It looks like you're using an Ad Blocker.
Please white-list or disable AboveTopSecret.com in your ad-blocking tool.
Thank you.
Some features of ATS will be disabled while you continue to use an ad-blocker.
Don't take my word for it! Heavens no! You could take take the pronouncements of United States District Court Judge Denny Chin, who's opinion I quoted.
Originally posted by TrickoftheShade
reply to post by TiffanyInLA
You're claiming that structural failure definitely occurs at 426 knots? Where are you getting your data from?
Originally posted by Helmkat
reply to post by TiffanyInLA
As pointed out in the presentation, if you think the NTSB data is wrong, you should think twice about getting on an aircraft in the NY area or arriving to a terminal area, as all separation is done by speed and radar.
I understand what they are saying but they are forgetting one important condition of the situation. The aircraft were not performing within normal parameters. Radar is rythmic in nature and a lot can happen between one sweep and the next. The systems used on 9/11 and today are not optomized for conditions experienced that day. So for your everyday flights around the world? sure the systems are fine but once you have lots of course/speed/apsect changes you are entering a scenario more akin to combat situations and again the everyday traffic control systems are not up to snuff for that.
Originally posted by GenRadek
reply to post by impressme
How sudden were the manuvers? Not very sudden. The 757 video shows a very rapid climb after a high speed pass without any problems. The Airbus showed no problems at its highspeed low flyby. The KC-135 didnt show any problems either.
The aircraft that hit the WTC werent doing Immelmanns, barrel rolls or inverted figure-8s. Nor where they doing snap flick rolls. All they did was a slow turn and dive. that was it. Just a nice long dive from a higher altitude to a lower altitude.
Impressme did you read about the 747 that went into a sudden high speed dive? It held up reaching the sound barrier and reaching 5Gs in the dive. Didnt fall apart. In fact there have been quite a few instances where an aircraft encountered high speed dives approaching or breaking the sound barrier and high G stresses. Airplanes are built a little more rugged than you'd think. I would look through the NTSB record and aircraft incident sites and look at how many time planes did have some serious stresses imposed on the aircraft in crazy near crashes or dive.
Also airliners "basic" cruise speeds are higher than what you put up. For the 767 for example:
Cruise speed Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft cruise altitude)
Max. Cruise speed Mach 0.86 (493 knots, 568 mph, 913 km/h at 35,000 ft cruise altitude)
Say, now thats a LOT higher than your guess of 320mph.
That's right Tricky. It says "Caution". This zone is above the Max operating of the aircraft This is your "buffer zone". It is telling you that if you don't slow down, you are going to break the aircraft. You may even break the aircraft if the air is not smooth. Hmmm.. think the air was silky smooth that day? If the smoke coming off the North tower is any indication, it looks rather turbulent that close to the ground. Makes sense given all the buildings churning up the air flowing in from the North.
The A300-600, which took off minutes after a Japan Airlines Boeing 747 on the same runway, flew into the larger jet's wake, an area of turbulent air. The first officer attempted to keep the plane upright with aggressive rudder inputs. The strength of the air flowing against the moving rudder stressed the aircraft's vertical stabilizer and eventually snapped it off entirely, causing the aircraft to lose control and crash. The National Transportation Safety Board (NTSB) concluded that the enormous stress on the rudder was due to the first officer's "unnecessary and excessive" rudder inputs, and not the wake turbulence caused by the 747. The NTSB further stated "if the first officer had stopped making additional inputs, the aircraft would have stabilized". Contributing to these rudder pedal inputs were characteristics of the Airbus A300-600 sensitive rudder system design and elements of the American Airlines Advanced Aircraft Maneuvering Training Program.
Originally posted by g146541
reply to post by TiffanyInLA
Redline or no.
Did you know that there were 2 planes that flew into the towers?
1 plane on each tower.
There is videotape of it. There are also thousands of witnesses.
these 2 planes never broke up, well until they hit the buildings.
Is this what you are disputing?
Because I don't think the pentagon was hit by a plane, it was a missile.
However there is no video of that and apparently no witnesses.
ahh as the screen name states is good ol' dave. Still a sucker born every minute who keeps on believing the official story.
Originally posted by airspoon
With that out of the way, do we have any data on the tailwinds at altitude? If you combine the possibility to exceed the maximum operating velocity with a high tailwind and the relatively short distance that the velocity was maintained, I don't see why the conditions could not be just right as to exceed the max operating velocity by 150 knots from point to target.
Originally posted by thedman
So you are saying that once you exceed Vmax the airplane starts to break up ?