring fault with one of the sensors that failed, which was stuck on wet, that reset to a dry indication some hours after detanking. If that is a fault due to cryogenic cooling causing an open circuit in wiring or connectors, then it should be fixed before flight unless it is the only faulty sensor.
What makes the indication "clear?" Just because you can detect an anomaly, does it follow that you know the cause of the anomaly?
ETEE - 7/12/2007 7:23 AM
The whole sensor system in the ET seems to be troublesome and pretending to ignore this is not the way to operate flight critical hardware.
What's the basis for this? You realize that a significant portion of this particular sensor circuit is in the orbiter, right?
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Couldn't agree more, Philip. This isn't "go fever".
Nobody but the MMT and people working on this are qualified to say what is OK and what is not.
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Gary - 7/12/2007 1:15 PM
montmein69 - 7/12/2007 11:09 AM
Has ESA any say in the matter ? (two astronauts in the crew and Columbus in the bay)
Any say over what? ESA can't force NASA to launch.
I think montmein69 meant if ESA could refuse to launch with their astronauts and their cargo if they are not comfortable with the safety situation.
My opinion is that ESA do not know the details of the inner workings of the shuttle system. NASA and USA do, and when ESA originally decided to lift their cargo and astronauts to orbit on the shuttle, they entrusted that cargo and those astronauts to the engineers and managers of the shuttle program.
I see no reason why ESA should not trust any decision made by shuttle managers and engineers, whether it is to fly as is or to roll back and fix the problem.
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Gary - 7/12/2007 1:30 PM
Even with two failed sensors you are on a fine line. If the other two fail and show DRY you are into engine shutdown and a very bad day.
The sensors aren't armed until they can make a TAL site [as I see you've spotted from your edit]. Also, they seem to have some confidence that the failures they're seeing are failures to the WET state due to an open circuit somewhere. But, I expect they're weighing up the likelihood of other failures in the risk calculations.
It seems too risky to me to go with two failed sensors but NASA have a lot more information on which to base a decision than I do. I'm sure if they do make a launch attempt they will do it having considered all the possible scenarios. If I had to place a bet, I'd bet against them launching on Saturday if they still have two failed sensors but that's just my opinion.
M.
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Gary - 7/12/2007 8:30 AM
AOA is the worst condition you can be in - You put the crew into a full re-entry regime without the benefit of the FD2 OBSS scans.
What's the difference between that and a TAL? The entry heating in some types of TAL aborts can be more severe than a normal entry.
Gary - 7/12/2007 8:30 AM
Absolutely. I firmly believe ANY abort will signal an end to the shuttle there and then.
EDIT TO ADD: Shuttle Q & A part 4 states the ECO sensors aren't armed until TAL regime of flight so that means RTLS is an open option even with faulty ECO sensors.
I wouldn't jump to that conclusion about an abort -- for example, if you want to play the press/political angle, the OUTCOME of the abort would be important. (As well as the cause.)
I don't understand the linkage between the ECO sensors and RTLS. If you cut all three engines that early in ascent you might go to OPS 6, but it's a contingency abort.
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psloss - 7/12/2007 2:12 PM
What is the basis for the assumption that they can't fly in December? If you make that assumption, what is it based on?
I pick one quote to illustrate the "problem". People (including me sometimes) jump to conclusions pretty fast, see anologies even if there aren't any and question things. This thinking is not bad in general. But with the limited information we have, conclusion are often simply wrong. There is the moderate majority of people and two more "extreme" camps:
- Some cry "rollback" whenever a switch is in the wrong positon,
- others want to launch even if the engines don't ignite.
The first group always sees "go fever", the second group is surrounded by risk adverse people.
I for myself hear the word "rollback" quite to often, which puts me into the direction of the second group, but still quite in the middle I believe :) Of course a rollback is always possible, but this does not mean it will happen. A few weeks ago Chris started a thread about the RCS valve problem with "potentially rollback". While this has been true, my thought was "pretty hard words" for a problem not well understood then. A rollback is always *possible*. Doesn't mean there will be one.
Hope this does not confuse things even more. :)
Analyst
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Gary> I think the idea is that you would not have the sensors armed but only monitored - so if a minute after launch they failed dry you know (from commonsense analysis, because there's no conceivable performance dispersion that could cause the tank to be empty at that point) that they have failed and that you need to provide low-propellant protection for the SSMEs via an alternate process; that would be to declare an intact abort mode which allowed for an early enough MECO to cover the maximum credible performance loss.
So the sensors indicating DRY would not result in a MECO in a zone where no intact abort was available - they would just be ignored and the interpretation as a "very bad day" is incorrect.
However, I think you're right to say that an intact abort would be a serious event for the shuttle programme (downtime to revisit ECO sensor issues) and a big logistics issue for the ISS. I personally don't think ending the shuttle programme early would be a proportionate response to a single systems failure that resulted in an abort. (ISTM that the shuttle *systems* (logic, electronics, computers, machinery) have not been safety issues, and were not a factor in either of the two accidents - they have been caused by issues of materials, construction and management)
edit: Ah, others got there first.
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Andrewwski - 7/12/2007 8:30 AM
Couldn't agree more, Philip. This isn't "go fever".
Nobody but the MMT and people working on this are qualified to say what is OK and what is not.
For the most part; I'm sure there are other rocket scientists who would be qualified. What I've observed over the years is very little public speculation from that community in these situations.
For us outsiders, here's the thing about whether it's go fever or not: we won't be able to determine that until AFTER the fact unless someone goes public in an unprecedented way.
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Analyst - 7/12/2007 1:46 PM
A few weeks ago Chris started a thread about the RCS valve problem with "potentially rollback". While this has been true, my thought was "pretty hard words" for a problem not well understood then. A rollback is always *possible*. Doesn't mean there will be one.
Analyst
So you don't want us to report the *facts* about the options open to managers evaluating status? Fact of the matter is, had the valve been the failure point, then yes, rollback would have been an option as the valve could not of been R&Red at the pad. The other option was to fly as-is with waivers, which we also reported. Thankfully, as written, we followed the process (do we hold back the information until after the event??) the issue was being caused downstream and was corrected.
We're not going to sugarcoat facts, and we sure as hell aren't going to be reporting the style of "can't tell you yet....we'll tell you more after the event". You're on the wrong site if so, as we report live status, as we all follow the process.
We'll be doing that today, from the options of launching tomorrow, delaying, or rollback. Whatever the MMT is evaluating, we'll be reporting it, regardless if it's "harsh words" or not. Facts are facts.
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Chris Bergin - 7/12/2007 9:24 AM
Analyst - 7/12/2007 1:46 PM
A few weeks ago Chris started a thread about the RCS valve problem with "potentially rollback". While this has been true, my thought was "pretty hard words" for a problem not well understood then. A rollback is always *possible*. Doesn't mean there will be one.
Analyst
So you don't want us to report the *facts* about the options open to managers evaluating status? Fact of the matter is, had the valve been the failure point, then yes, rollback would have been the call as the valve could not of been R&Red at the pad. Thankfully, as written, as we followed the process (do we hold back the information until after the event??) the issue was being caused downstream and was corrected.
We're not going to sugarcoat facts, and we sure as hell aren't going to be reporting the style of "can't tell you yet....we'll tell you more after the event". You're on the wrong site if so, as we report live status, as we all follow the process.
We'll be doing that today, from the options of launching tomorrow, delaying, or rollback. Whatever the MMT is evaluating, we'll be reporting it, regardless if it's "harsh words" or not. Facts are facts.
As it should be, Chris.
Well said.
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Chris Bergin - 7/12/2007 8:24 AM
Analyst - 7/12/2007 1:46 PM
A few weeks ago Chris started a thread about the RCS valve problem with "potentially rollback". While this has been true, my thought was "pretty hard words" for a problem not well understood then. A rollback is always *possible*. Doesn't mean there will be one.
Analyst
So you don't want us to report the *facts* about the options open to managers evaluating status? Fact of the matter is, had the valve been the failure point, then yes, rollback would have been the call as the valve could not of been R&Red at the pad. Thankfully, as written, as we followed the process (do we hold back the information until after the event??) the issue was being caused downstream and was corrected.
We're not going to sugarcoat facts, and we sure as hell aren't going to be reporting the style of "can't tell you yet....we'll tell you more after the event". You're on the wrong site if so, as we report live status, as we all follow the process.
We'll be doing that today, from the options of launching tomorrow, delaying, or rollback. Whatever the MMT is evaluating, we'll be reporting it, regardless if it's "harsh words" or not. Facts are facts.
I'm totally with you Chris!! This site is wonderful on reporting all the possibilities firsthand. :)
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psloss - 7/12/2007 11:06 AM
L2 plug: if you review the STS-93 ascent video, you can hear that event called out on one of the booster console's loops.
It's about a 100mb video, but I'll cut some of the end and publish it into this thread.
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Ok, cut it down and reduced the quality to make it fit as an attachment in this thread.
STS-93 (very eventful). Full video (100mb) on L2. There's another clip at the start here (second post): http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=9944&start=1
See below for attachment to download the ECO element of the launch:
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mark147 - 7/12/2007 7:01 AM
The cost would be that they would then have an abort condition which would mean a TAL, AOA or ATO, none of which would get Columbus attached to the station and two of which would create delay in getting Atlantis back to KSC (considerably so in the case of a TAL!).
They can trade crew safety against the risk to the programme (due to an abort) but the cost is there in one or the other. Those are no doubt the issues they will be working through today.
Mark
Mark, I seem to recall that landing with undeployed payload was 'possible but not recommended' due to much heavier than nominal touchdown forces, that in the old days would have called for a total orbiter structural inspection and overhaul -- and possibly just writing it off as 'probably damaged and non-verifiable'. An intact orbit might have been the last mission for that particular orbiter, even if the landing was made perfectly.
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Mr Oberg. What in your experience do you think NASA will decide to do?
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rfoshaug - 7/12/2007 7:32 AM
Gary - 7/12/2007 1:15 PM
montmein69 - 7/12/2007 11:09 AM
Has ESA any say in the matter ? (two astronauts in the crew and Columbus in the bay)
Any say over what? ESA can't force NASA to launch.
I think montmein69 meant if ESA could refuse to launch with their astronauts and their cargo if they are not comfortable with the safety situation.
That was exactly my mind in case the safety rules are modified.
My opinion is that ESA do not know the details of the inner workings of the shuttle system. NASA and USA do, and when ESA originally decided to lift their cargo and astronauts to orbit on the shuttle, they entrusted that cargo and those astronauts to the engineers and managers of the shuttle program.
Yes, but the deal was made with the "3 of 4" .. and maybe it could be changed to launch in the december window.
I see no reason why ESA should not trust any decision made by shuttle managers and engineers, whether it is to fly as is or to roll back and fix the problem.
My question was not to discuss about NASA skills but only "Would ESA be consulted or not ?" before the decision is taken to launch as is.
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ESA is a customer as well as a partner. They are always consulted. As for a rush to launch, not true!! If there was a rush to launch, we would be trying to fly today. By not going into the shuttle or ET, we keep all options open. By topping off the fuel, we keep all options open. Remember, they call it a launch "window" because they keep all options open.
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Chris Bergin - 7/12/2007 9:28 AM
Ok, cut it down and reduced the quality to make it fit as an attachment in this thread.
STS-93 (very eventful). Full video (100mb) on L2. There's another clip at the start here (second post): http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=9944&start=1
See below for attachment to download the ECO element of the launch:
Thanks! That's awesome!
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When NASA are going to make the decision if they can fly with two faulty sensors?
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Yegor - 7/12/2007 4:53 PM
When NASA are going to make the decision if they can fly with two faulty sensors?
MMT meet at 2pm Eastern (two hours time). Engineering data is still being collected, though I'm close to getting a new article on site with the latest. I'll have that up as the MMT meets and then update as that proceeds (will be a long MMT).
Also remember, "two faulty sensors" is not exactly the case.
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Thank you very much for a quick reply!
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I sure hope it liftoffs tommorrow!!!
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I think the decision will rest on how mature the Booster console's decision charts
are for all permutations of sensor failure modes. My suspicion is that their charts
were pretty mature yesterday, and in the past 24 hrs have fully ripened.
If the MMT isn't convinced, they can give them a few more days and more test resources.
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I would assume that if nasa is going to attempt a launch tomorrow the RSS would be retracted sometime this evening. Any more news?
I have been away for most of the morning.
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If this gets delayed any further, will the Atlas scheduled for 10 December wait for the Shuttle, or will the Shuttle be expected to wait?
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They will work with ULA if it gets to that point. The way i understand it.
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MMT delayed. There's a huge effort going on with this. Still 50/50 on flying tomorrow.
Incidently, there's bigger news brewing...so it's going to be a long night folks!
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Chris Bergin - 7/12/2007 1:50 PM
MMT delayed. There's a huge effort going on with this. Still 50/50 on flying tomorrow.
Incidently, there's bigger news brewing...so it's going to be a long night folks!
Now you've really got us curious, Chris.
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Do tell Chris! You can't leave us hanging like that!
Now where'd I put my credit card for L2...
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Chris Bergin - 7/12/2007 1:50 PM
MMT delayed. There's a huge effort going on with this. Still 50/50 on flying tomorrow.
Incidently, there's bigger news brewing...so it's going to be a long night folks!
Uh-oh. This doesn't sound good...
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iloco - 7/12/2007 2:08 PM
Do tell Chris! You can't leave us hanging like that!
Now where'd I put my credit card for L2...
I'm sure he'd tell you what he knew.. I'm not sure if he has more information than that... but if he had things he could release, he would have.
This doesn't rule out anything for tomorrow (as of this post), just means they will have a very long day today if they are working towards a launch tomorrow. Feel free to correct me, if something is wrong, but I'm just going off of what I see.
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iloco - 7/12/2007 7:08 PM
Do tell Chris! You can't leave us hanging like that!
Now where'd I put my credit card for L2...
L2's great :) but we'll be running this as a news article, so you'll only need to wait until about 5pm Eastern. I'm unable to say anymore (even on L2, by the way) until then, as I don't have all the info yet. When I do, it's straight to article. It will be 'good' news.
Back to the ECOs....
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Chris, you just guaranteed that start about 4:50 EST, your servers are going to see a load that exceeds that of launch day!
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Chris you tease, you are certainly a good showman.
I look forward to the article.
Any hints? Is it STS related?
Edit: I was going to post a guess but I think its better to just wait and not stoke the flames.
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MMT still delayed?
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dember - 7/12/2007 8:05 PM
MMT still delayed?
Was due to start at 3pm (nowish). Waiting for word.
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Chris Bergin - 7/12/2007 7:50 PM
MMT delayed. There's a huge effort going on with this. Still 50/50 on flying tomorrow.
Incidently, there's bigger news brewing...so it's going to be a long night folks!
Some idea when the briefing will take time?
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Article, quote heavy from L2 (you don't need to hear from me, going on about how ECOs work, so just threw in quotes....)
http://www.nasaspaceflight.com/content/?cid=5303
Will be updated as we go through the MMT. Likely to be several hours long.
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"ET Project and JSC Engineering are believed to be against any launch attempt on Saturday"
Definitely not going to be a 5-minute we-all-agree-lets-fly kind of meeting.
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JSC Engineering would dissent their own existance if you asked them.
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Bruce - 7/12/2007 3:24 PM
"ET Project and JSC Engineering are believed to be against any launch attempt on Saturday"
Definitely not going to be a 5-minute we-all-agree-lets-fly kind of meeting.
Don't forget..JSC Engineering was against Endeavor coming back with that "Huge" gouge in her belly. LOL.
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NASA_Langley_spammer - 7/12/2007 3:25 PM
JSC Engineering would dissent their own existance if you asked them.
Both funny and disturbing.
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Nobody ever said they're not listening to them.
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Are they for or against?
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JSC and ET eng are speaking against at this moment , assumption is they want more time to analyze before taking any risks
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If they scrub tomorrow is there a good chance that there will be a rollback?
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dember - 7/12/2007 1:07 PM If they scrub tomorrow is there a good chance that there will be a rollback?
Depends on what caused the scrub (besides the ECO problem). And Atlantis still has 6 more days to get off the ground (assuming ULA will be flexible with the Atlas V launch).
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If they scrub tomorrow, chances are they will rollback for repair
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Chris Bergin - 7/12/2007 1:50 PM
Incidently, there's bigger news brewing...so it's going to be a long night folks!
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=11084&posts=1#M220993
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Chris Bergin - 7/12/2007 8:51 PM
Chris Bergin - 7/12/2007 1:50 PM
Incidently, there's bigger news brewing...so it's going to be a long night folks!
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=11084&posts=1#M220993
2015! - no need to rush STS-122 then ;)
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Don't you go trying to make it related to this thread ;)
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NET 6:30pm for the presser.
We're thinking they'll say they need more time for evaluations....
By the way, they've found a crack in a feedline bracket :(
http://www.nasaspaceflight.com/content/?cid=5303
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Make that NET 7pm
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Chris Bergin - 7/12/2007 4:46 PM
By the way, they've found a crack in a feedline bracket :(
Official word: There is no 8-inch crack. There were "scuff marks", well within limits, noticed during a routine inspection. No other teams are being sent out and the issue never reached the MMT as it was considered too minor for mention.
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Post MMT Meeting now NET 7:30 PM EST
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^ great, thanks Bob!
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zentripcity - 7/12/2007 4:14 PM If they scrub tomorrow, chances are they will rollback for repair
What are you basing that on?
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ntschke - 7/12/2007 5:57 PM
zentripcity - 7/12/2007 4:14 PM If they scrub tomorrow, chances are they will rollback for repair
What are you basing that on?
He's noting his opinion, is how I read it.
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James Lowe1 - 7/12/2007 6:59 PM ntschke - 7/12/2007 5:57 PM zentripcity - 7/12/2007 4:14 PM If they scrub tomorrow, chances are they will rollback for repair
What are you basing that on?
He's noting his opinion, is how I read it.
Thanks James, just wondering if there was some talk about that in the later part of today's meetings and/or some other source of info.
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Seems NET 8:00 PM EST, as they're still running videos? Anyone confirm?
UPDATE: Confirmed via NASA TV slate.
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Not showing anything on NASA TV. Your guess is as good as mine.
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Ford Mustang - 7/12/2007 6:30 PM
Seems NET 8:00 PM EST, as they're still running videos? Anyone confirm?
Yes, and actually it will probably be later than that even.
Mark Kirkman
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If we have any chance of resuming the count for a launch Sat.. we are at 11 hrs and holding.. so the hold would need to be release in what 3 hour max??
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Based on the fact that they're going to start this press conference late...is there any indication from other sources or via wbecams of any activity that would indicate preps for a launch attempt tomorrow? Such as RSS rollback, lighting or other tell-tale signs?
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From my opinion, I think they will not try for the launch tomorrow and evaluate their options a little longer.
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Chris probably has this posted elsewhere but for those impatiently waiting, like myself. The link for KSC video feeds http://science.ksc.nasa.gov/shuttle/countdown/video/
I really don't want to go home to the snow and ice, Sunday sounds good to me, Monday everything starts to melt back home
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ntschke - 7/12/2007 6:40 PM Based on the fact that they're going to start this press conference late...is there any indication from other sources or via wbecams of any activity that would indicate preps for a launch attempt tomorrow? Such as RSS rollback, lighting or other tell-tale signs?
Still closed around Atlantis.
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NET 8:15 PM EST.
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presser now net 8:15
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How are we looking for the time they'll need to retract the RSS? Getting close isn't it?
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Chris Bergin - 7/12/2007 7:50 PM
How are we looking for the time they'll need to retract the RSS? Getting close isn't it?
Last time they retracted it, it was 8:00 PM EST (coming up in 9 minutes)...
EDIT: I'm keeping a look-out on the webcams for RSS Retract... Hoping it'll be soon. :)
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Chris Bergin - 7/12/2007 6:50 PM How are we looking for the time they'll need to retract the RSS? Getting close isn't it?
Looks like by now they would need to retract the RSS. With no retract any time soon that can tell us that they aren't going to try for tomorrow.
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8:30 and counting.. do I have a 9pm
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I'm also Hoping they will begin RSS retract SOON.
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Justin Wheat - 7/12/2007 6:53 PM
Chris Bergin - 7/12/2007 6:50 PM How are we looking for the time they'll need to retract the RSS? Getting close isn't it?
Looks like by now they would need to retract the RSS. With no retract any time soon that can tell us that they aren't going to try for tomorrow.
Remember STS-116 a year ago when they didn't retract the RSS until very-late in the count for the second attemt? They've got plenty of time yet. ;)
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Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test.
Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
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Chris Bergin - 7/12/2007 6:56 PM Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test. Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
You thinking they aren't going to try for tomorrow?
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Justin Wheat - 8/12/2007 12:58 AM
Chris Bergin - 7/12/2007 6:56 PM Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test. Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
You thinking they aren't going to try for tomorrow?
No, we think they will launch this weekend. Trying to work out if it'll be Sat or Sun.
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Justin Wheat - 7/12/2007 7:58 PM
Chris Bergin - 7/12/2007 6:56 PM Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test. Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
You thinking they aren't going to try for tomorrow?
A try would work as a test... if the ECO's behave then we must be as good to go as any other flight.. they have been a UA for many a year.. so there is nothing new here... other than we see some strange readings, but now know that is conductivity... I would guess that the tanking has done the thermal thing to the connectors and we will be in "steady" state going forward...
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Chris Bergin - 7/12/2007 6:59 PM
Justin Wheat - 8/12/2007 12:58 AM
Chris Bergin - 7/12/2007 6:56 PM Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test. Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
You thinking they aren't going to try for tomorrow?
No, we think they will launch this weekend. Trying to work out if it'll be Sat or Sun.
I would prefer that they went ahead and carried out the tanking test first to be on the safe side. That is, if they think it will be ok to tank another time. I know they don't like to unless absolutely necessary. If they perform a test, how many more chances would they have to tank again later?
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Chris Bergin - 7/12/2007 6:59 PM
Justin Wheat - 8/12/2007 12:58 AM
Chris Bergin - 7/12/2007 6:56 PM Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test. Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
You thinking they aren't going to try for tomorrow?
No, we think they will launch this weekend. Trying to work out if it'll be Sat or Sun.
Flight Control Team in Houston is being told NET Sunday!
Mark Kirkman
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mkirk - 8/12/2007 1:06 AM
Chris Bergin - 7/12/2007 6:59 PM
Justin Wheat - 8/12/2007 12:58 AM
Chris Bergin - 7/12/2007 6:56 PM Well they'll have some buffer time yet. Trying to work out the very latest for the S0007 requirements, and also if they can do this later if they decide on a tanking test. Speaking of which ET gave strong rationale to carry out a tanking test, pre-MMT.
You thinking they aren't going to try for tomorrow?
No, we think they will launch this weekend. Trying to work out if it'll be Sat or Sun.
Flight Control Team in Houston is being told NET Sunday!
Mark Kirkman
Copy that Mark!
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Sounds like a good decision to try on Sunday and not rush things.
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shuttlefan - 7/12/2007 7:56 PM
Remember STS-116 a year ago when they didn't retract the RSS until very-late in the count for the second attemt? They've got plenty of time yet. ;)
Yes, and that was working a 48-hour scrub turnaround, too.
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Now bumped to NET 8:45 pm Eastern...
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Florida Today just reported via text message scrubbed NET 1515ET Sunday
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mike robel - 7/12/2007 7:19 PM
Florida Today just reported via text message scrubbed NeTl Sunday around 1500
They announced Sunday at 3:21 p.m. EST at the KSC press site.
MMT is still meeting. Wayne Hale and Mike Leinbach are expected to come over to briefing.
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Gary - 7/12/2007 7:19 PM
psloss - 8/12/2007 1:17 AM
Now bumped to NET 8:45 pm Eastern...
And to paraphrase an earlier reply - I'll see your 8:45pm and raise you a 9pm :laugh:
LOL! I think I can quote this STS-122 Mission Overview by heart now. This is like the 20th time I have seen it now. :laugh:
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Bubbinski - 7/12/2007 7:30 PM
Seattle Dave, are you saying Saturday is still on the table?
No, I was saying that scrubbed Sunday is wrong, they are looking at Sunday. And the launch time is wrong anyway. See Robert's post for the correct launch time.
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NET 9pm.
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Chris mentioned earlier that the ET project was leaning towards a tanking test going into the MMT meeting. Would a tanking test tomorrow, then a launch count Sunday be an option?
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Chris Bergin - 7/12/2007 8:37 PM
NET 9pm.
Do I hear 9:15? 9:30? Sold to the bidder on the left for midnight!
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shuttlefan - 8/12/2007 1:40 AM
Chris mentioned earlier that the ET project was leaning towards a tanking test going into the MMT meeting. Would a tanking test tomorrow, then a launch count Sunday be an option?
ET gave good rationale for the tanking test, but it doesn't mean MMT would take up that option.
We have a lot more presentations via L2, and tomorrow I'll do an article based on Flight Controller proccedures with regards to the ECOs and other items to round it up.
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Andrewwski - 7/12/2007 7:44 PM
Do I hear 9:15? 9:30? Sold to the bidder on the left for midnight!
It was announced here at the press site as a solid 9pm.
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from nasa.gov
Dec. 7 - 8:30 p.m. EST
Due to the length of tonight's Mission Management Team discussion, we are no go for a Saturday launch. The next attempt would be no earlier than Sunday at 3:21:00 p.m. EST.
A news conference is coming up on NASA TV no earlier than 9 p.m.
For a launch attempt on Sunday, tanking coverage on NASA TV would begin at 6 a.m., with launch coverage starting at 10 a.m.
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I guess adding tanking coverage for the next attempt is unsurprising...
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Seattle Dave - 7/12/2007 5:34 PM Bubbinski - 7/12/2007 7:30 PM Seattle Dave, are you saying Saturday is still on the table?
No, I was saying that scrubbed Sunday is wrong, they are looking at Sunday. And the launch time is wrong anyway. See Robert's post for the correct launch time.
The launch target for Sunday is 3:21 PM, EST
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Press Briefing coming up in 7 minutes:
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Jim Oberg article on flight rules:
http://www.msnbc.msn.com/id/22151584/
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Briefers are in the room...
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Briefing starting w/PAO intros...
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Wayne Hale starts with historical background...noted 3 low-level sensors failed during the first tanking/detanking...
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Hale: Right now, at the pad, all ECO's and wiring are good..
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They are going to review the flight crew office proposal to tighten the flight rules and use a shorter launch window around the in-plane time (to maximize APM), meet again tomorrow at 1 pm local.
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Hale: If FCO [Flight Crew Office] gives a good plan, we will try to launch on Sunday. If they do not, we will stand down and try something different.
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Wayne Hale underwear manifest reference ;)
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Mike Leinbach notes that the LH2 top off completed a few hours ago; can support Sunday and Monday attempts. After that 72-hour recycle to top both cyro quantities.
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Nice reference to Wayne Hales clothing packing strategy :-) (Search for WHUM)
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The shortened launch window would be on the order of about one minute beginning at the in-plane time.
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As seen on some of the screencaps, they are holding at T-11, will extend for another 24 hours.
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Mike Leinbach just said the new flight rules require all 4 of the ECO sensors to be working. So if they try to launch Sunday and there are any problems with the ECO sensors, it'll be a scrub.
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Falcon - 7/12/2007 9:16 PM
Mike Leinbach just said the new flight rules require all 4 of the ECO sensors to be working. So if they try to launch Sunday and there are any problems with the ECO sensors, it'll be a scrub.
Yes, that was part of the proposal that Wayne Hale mentioned came from the Flight Crew Office (FCOD).
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Marcia Dunn had a good question about flying with 2 ECO sensors.
Hale says "Going to 2 of 4 is not where we want to be.."
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The logic behind going back to 4 of 4 is the tanking history (no failed WET channels during retanking).
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The FCOD proposal would be to allow the voltage readings to be used as a part of the decision-making during ascent.
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Wayne Hale answering Bill Harwood's question now doing a shortened version of ECOs 101. (Now talking about the arming mass noted in this thread earlier.)
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Another nice description from Wayne Hale about the orbiter software logic after reaching the arming mass.
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Just to expand on psloss' explanation of 4/4, for those who may not have seen the briefing: Hale explained that they have decided to require all four ECO sensors, because evidence shows that when this has happened in the past, all four ECO sensors worked nominally during re-tanking in the subsequent attempt. So, if all four work nominally when they go for the next attempt, that tells them that it is a (so far) consistent off-nominal issue that acts the same in every situation. If less than 4/4 function, this tells them it is not necessarily the same issue, and would require them to evaluate it differently. For instance, Hale said the sensors have never "failed dry", so if they were to see something like that, this would alert them that it was something different from what has been seen in the past. Hope that helps explain it to those who may not be as technically knowledgeable.
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Thanks for elaborating...just to be clear, Wayne Hale said that they are still evaluating the FCOD proposal and will decide on whether to accept it tomorrow.
Basically, if the proposal is accepted and any of the LH2 ECO circuits fail (WET or DRY) during the next tanking, they would be no-go.
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Briefing completed.
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Press conference after tomorrow's MMT meeting at 1.
Tanking will start at 5:55 AM EST on Sunday, if they do decide to go with a Sunday launch.
Intermittent updates on tanking will be before launch coverage, barring they go with Sunday.
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Good Plan! I'm comfortable with it.
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Someone at the briefing did ask about when during the count down 4/4 sensors had to be working. I didn't think the answer was clear. Is it the case that if one sensor behaves unexpectedly at any point that day's tanking and subsequent launch attempt will be scrubbed, or are they looking just for 4/4 to be working at the point they commit to launch? (As I write this I can see psloss has interpreted the briefing as any sensor failure during tanking will result in a scrub. )
Another question arising from the briefing is where does the output of the new "voltmeter" readings coming out of these sensors get routed to - do the crew have access to these live during ascent, are they fed into the computers, or are they read by people on the ground?
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This is a very good plan and I have every confidence in Mr Hale. I also understood that there has to be a 4/4 no fault sensor flight rule in order to launch. The extra telemetry from the additional circuits would be used if sensors failed after launch.
On the sensor system, it seems strange to me that an open circuit wiring fault on the ECO sensors is designed as a fail to wet. Surely it would be better and safer if an o/c fault failed to dry?
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What time is T-0 on Sunday attempt?
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TJL - 8/12/2007 2:55 AM
What time is T-0 on Sunday attempt?
3:21pm in a one minute launch window (mentioned earlier ;) but it's a long ass thread now).
Thinking of starting a new one half way through tomorrow when the next article on MMT documentation is up.
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nsf-rt - 7/12/2007 9:54 PM
Someone at the briefing did ask about when during the count down 4/4 sensors had to be working. I didn't think the answer was clear. Is it the case that if one sensor behaves unexpectedly at any point that day's tanking and subsequent launch attempt will be scrubbed, or are they looking just for 4/4 to be working at the point they commit to launch? (As I write this I can see psloss has interpreted the briefing as any sensor failure during tanking will result in a scrub. )
Yes, that's how I interpret 4/4 -- because any failure of any of the circuits (the likelihood would be failing WET) wouldn't fit the behavior seen in the past. Granted the second STS-114 tanking (on the second ET) occurred after they went into the aft and did a lot of work, but in both the STS-114 and STS-115 cases on the second tanking all the sensor circuits behaved as expected.
nsf-rt - 7/12/2007 9:54 PM
Another question arising from the briefing is where does the output of the new "voltmeter" readings coming out of these sensors get routed to - do the crew have access to these live during ascent, are they fed into the computers, or are they read by people on the ground?
Telemetry that can be seen in the control centers (LCC and MCC) and not directly by the crew on the flight deck. I don't believe the orbiter flight software uses the voltage parameters in its logic.
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ETEE - 7/12/2007 9:54 PM
This is a very good plan and I have every confidence in Mr Hale. On the sensor system design, it seems strange to me that an open circuit wiring fault on the ECO sensors is being interpreted as a fail to wet. Surely a design with o/c fault failing to dry would be better and safer?
No, because an ECO sensor reading dry implies an already off-nominal condition. With the current setup, a completely empty tank will result only if three ECO sensors fail and fuel is used at an abnormally high rate. If the ECO sensors failed dry, a failure of only two sensors would result in premature engine cutoff.
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nsf-rt - 7/12/2007 6:54 PM Someone at the briefing did ask about when during the count down 4/4 sensors had to be working. I didn't think the answer was clear. Is it the case that if one sensor behaves unexpectedly at any point that day's tanking and subsequent launch attempt will be scrubbed, or are they looking just for 4/4 to be working at the point they commit to launch? (As I write this I can see psloss has interpreted the briefing as any sensor failure during tanking will result in a scrub. )
The sensors have to be 4/4 during tanking. Otherwise, NASA would have proceeded with the launch attempt yesterday in the hopes the 2 ECO sensors suddenly started to work nominally by T-0. :bleh:
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psloss - 7/12/2007 9:13 PM
Mike Leinbach notes that the LH2 top off completed a few hours ago; can support Sunday and Monday attempts. After that 72-hour recycle to top both cyro quantities.
I'm wondering if that's absolute. If they scrub early say due to weather on Monday would they have sufficient cyro to consider Tuesday? or start top off early for a Wednesday attempt?
Scott.
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They won't scrub early due to weather either of those days, at the worst it would be a late-in-the-count call.
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There's much longer threads on the site's forum than this 27 pager. So I would keep it going until there's a confirmed go for tanking on Sunday. It's a fantastic resource thread.
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SiameseCat - 7/12/2007 8:05 PM
ETEE - 7/12/2007 9:54 PM
This is a very good plan and I have every confidence in Mr Hale. On the sensor system design, it seems strange to me that an open circuit wiring fault on the ECO sensors is being interpreted as a fail to wet. Surely a design with o/c fault failing to dry would be better and safer?
No, because an ECO sensor reading dry implies an already off-nominal condition. With the current setup, a completely empty tank will result only if three ECO sensors fail and fuel is used at an abnormally high rate. If the ECO sensors failed dry, a failure of only two sensors would result in premature engine cutoff.
and the track record to-date - 2 uses of ECO sensors out of 120 launches - tells us with 99% confidence that the chance of even needing the ECO sensors is less than 7% (binomial stats), so risking the mission on a faulty sensor going DRY would be a serious unnecessary loss-of-mission risk.
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In my opinion I find it horrifying and unacceptable that this dangerous ECO sensor system has not been disabled. You cannot tell me there is no other way to tell if you got a giant leaking hole in the ET (Quickly losing pressure obviously) or the engine is using an extreme amount of fuel.
Please don't fire back with the "You want to put the crew at risk?" junk I think the crew will be in a much more serious position if they suddenly found themselves the first to attempt the most realistic version of the TAL abort. Even if they do manage to get over the panic and shock of suddenly finding yourself in such a situation and making it to a smooth landing. Do you think any of them will be fit for flying again? (Mentally) Do you think there even will be shuttle flights afterwards?
Call me an idiot if you wish but I think the chances of them losing their lives to an ECO sensor failure (DRY) is much higher than somehow getting in a position where the engine destroys the shuttle due to the tank running dry (Think about what has to happen for that to happen). The chances of a piece of metal or worse blocking the fuel transport and causing a failure has to be much higher
EDIT: Forgot that it takes engine power to do a RTLS.
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Joffan - 8/12/2007 12:19 AM
SiameseCat - 7/12/2007 8:05 PM
ETEE - 7/12/2007 9:54 PM
This is a very good plan and I have every confidence in Mr Hale. On the sensor system design, it seems strange to me that an open circuit wiring fault on the ECO sensors is being interpreted as a fail to wet. Surely a design with o/c fault failing to dry would be better and safer?
No, because an ECO sensor reading dry implies an already off-nominal condition. With the current setup, a completely empty tank will result only if three ECO sensors fail and fuel is used at an abnormally high rate. If the ECO sensors failed dry, a failure of only two sensors would result in premature engine cutoff.
and the track record to-date - 2 uses of ECO sensors out of 120 launches - tells us with 99% confidence that the chance of even needing the ECO sensors is less than 7% (binomial stats), so risking the mission on a faulty sensor going DRY would be a serious unnecessary loss-of-mission risk.
I'm aware of the Columbia low-level cutoff on STS-93... what was the other occurrence of the use of the ECO sensors?
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psloss - 7/12/2007 6:21 PM
The logic behind going back to 4 of 4 is the tanking history (no failed WET channels during retanking).
This logic is not compelling. We have no clue about the root cause. Sure, we've launched while clueless like this several times before and we didn't lose the crew, vehicle or mission those times. Does that mean if we launch clueless again, we can expect the same result?
How many tanks have been launched with sensors that had incorrectly indicated "wet" on tests during prior tankings, and then 4 of 4 correctly responded "dry" on the test for the final tanking? Would a Bayesian analysis give us very high confidence in the outcome of the next such launch?
We shouldn't even be in this situation, because we shouldn't have attempted those prior launches when there had been unexplained behavior from a life-critical system. That was "go fever" thinking then, and it is "go fever" thinking to launch with this tank now. STS should not launch again until a root cause for the sensor failures has been determined.
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sdsds - 8/12/2007 1:31 AM
psloss - 7/12/2007 6:21 PM
The logic behind going back to 4 of 4 is the tanking history (no failed WET channels during retanking).
This logic is not compelling. We have no clue about the root cause. Sure, we've launched while clueless like this several times before and we didn't lose the crew, vehicle or mission those times. Does that mean if we launch clueless again, we can expect the same result?
How many tanks have been launched with sensors that had incorrectly indicated "wet" on tests during prior tankings, and then 4 of 4 correctly responded "dry" on the test for the final tanking? Would a Bayesian analysis give us very high confidence in the outcome of the next such launch?
We shouldn't even be in this situation, because we shouldn't have attempted those prior launches when there had been unexplained behavior from a life-critical system. That was "go fever" thinking then, and it is "go fever" thinking to launch with this tank now. STS should not launch again until a root cause for the sensor failures has been determined.
If you'd have listened to the briefings you would know that this is an intermitant problem with the ECO sensors or their related wiring. You can't diagnose a problem (let a lone find root cause) if the problem goes away the next time you tank for troubleshooting.
And saying that we shouldn't have launched those previous attempts means STS-114 would still be on the ground and we'd still be waiting to Return to Flight from Columbia. That's not very logical! You have to take it for what it is. There is always risk in space flight and having one ECO sensor fail still leaves plenty of redundancy in the system. Granted this situation is different, but for all we know we could tank and de-tank this ET a hundred times and never recreate what we saw on Thursday. How would that help us find root cause?
Also, keep in mind that this management team has done a tremendous job preventing launch fever. If this were launch fever Atlantis would have launched on Friday, the day after the three ECO sensors first gave them trouble.
Also, keep in mind that Sunday is a No Earlier Than date... it doesn't mean they're defeinetely going to try to launch tomorrow it just means they've told the launch team to be ready to try on Sunday. They could just as easily come back tomorrow and say "we're not going to try until Monday or even January.
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Sdsds What? The ECO system is wrong, broken, gone to hell, or whatever you want to call it. You want them to actually spend potentially years finding the "root cause" on a system which should be disabled? What if the supposed fix causes the sensors to fail DRY during launch and the crew crashes the shuttle attempting a TAL Abort?
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Zachstar - 7/12/2007 10:40 PM
Sdsds What? The ECO system is wrong, broken, gone to hell, or whatever you want to call it. You want them to actually spend potentially years finding the "root cause" on a system which should be disabled?
A tank could run dry for a variety of reasons, and without ECO sensors reporting that condition it would likely result in a catastrophic engine failure leading to loss of the crew.
Zachstar - 7/12/2007 10:40 PM
What if the supposed fix causes the sensors to fail DRY during launch and the crew crashes the shuttle attempting a TAL Abort?
The crews train to perform TAL aborts, and there is every reason to have confidence in their ability to do so. But there is no way to save a vehicle if an engine explodes.
I would like to see NASA return humans to the Moon in my lifetime, and if we lose another Shuttle crew that just won't happen.
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Sorry for asking a probably dumb question, but just to be sure about the "4 of 4 ECO sensors" flight rule: If 1 of the ECO sensors fail during tanking on Sunday the way it failed on Thursday, i.e. not responding correctly to the test signal, do they scrub already because of this or do they use the new instrumentation to diagnose the failing sensor and do not scrub if the new instrumentation says the sensor is fine despite the failed test?
Thanks
Tschachim
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Yes, with 4/4, if they have one LH2 ECO sensor fail, then they scrub.
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So Sunday is the new launch date?
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sdsds - 8/12/2007 1:31 AM
How many tanks have been launched with sensors that had incorrectly indicated "wet" on tests during prior tankings, and then 4 of 4 correctly responded "dry" on the test for the final tanking? Would a Bayesian analysis give us very high confidence in the outcome of the next such launch?
We shouldn't even be in this situation, because we shouldn't have attempted those prior launches when there had been unexplained behavior from a life-critical system. That was "go fever" thinking then, and it is "go fever" thinking to launch with this tank now. STS should not launch again until a root cause for the sensor failures has been determined.
Are your questions above rhetorical? If not, then it's hard to agree with your conclusion because you have presented very little rationale for it. The way I read it, you're asserting that they shouldn't launch until they completely understand how the system works. If that's the rule, then it's a Catch-22.
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Trekkie07 - 8/12/2007 1:17 AM
I'm aware of the Columbia low-level cutoff on STS-93... what was the other occurrence of the use of the ECO sensors?
51-F. In both cases the LOX low-level sensors went dry first, as designed.
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Maybe this is available here on another site but I haven't found it yet...does anyone know if there is an ET reference guide, schematic, cut-away view etc that might be of use in visualizing the different components invovled in this debate?
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ntschke - 8/12/2007 7:18 AM
Maybe this is available here on another site but I haven't found it yet...does anyone know if there is an ET reference guide, schematic, cut-away view etc that might be of use in visualizing the different components invovled in this debate?
NASA.gov reposted schematics:
http://www.nasa.gov/mission_pages/shuttle/main/
Or do you mean something else?
(And actually, the overall schematic is in Mark's Interspacenews story that has been linked in this thread already.)
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psloss - 8/12/2007 1:15 PM
Trekkie07 - 8/12/2007 1:17 AM
I'm aware of the Columbia low-level cutoff on STS-93... what was the other occurrence of the use of the ECO sensors?
51-F. In both cases the LOX low-level sensors went dry first, as designed.
If I read it correctly, this time the LH2 sensors failed, right? Are those same sensors used in the LOX tank or do they have a different design. (I am wondering why only those sensors in the LH2 tank show this erroneous readings.)
Couldn't it be that the material of the sensors has changed over time to an extent, that it is susceptible to a "chemical" LH2 attack in some way. As I work steel industry, I experienced quite a few cases where H2 is altering material to a point where it's beyond it's designed behaviour and has to be replaced.
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psloss - 8/12/2007 7:31 AM ntschke - 8/12/2007 7:18 AM Maybe this is available here on another site but I haven't found it yet...does anyone know if there is an ET reference guide, schematic, cut-away view etc that might be of use in visualizing the different components invovled in this debate?
NASA.gov reposted schematics: http://www.nasa.gov/mission_pages/shuttle/main/ Or do you mean something else? (And actually, the overall schematic is in Mark's Interspacenews story that has been linked in this thread already.)
Thanks,I saw those from an erlier post and they help but I thought in the past, somehwere, I saw a nice detailed cut away view of the ET and exploded views of the seperate tanks, pipes, etc. Just tying to get an idea of access and internal workings of the bottom of the tank.
And just to get my "Mulligan" dumb question of the day out of the way early...I'm assuming that the shear velocity of the vehicle throughout ascent (and at the point that ECOs would even be needed) keeps the fuel forced to the bottom of the tank? I assume at those speeds the tank almost always "feels" like its in a vertical position?
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ntschke - 8/12/2007 7:41 AM
And just to get my "Mulligan" dumb question of the day out of the way early...I'm assuming that the shear velocity of the vehicle throughout ascent (and at the point that ECOs would even be needed) keeps the fuel forced to the bottom of the tank? I assume at those speeds the tank almost always "feels" like its in a vertical position?
It's not the velocity, it's the acceleration, but yes, that's what keeps the fuel filling the bottom dome.
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ntschke - 8/12/2007 12:41 PM
Thanks,I saw those from an erlier post and they help but I thought in the past, somehwere, I saw a nice detailed cut away view of the ET and exploded views of the seperate tanks, pipes, etc. Just tying to get an idea of access and internal workings of the bottom of the tank.
L2, STS-122: ECO SYSTEM INFO/BACKGROUND on the STS-122 Special Section has the Booster Console handbook area for ECO and lots of very cool schematics and images of the sensors that are obviously not on NASA.gov
I've bumped it for you, as I know you're on L2.
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ntschke - 8/12/2007 7:41 AM
And just to get my "Mulligan" dumb question of the day out of the way early...I'm assuming that the shear velocity of the vehicle throughout ascent (and at the point that ECOs would even be needed) keeps the fuel forced to the bottom of the tank? I assume at those speeds the tank almost always "feels" like its in a vertical position?
Shortly before liftoff both tanks are pressurized and then the MPS maintains a "top" pressure (ullage pressure) within them; this isn't the best link, but it was quick:
http://spaceflight.nasa.gov/shuttle/reference/shutref/orbiter/prop/et.html
The program folks here can explain better.
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ShuttleFan75 - 8/12/2007 7:47 AM ntschke - 8/12/2007 12:41 PM Thanks,I saw those from an erlier post and they help but I thought in the past, somehwere, I saw a nice detailed cut away view of the ET and exploded views of the seperate tanks, pipes, etc. Just tying to get an idea of access and internal workings of the bottom of the tank.
L2, STS-122: ECO SYSTEM INFO/BACKGROUND on the STS-122 Special Section has the Booster Console handbook area for ECO and lots of very cool schematics and images of the sensors that are obviously not on NASA.gov I've bumped it for you, as I know you're on L2.
Thanks to all of you. Also, I found this on wiki (http://en.wikipedia.org/wiki/Space_Shuttle_external_tank):
"There are eight propellant-depletion sensors, four each for fuel and oxidizer. The fuel-depletion sensors are located in the bottom of the fuel tank. The oxidizer sensors are mounted in the orbiter liquid oxygen feed line manifold downstream of the feed line disconnect. During SSME thrusting, the orbiter general-purpose computers constantly compute the instantaneous mass of the vehicle due to the usage of the propellants. Normally, main engine cutoff is based on a predetermined velocity; however, if any two of the fuel or oxidizer sensors sense a dry condition, the engines will be shut down.
The locations of the liquid oxygen sensors allow the maximum amount of oxidizer to be consumed in the engines, while allowing sufficient time to shut down the engines before the oxidizer pumps cavitate (run dry). In addition, 1,100 pounds (500 kg) of liquid hydrogen are loaded over and above that required by the 6-1 oxidizer / fuel engine mixture ratio. This assures that cutoff from the depletion sensors is fuel-rich; oxidizer-rich engine shutdowns can cause burning and severe erosion of engine components.
Four pressure transducers located at the top of the liquid oxygen and liquid hydrogen tanks monitor the ullage pressures"

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(Sorry to the mods -- this discussion should be moved over to Q & A...)
Here's a post that Mark made a while back -- scroll down to the part on NPSP:
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=7886&start=1#M139197
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ntschke - 8/12/2007 7:54 AM
Also, I found this on wiki
please don't use wiki for space
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I know Chris will be writing it up, so I'm not teasing, but the presentations on L2 really show they could do this even with no ECOs. They just won't get into a problem of relying on the ECOs unless there was a big problem with the engines or MPS. I know Hale said that last night, but reading it in black and white says a lot.
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Maybe I interpreted this wrong, but didn't they say at the press conference last night that the onboard computer system won't even use the ECO sensors unless they are within 10 seconds of nominal MECO anyways? At that point, the velocity and altitude would leave only an ATO with the OMS engines, not the RTLS or TAL that other people are talking about.
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Life_Support_32 - 8/12/2007 10:17 AM
Maybe I interpreted this wrong, but didn't they say at the press conference last night that the onboard computer system won't even use the ECO sensors unless they are within 10 seconds of nominal MECO anyways? At that point, the velocity and altitude would leave only an ATO with the OMS engines, not the RTLS or TAL that other people are talking about.
Remember that the vehicle acceleration is 3g for the last several seconds of a nominal ascent. Cutting off at "arm" would cause a still substantial underspeed and may be beyond the delta-V capability of the OMS and RCS.
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Bump. Having some pagination issues with forum threads like this now, too...
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We'll start a new one shortly. For some reason, some of the long threads jump to the next page, but don't display that latest post (at the start of the new page).
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Launch window (edited after user seemed to forget about copyright. Though we knew this already! - James).
http://www.cbsnews.com/network/news/space/122/122windows.html
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Is this news conference scheduled for 1:00?
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dember - 8/12/2007 10:56 AM
Is this news conference scheduled for 1:00?
No, as stated in the article on the front of the site (do read it), the MMT starts at 1pm.
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thanks james.
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MMT meets at 1 - so any what time should we hear if Sunday is a go or not?
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trlstyle - 8/12/2007 11:05 AM
MMT meets at 1 - so any what time should we hear if Sunday is a go or not?
Probably a few hours later at least.
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Time to move to a new thread:
http://forum.nasaspaceflight.com/forums/thread-view.asp?tid=11092&posts=1&start=1