Go Back  PPRuNe Forums > Flight Deck Forums > Tech Log
Reload this Page >

STS-107, Chronicle Of A Disaster Foretold?

Wikiposts
Search
Tech Log The very best in practical technical discussion on the web

STS-107, Chronicle Of A Disaster Foretold?

Thread Tools
 
Search this Thread
 
Old 3rd Feb 2003, 10:51
  #61 (permalink)  
 
Join Date: Sep 2000
Location: England
Posts: 303
Likes: 0
Received 0 Likes on 0 Posts
An interesting article on Shuttle Safety deficiencies from the UK Observer newspaper.

http://www.observer.co.uk/internatio...887236,00.html
TheShadow is offline  
Old 3rd Feb 2003, 11:42
  #62 (permalink)  
 
Join Date: Jun 2000
Posts: 471
Likes: 0
Received 0 Likes on 0 Posts
nasaboy, I entirely agree with your statement and might I suggest a re-read of my post will dispell your assertion
fire wall is offline  
Old 3rd Feb 2003, 12:30
  #63 (permalink)  
 
Join Date: Feb 1999
Location: UK
Posts: 1,091
Likes: 0
Received 0 Likes on 0 Posts
My initial thought is that thrust would be used, but in thinking about it, control surfaces may be used at those heights because of the speed and some atmosphere. Certainly, the roll-trim was being added by the on-board computer to react to the drag of the left wing, so one would assume control surfaces were sufficient to attain and execute the roll routines to lose speed (which occur at 56 degrees nose up.

(edited for spelling)

Last edited by no sponsor; 3rd Feb 2003 at 12:44.
no sponsor is offline  
Old 3rd Feb 2003, 13:50
  #64 (permalink)  

PPRuNe Person
 
Join Date: Jun 2001
Location: see roster
Posts: 1,268
Likes: 0
Received 0 Likes on 0 Posts
atacaks:

The re-entry profile is already the least stressful. This question was asked during last night's press conference and answered by Mr Dittemore
overstress is offline  
Old 3rd Feb 2003, 14:06
  #65 (permalink)  
 
Join Date: Jun 2002
Location: Geneva, Switzerland
Age: 58
Posts: 1,908
Received 3 Likes on 3 Posts
ISS or NOT

I think you are not understanding the problems of "orbit". It is massively difficult to rendevous when it is the aim of the mission. To do so on an ad hoc basis, particularly when something has gone wrong = degraded capability is just impractical.
Just wondering: would anyone more skilled than myself do the actual calculation and come up with the ammount of fuel necessary for an ISS rendevous vs. the on board ammount (including the desorbintg reserve) ?
The re-entry profile is already the least stressful. This question was asked during last night's press conference and answered by Mr Dittemore
Thanks - I missed that one.

Would anyone care to expand on that one ? What would be the problems of doing a less agressive entry ?
atakacs is offline  
Old 3rd Feb 2003, 14:07
  #66 (permalink)  
 
Join Date: Jan 2001
Location: Fantasy Island
Posts: 555
Likes: 0
Received 0 Likes on 0 Posts
Just totally off-topic............does anyone else find it slightly peculiar that Challenger, Endeavour and Discovery were all named after British ships?
BahrainLad is offline  
Old 3rd Feb 2003, 15:06
  #67 (permalink)  
Ecce Homo! Loquitur...
 
Join Date: Jul 2000
Location: Peripatetic
Posts: 17,427
Received 1,593 Likes on 730 Posts
Atlantis, Challenger and Columbia were named after American ships. The Endeavour and Discovery were named after Captain Cook's ships. And the Enterprise was named after a certain starship........
Shuttle names
ORAC is offline  
Old 3rd Feb 2003, 15:06
  #68 (permalink)  
 
Join Date: Mar 2001
Location: Europe
Age: 56
Posts: 409
Likes: 0
Received 0 Likes on 0 Posts
Post

A link to a very good close up video showing the "foam" debris hiting the orbiter at launch.

http://www.floridatoday.com/columbia/debrisvideo.htm
Vortex what...ouch! is offline  
Old 3rd Feb 2003, 15:14
  #69 (permalink)  
 
Join Date: Feb 2001
Location: US
Posts: 604
Likes: 0
Received 0 Likes on 0 Posts
Would anyone care to expand on that one ? What would be the problems of doing a less agressive entry ?
There is no possible "less aggressive entry." Nasa already determined the entry profile that would cause the least stress on the shuttle and that's the one they're using. Any other profile would result in more stress on the shuttle, not less. If there was a less risky, lower stress profile, they'd already be using it.
OFBSLF is offline  
Old 3rd Feb 2003, 15:43
  #70 (permalink)  

Victim of Blackmailing Scouser
 
Join Date: Aug 2000
Location: Zürich, Switzerland (But a Brit)
Age: 59
Posts: 113
Likes: 0
Received 0 Likes on 0 Posts
fish

Ok, for once I'm on par with the rest of you on an aeronautical subject: I also know sod all about it.

For years now I've been tracking the Shuttle and ISS on the web. It has long seemed to me that the Space Shuttle as a concept has been oversold to the American public, probably in order to secure NASA the immense budgets needed to develop it, and then to keep it running.

i. It is not reusable. (Recycleable, more like, or, perhaps, semi-expendable).

ii. It is not routine.

iii. It is not safe. (i.e. Even the post-Challenger target of 1:1,000 failure ratio is not 'safe').

iv. It is not casual. (i.e. ad-hoc EVAs).

v. Once in orbit, it is not really a 'space ship', in the popular sense. (More like a sophisticated projectile, with the ability to perform minor adjustments to its orientation and orbit).


Even a brand new Shuttle system is not going to meet all of the above criteria, and unlikely to meet even two of them.

The reality is that technology has yet to catch up to the space travel expectations of the public imagination. The Shuttle was, and is, a magnificent demonstration of American technology. But even that's not enough, yet.

TW
Tricky Woo is offline  
Old 3rd Feb 2003, 15:55
  #71 (permalink)  
 
Join Date: Jan 2001
Location: Fantasy Island
Posts: 555
Likes: 0
Received 0 Likes on 0 Posts
So which is right?

Challenger, the second orbiter to become operational at Kennedy Space Center, was named after the British Naval research vessel HMS Challenger that sailed the Atlantic and Pacific oceans during the 1870's.
http://science.ksc.nasa.gov/shuttle/...hallenger.html
BahrainLad is offline  
Old 3rd Feb 2003, 16:11
  #72 (permalink)  
 
Join Date: Jan 2000
Location: 03 ACE
Age: 73
Posts: 1,015
Received 30 Likes on 20 Posts
Atakacs, you say "(and this was the heaviest landing in the Shuttle history)"

This interests me. Do we know what the Main Mission was on this particular launch.

I assume from your point, that some kind of recovery operation must have been at least, part of the Mission.
El Grifo is offline  
Old 3rd Feb 2003, 17:27
  #73 (permalink)  
Hwel
Guest
 
Posts: n/a
The weight was due to the science modules in the cargo bay, no recovery operation was carried out.

On another note in 1979 NASA said it intended 560 shuttle flights in the first 12 years. Peaking at 65 flights in 1988. the anticipated turn around times were 2 weeks for routine ops and "a matter of hours for rescue missions" Designs were started in the early 80's for 74 seat pax modules (to ferry crews to orbiting production facilities) and liquid fuel boosters to replace the srb's allowing 50,000kg payload. Its a pity those dreams have not been recognised.

The cost for development in 1980 dollars was $3bn over 10 years.
 
Old 3rd Feb 2003, 18:44
  #74 (permalink)  
 
Join Date: Jan 2000
Location: 03 ACE
Age: 73
Posts: 1,015
Received 30 Likes on 20 Posts
I reiterate, does anyone know what the Main Mission was on this particular launch.
El Grifo is offline  
Old 3rd Feb 2003, 19:29
  #75 (permalink)  
Ecce Homo! Loquitur...
 
Join Date: Jul 2000
Location: Peripatetic
Posts: 17,427
Received 1,593 Likes on 730 Posts
BahrainLad,

The British one, someone at NASA playing a blinder...
I thought it might have been possible they acquired later, but not so.

"On 21 December 1872 the 2306 ton steam assisted corvette HMS Challenger sailed from Portsmouth on a 3-year voyage of marine exploration which laid the foundations of almost every branch of oceanography as we know it today."

"After her three years of glory, her fate was even more ignominious. Commissioned as a Coast Guard and Drill ship of Naval Reserves at Harwich in July 1876, she was finally paid off at Chatham in 1878. She remained in reserve until 1883, when she was converted into a receiving hulk in the River Medway, where she stayed until she was finally broken up for her copper bottom in 1921."

El Grifo, research. See the Mission Preview.
ORAC is offline  
Old 3rd Feb 2003, 19:50
  #76 (permalink)  
 
Join Date: Nov 1999
Location: LGW
Posts: 47
Likes: 0
Received 0 Likes on 0 Posts
El Grifo, the "Main Mission" was a host of scientific experiments - a Space Laboratory, if you like. A wealth of info is avaiable on the STS-107 site at NASA. This is on the Missions site which has details of previous & future flights. Further exploration of the NASA site will answer most of the other foregoing questions (or FAQs!) on the subject.

Due to the fact that there has suddenly been an uncharacteristic surge in space-interest from the press and public, no doubt some sites are a bit slow right now.

There is also an excelent and very up-to-date site at Space.com, and many others. Hope this helps.
whitehat is offline  
Old 3rd Feb 2003, 20:56
  #77 (permalink)  
Swounger
 
Join Date: May 1999
Location: New York, NY USA
Posts: 422
Likes: 0
Received 0 Likes on 0 Posts
From the Jerusalem Post: According to news reports, a team of NASA engineers sent a report two days before Columbia's break-up on reentry stating that the damage caused to the shuttle's left wing during takeoff was greater than originally thought and could seriously affect its reentry and landing.

http://www.jpost.com/servlet/Satelli...=1044246922125

Flash presentation: http://lb.wnd.com/columbia.html

Last edited by Bubbette; 3rd Feb 2003 at 23:13.
Bubbette is offline  
Old 4th Feb 2003, 01:56
  #78 (permalink)  

Iconoclast
 
Join Date: Sep 2000
Location: The home of Dudley Dooright-Where the lead dog is the only one that gets a change of scenery.
Posts: 2,132
Likes: 0
Received 0 Likes on 0 Posts
Question What happenbed?

I entered a post on the other shuttle thread indicating that the Reliability of the shuttle degrades with every launch. NASA may make welding repairs to engine plumbing but they do nothing to determine if there is structural degradation. The Columbia accident investigation is more open and transparent than the Challenger accident and if it is proven that the thermal tiles were damaged during transition to orbit then NASA will have to accept full responsibility which they did not on Challenger.

I personally believe that NASA was not completely forthcoming relative to the cause for the Challenger accident. If anyone wishes to question me regarding this statement I will gladly post my reasoning. It can be done on this thread or on a new thread.

Lu Zuckerman is offline  
Old 4th Feb 2003, 02:06
  #79 (permalink)  
 
Join Date: Sep 2000
Location: CYYZ
Posts: 76
Likes: 0
Received 0 Likes on 0 Posts
There is much talk about "foam" hitting the left wing on launch. Could one of you better informed technical types elaborate on what this "foam" is. Was it ice? (Heard something like that on the news). For the layman foam is what you find in your couch/mattress, so all this makes no sense to me, really.

Thank you.
PCav8or is offline  
Old 4th Feb 2003, 02:58
  #80 (permalink)  

Total Internal Reflection
 
Join Date: Sep 2000
Location: Between the Tropics
Posts: 46
Likes: 0
Received 0 Likes on 0 Posts
And ORAC,
as you are no doubt aware, another of Cook's ships was the Resolution, which heroically sailed Antarctic waters, among others.

Let the next Shuttle constructed, or derivative spacecraft evolved, be so named.
rainbow is offline  


Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.