Author Topic: SCRUB: STS-119: LAUNCH ATTEMPT 1 and interim processing coverage  (Read 101319 times)

Offline astrobrian

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NASA just tweeted the following:


At 2:37 p.m. EDT today's launch attempt was scrubbed. Try again in 24 hours. The cause is a hydrogen leak at an attach point to the orbiter.


Does this description fit the information you have or is their 24 hour slip too optimistic?
That would seem to indicate the bipod would it not?

Offline cb6785

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It definetly get's hotter if we wanna get the full mission duration.
You know, if I’d had a seat you wouldn’t still see me in this thing. - Chuck Yeager

Offline NavySpaceFan

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It seems that everything that can happen to delay launch has happened.

Nah, I put this in the "it's always something" category.  The pad flow up to this point has been very smooth.
<----First launch of DISCOVERY, STS-41D!!!!

Offline rsnellenberger

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The leak downstream of the skid, somewhere around the GUCP.
What/which/where/who is "the skid", please?
« Last Edit: 03/11/2009 06:06 pm by rsnellenberger »

Offline Chris Bergin

The leak downstream of the skid, somewhere around the GUCP.
What/which/where/who is "the skid"?

Asking, might be engineer talk, as I was copying across the notes.
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Offline collectSPACE

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An MMT meeting has been set for 5:00 p.m. EDT.
« Last Edit: 03/11/2009 06:11 pm by collectSPACE »

Offline Ford Mustang

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An MMT meeting has been set for 5:00 p.m. EDT.

I'll provide a live transcription of the event.

Offline Chris Bergin

An MMT meeting has been set for 5:00 p.m. EDT.

I'll provide a live transcription of the event.

MMT meetings are internal. A post-MMT presser would be what you're thinking.
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Offline Ford Mustang

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An MMT meeting has been set for 5:00 p.m. EDT.

I'll provide a live transcription of the event.

MMT meetings are internal. A post-MMT presser would be what you're thinking.

Right, sorry.  Rushed home for coverage to find out they scrubbed, kinda in a downer mood!

Offline Ronsmytheiii

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Quote
The Hydrogen Vent Line Access Arm is used to mate the External Tank (ET) Ground Umbilical Carrier Plate (GUCP) to the launch pad hydrogen vent line. The GUCP provides support for plumbing and cables, called umbilicals that transfer fluids, gases, and electrical signals between two pieces of equipment.

During Shuttle fueling operations, hazardous hydrogen gas is vented from a fuel tank inside the ET. This gas travels through the GUCP and vent line over to a flare stack located a safe distance from the Shuttle. The flare stack is a tall pipe with a flame igniter at top that safely burns away the hydrogen gas.

The Hydrogen Vent Line Access Arm also provides contingency access to the ET. It is retracted several hours before launch, leaving the umbilical attached. When the solid rocket boosters ignite, the umbilical carrier plate releases from the ET and falls back against the tower. A curtain of sprayed water protects it from flames produced by the Shuttle engines during launch.

http://enterfiringroom.ksc.nasa.gov/systemSwingArm.htm

Offline rsnellenberger

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The leak downstream of the skid, somewhere around the GUCP.
What/which/where/who is "the skid"?

Asking, might be engineer talk, as I was copying across the notes.
I'm now guessing that it's the attach plate itself, which would be good in that "downstream" would indicate that it's not in the vehicle or in the attach points to the orbiter.  If so, might not be as hard to pin down as those earlier H2 leaks in the ET/Orbiter umbilicals (STS-35?). 

Offline rsnellenberger

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An MMT meeting has been set for 5:00 p.m. EDT.

I'll provide a live transcription of the event.

MMT meetings are internal. A post-MMT presser would be what you're thinking.

Right, sorry.  Rushed home for coverage to find out they scrubbed, kinda in a downer mood!
We were all prepared to be very impressed  :)

Offline Namechange User

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The leak downstream of the skid, somewhere around the GUCP.
What/which/where/who is "the skid"?


Asking, might be engineer talk, as I was copying across the notes.
I'm now guessing that it's the attach plate itself, which would be good in that "downstream" would indicate that it's not in the vehicle or in the attach points to the orbiter.  If so, might not be as hard to pin down as those earlier H2 leaks in the ET/Orbiter umbilicals (STS-35?). 


It is not in the orbiter or at the umbilicals.  It is in the GUCP area, hopefully just a bad alignment or seal. 
Enjoying viewing the forum a little better now by filtering certain users.

Offline glanmor05

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Is it too early or does anyone know where the count will commence from and at what time?  Assuming, tanking therefore 6 hours?
"Through struggles, to the stars."

Offline padrat

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except the skid is downstream of the GUCP, not the other way around.
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Offline hobson911

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Thanks Pad rat for the photo and pointing out the locations on the FSS

Offline Chris Bergin

Is it too early or does anyone know where the count will commence from and at what time?  Assuming, tanking therefore 6 hours?

Wait for the MMT. We're hearing its 18 hours just to boil off the tank if it needs to be inert. That makes 24 hours tight, but it depends on how much troubleshooting is required. Bottom line is they are still draining the tank, wait for the MMT.
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Offline rsnellenberger

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Thanks Pad rat for the photo and pointing out the locations on the FSS

Ditto...

Offline violin1238

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I have been very skeptical of this particular external tank. I don't know why. I wasn't confident when Atlantis was at the pad with ET-127 back in September and know I feel the same with Discovery at the pad  with ET-127.

Offline Paul Howard

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