Free Republic
Browse · Search
News/Activism
Topics · Post Article

Skip to comments.

NASA engineer warned of possible shuttle breach, e-mails indicate
Jerusalem Post ^ | Feb. 22, 2003 | THE ASSOCIATED PRESS

Posted on 02/21/2003 4:34:05 PM PST by yonif

click here to read article


Navigation: use the links below to view more comments.
first previous 1-2021-4041-50 next last
To: Resolute
My recollection is that the shuttle was moving at about 1900 miles per hour when the insulations peeled off the external tank. This is about Mach 2.5, well into the supersonic velocities.

For subsonic velocities, the drag force on the foam, which accelerates it back towards the shuttle, would be proportional to the cross sectional area of the foam times the square of the velocity.

However, for supersonic velocities, I think that the drag is much higher, due to the foam having to create the supersonic shock wave and high-pressure area at its bow.

Therefore, given that the foam has little mass, a large cross-section, and is in a supersonic flow, I think that it would be very rapidly accelerated backwards toward the shuttle wing.

Do you know the correct power of velocity for drag in a supersonic flow?

21 posted on 02/21/2003 6:22:00 PM PST by Lessismore
[ Post Reply | Private Reply | To 14 | View Replies]

To: yonif

22 posted on 02/21/2003 6:34:50 PM PST by Nick Danger (Freeps Ahoy! Caribbean cruise May 31... from $610 http://www.freeper.org)
[ Post Reply | Private Reply | To 1 | View Replies]

To: Uncle George
There is a difference between a blow out on landing and it blowing up due to extreme heat. If these tires had thermal plugs like military aircraft it would not have blown. Take that same tire with the air released and expose it to the extreme airspeeds as the shuttle came apart and it would probably come to pieces. I'm not saying your hypothesis is incorrect. I'm giving my two cents based on a high performance aircraft (though strictly atmospheric) background.
23 posted on 02/21/2003 6:43:14 PM PST by USNBandit
[ Post Reply | Private Reply | To 15 | View Replies]

To: Resolute
Dude, I was told there would be no math.
24 posted on 02/21/2003 6:45:40 PM PST by USNBandit
[ Post Reply | Private Reply | To 14 | View Replies]

To: Uncle George
I posted here two days after the shuttle breakup that the left tire exploded and blew the wing off so we freepers are pretty good detectives also.

I was posting some things too. See #6

25 posted on 02/21/2003 7:19:21 PM PST by isthisnickcool
[ Post Reply | Private Reply | To 8 | View Replies]

To: Milwaukee_Guy
"Why only 0.5 times mass though?"

I probably learned that once upon a time, but I don't recall exactly. It probably has to do with the relationship between Kinetic Energy (KE) and Potential Energy (PE). KE is as stated previously. PE of a raised object given by:

E = M*g*h

where M = mass, g = acceleration due to gravity, and h = height. If we raise an object of mass "M" to at height "h" (assuming velocity = 0 at the top), then when it falls to the starting point, its KE will be 0.5*M*V^2 (assuming no slowdown due to drag).Thus KE = PE or

M*g*h = 0.5*M*V^2

This has to do with the fact that when the object falls through height "h" the time of descent "t" is related to "h" by

h = 0.5*g*t^2

which yields

t = sqrt ( 2*h/g)

The terminal velocity is given by

V = g*t

When we play with all these terms, starting from KE = PE, the 0.5 term gets in there. Yes, I may have made this too complicated, and maybe even made a logic mistake, and no I am not trying to be obtuse. That is just the way I remember it from long ago . . .

26 posted on 02/21/2003 7:46:32 PM PST by Resolute
[ Post Reply | Private Reply | To 19 | View Replies]

To: Lessismore
"Therefore, given that the foam has little mass, a large cross-section, and is in a supersonic flow, I think that it would be very rapidly accelerated backwards toward the shuttle wing."

We looked at this on another thread, and it would be easier for you to visit that thread, than for me to rehash it here. Here are some links:

Nominal ascent timeline (reference data)

Simulated Drag Effects

Impact velocity vs. Drag Coefficient

27 posted on 02/21/2003 7:58:52 PM PST by Resolute
[ Post Reply | Private Reply | To 21 | View Replies]

To: Lessismore
Here's a link to discussion of drag force and coefficient of drag:

Drag coefficient vs. Mach number (for spinning metal cubes)

The data are for spinning steel cubes, 1/4 to 3/8 inch per side. I am not an aerodynamics whiz. These data may or may not apply to larger or smaller debris of arbitrary shape and roughness.

28 posted on 02/21/2003 8:44:54 PM PST by Resolute
[ Post Reply | Private Reply | To 21 | View Replies]

To: USNBandit
Sorry :-) I really didn't want to do any math. Unfortunately it is very hard to convey the notion that even foam can impart a HUGE amount of kinetic energy, without going to the basic physics & math. If we ignore the math, it becomes very easy to let O'Keefe get by with saying that the foam striking the wing, is like a styrofoam beer cooler hitting your windshield at highway speeds. When we go to the math, we find that 4 or 5 orders of magnitude more energy is involved.
29 posted on 02/21/2003 8:59:33 PM PST by Resolute
[ Post Reply | Private Reply | To 24 | View Replies]

To: Resolute
Besides problems in previous flights, the foam/ice sloughed off two flights before. It wacked the SRB and put a good dent in it. The SRB external skin is not real tough but I expect it's tougher than the "carbon" material on the leading edge of the wing.

NASA knew they had a problem with the material coming off the external fuel tank. They should have grounded the shuttles like some people were calling for after STS-112 which was flight when material from the external fuel tank dented the SRB.

Supposedly, the crew could see the damage to the leading edge of the left wing. One of the crew emailed his wife about the damage. Rumor is that after the accident she brought this up to the suits at NASA and they sent a "group" out to see if indeed it was possible to see the damage by "eyeballing" using one of the mockup/trainers. The "group" supposedly concluded it was not possible to see the damage. The people that assisted the "group" with this, it is rumored, were agitated at this news since they did not agree and felt that it was obvious the crew could see the damage. From the flight deck and maybe from another spot.

NASA knew material was coming off the external tank and hitting parts of the system and they let the shuttle fly. Bummer....

30 posted on 02/21/2003 9:10:22 PM PST by isthisnickcool
[ Post Reply | Private Reply | To 27 | View Replies]

To: yonif
This E-mail relates to what they should do if data tells them there is no pressure in both tires on the left main landing gear. Should Colombia have ever had opportunity to make the final approach, I'm sure they would have been given their options of bail out, belly or gear down landing. They got the tire pressure failing data some 15 minutes or so before their scheduled landing so there was nothing they could have planned for before committing to retro burn. There is no hidden NASA agenda here.

What I think happened, based on small but larger than I expected damage possible from impact of the foam (ramp covering), is that it actually hit the leading edge carbon-carbon, either in close proximity to or in such a place that the leading edge deflected sufficiently from the impact, so as to disrupt the carbon-carbon "T" seal between these panels or damage the panel attach fittings so that upon initial reentry the seal failed or the panel broke loose. This TPS breach would have allowed hot gasses to enter the wing, leading to structural failure.

Few of these hot gasses would have entered the wheel well, accounting to the relatively low temperature increases. The "T" seal failure would have led to local carbon-carbon panel separations, or the attachment failure would have had the same effect, either of which would have shown the same irregular leading edge profile "jagged edge" that appeared in the Air Force long range photograph.

If the failure was in extensive tile damage, I don't think we would have gotten the "jagged edge" photo but rather the wing would have failed without the upstream leading edge damage.
31 posted on 02/21/2003 9:26:49 PM PST by NJJ
[ Post Reply | Private Reply | To 1 | View Replies]

To: silverlizzard; DoughtyOne; Milwaukee_Guy; Uncle George; dep
<< This program should be halted. I don't know how those poor guys get down in the space station. I bet they send one guy up to get them and then quit this nonsense. >>

<< NASA, "Well Boeing said it was OK." Boeing: "Well NASA has operational control. We just make the silly tiles for them." >>

The Siberia-based "Russian" branch of the abjectly-corrupt and systemically-dishonest NASA
[Never in the History of the Human Species has so much of the confiscated wealth of
America's (Of the world's, that is) most creative, innovative, productive and industrious Men been
S quandered on so few in their
Accomplishment of so little] can send a Soyez and; after they have dropped NASA's floating junkyard into the Atlantic; drop them back to Siberia.

Columbia's demise was as inevitable as was Challenger's as is the entire Rube Goldberg/Heath Robinson-Joint-Venture designed and low-bidder gummint-contractor built "space" shuttle boondoggle.

NASA and its contractors current one-legged-man-in-an-arse-kicking-contest-like exercise in butt covering and buck shuffling brings to mind the valiant efforts of the last American Man of Moral Integrity to have been allowed near NASA, the Modern American Hero, Morton Thiokol's Roger M. Boisjoly.

Engineer Boisjoly predicted Challenger's loss and paid the price extracted by our much-vaunted Peter-Principled feral-gummint bureaucracy and by its universally-corrupted-by-the-relationship suppliers and contractors from all those who dare challenge the bureaucrats' systemic "the world is flat" and "the emperor is not naked" approach to building their own unearned power and influence by the inevitably-corrupt squandering of other peoples confiscated wealth.

32 posted on 02/21/2003 9:53:37 PM PST by Brian Allen (This above all -- to thine own self be true)
[ Post Reply | Private Reply | To 11 | View Replies]

To: USNBandit
Dude, I was told there would be no math.

Well, now we're experiencing the aftermath.

33 posted on 02/22/2003 1:42:10 AM PST by Erasmus
[ Post Reply | Private Reply | To 24 | View Replies]

To: Resolute
Thanks for the links. It appears that the drag still increases with the square of the velocity, and that the supersonic flow effects are characterized by increasing the drag coefficient by about 50%. That would increase the velocity of the impact above the 500 MPH that NASA quoted.
34 posted on 02/22/2003 8:36:05 AM PST by Lessismore
[ Post Reply | Private Reply | To 28 | View Replies]

To: Brian Allen
DOCTOR Roger M. Boisjoly:
Memo writer says Thiokol froze him out of work:
Reassignment given 2 workers in O-ring warning

Houston Chronicle, Jan. 25, 1987

A MORTON THIOKOL Inc. engineer who warned of problems with the Challenger's solid rocket booster O-rings six months before the disaster last January says the company has turned him into a "non-entity" because of his revealing testimony before the Rogers commission.

The commission blamed the shuttle accident on the faulty O-ring seals in the rear of the Challenger's right solid rocket booster, manufactured by Morton Thiokol.

The engineer, Roger M. Boisjoly of Willard, Utah, is one of two men who wrote in-house memos before the disaster warning of a potential catastrophe because of problems with the booster's O-ring seals. On the eve of the January Challenger launch, Boisjoly recommended that Challenger not be launched.

The other man is Richard C. Cook, 40, a former senior analyst with the National Aeronautics and Space Administration headquarters in Washington, now with the U.S. Treasury Department. Cook also testified before the Rogers commission. [...]

Boisjoly is still on the Morton Thiokol payroll but he is not working, he said in a recent telephone conversation.

After testifying before the Rogers commission, Boisjoly was assigned to a team of Morton Thiokol engineers charged with redesigning the solid rocket booster (SRB). But, he said, he was never allowed to participate and wasn't allowed to attend meetings, and has now stopped reporting to work. "It was a terrible environment," he said.

"On the one hand, I was part of the redesign team but on the other hand I wasn't allowed to participate in the meetings. So basically, I was a non-entity, if you will," Boisjoly said. [...]

Allan McDonald, ther Morton Thiokol engineer who had warned about the O-ring problem and who also testified before the commission, was reassigned by the company after his testimony. [...]

Without mentioning Boisjoly, company President Charles S. Locke later told the Wall Street Journal that "people are paid to do productive work for our company and not to wander around the country gossiping with people."[...]

"I didn't know any of the Morton Thiokol guys, but the shuttle flight in April (1985) had suffered a secondary erosion of the nozzle O-ring," Cook said. "That had alarmed Roger and it alarmed people at the Marshall Space Flight Center. The NASA center was responsible for the rocket booster development."

Cook says he left the space agency because his job required extensive overtime, and he wanted to spend more time with his family. He left NASA before he testified, but not before his warning in-house memo had been publicized.

"I felt freer to speak to the Rogers commission than if I had stayed at NASA," said.

"The people at NASA were angry because I spoke to the press (about the O-ring problem). I was told to say things to the press and the commission that I did not think were right, and I was told someone on the commission wanted to discredit me.

"Actually, my memo only repeated what some of the most senior NASA officials were saying (about the O-rings) and the most alarming stuff I didn't even put in my memo. There were (NASA) headquarters' engineers with 20 and 30 years experience who knew about the seriousness of the problems, and they were never called to testify by the Rogers commission."[...]


35 posted on 02/22/2003 9:16:05 AM PST by bvw
[ Post Reply | Private Reply | To 32 | View Replies]

To: Brian Allen; Fred Mertz; TLBSHOW; Admin Moderator
We see the old "Shoot the Messenger" pack mentality -- one that keeps sicknesses from being cured, btw -- quite a lot around old FR lately.

It's a very old social dynamic.

36 posted on 02/22/2003 9:23:33 AM PST by bvw
[ Post Reply | Private Reply | To 32 | View Replies]

To: bvw
<< We see the old "Shoot the Messenger" pack mentality -- one that keeps sicknesses from being cured, btw -- quite a lot around old FR lately. >>

Yep.
37 posted on 02/22/2003 9:34:39 AM PST by Brian Allen (This above all -- to thine own self be true)
[ Post Reply | Private Reply | To 36 | View Replies]

To: bvw
Thanks for the ping over. You already know my feelings bvw. Nasa should never of been allowed to fly this shuttle.

38 posted on 02/22/2003 9:50:38 AM PST by TLBSHOW (God Speed as Angels trending upward dare to fly Tribute to the Risk Takers)
[ Post Reply | Private Reply | To 36 | View Replies]

To: TLBSHOW
This quote from the washington post article today...
We can't imagine why getting information is being treated like the plague. Apparently the thermal folks have used words like they think things are survivable, but marginal," Daugherty said.
That's what is bothering about this whole thing is the coverup. Even engineers on the inside can not seem to avoid flying safes.

39 posted on 02/22/2003 11:21:06 AM PST by fooman (PC Kills!)
[ Post Reply | Private Reply | To 5 | View Replies]

To: isthisnickcool
IF true, group think at its finest. I remember the email story too in the early days of this mess.
40 posted on 02/22/2003 11:30:50 AM PST by fooman (PC Kills!)
[ Post Reply | Private Reply | To 30 | View Replies]


Navigation: use the links below to view more comments.
first previous 1-2021-4041-50 next last

Disclaimer: Opinions posted on Free Republic are those of the individual posters and do not necessarily represent the opinion of Free Republic or its management. All materials posted herein are protected by copyright law and the exemption for fair use of copyrighted works.

Free Republic
Browse · Search
News/Activism
Topics · Post Article

FreeRepublic, LLC, PO BOX 9771, FRESNO, CA 93794
FreeRepublic.com is powered by software copyright 2000-2008 John Robinson