It's not that they believe the path is miles off. They are trying to find a way to pinpoint further using the existing path.
Exactly.
Except if you get sucked in by ELVIS you will wind up believing the Cooper hijacking involved twenty camels being sold to Iraq at below market prices, all to forstal global warming in Seattle, in case residents of Seattle should ever want to vacation is Israel! The plot to end all plots.
Georger, You are the one putting out the BS (or is it CS?). You haven't come up with a single rational explanation to justify your claims about the validity of the FBI flight path.
Deny and deflect and then claim you are not doing either one. I'll bet you are on a short list for a presidential cabinet appointment.
Specifically what!? Be specific for a change?
Since you wont be specific let me be specific! Quote:
Eric,, EU wrote
“It is noteworthy that in August of 1972 the FBI reviewed the NORJAK file which led to some things including what they termed “a more accurate method of plotting of radar data of the NORJAK flight using a computer.” Additionally, they said a “new search area” was plotted and searched with negative results.
SAGE? Why the uncertainty?”
REPLY BY FLYJACK:
Your answer is in the files… they used a more accurate method for plotting the SAGE data, from a 1 mile error to 1/2 mile.
FBI FILE PART 30 P 10802
Re: Seattle airtel to the Bureau, 2/7/73.
SEARCH AREA AND COURSE
In attempt to determine the accuracy of the first search area, the following was learned:
The first search area was calculated using a system of plotting known as “GEOREF” (i.e. Geographical Reference) which has a plotting error of plus or minus one mile. A new system using latitude and longitude has a plotting error of plus or minus 1/2 mile. Using the new system, ___________ Northwest Orient Airlines ________ plotted a new course for the Norjak airplane and a new search area based on the new course. The new search area is partially outside the first area.
It is felt that if Unsub’s parachute opened, he is no longer in the southwest Washington area, but if his parachute did not open, he would be in a corridor along the flight path. The time of jump is known, and an area approximately one mile by seven represents the area Unsub. would have landed in if his parachute did not open.
Seattle Division is currently making arrangements to search that portion of the above described area not previously searched.
Okay, let's be specific. The above indicates that the if Cooper was a no-pull, he would have landed in a corridor along the flight path that was "approximately one mile by seven (statute miles?)". In and off itself, this statement is wildly inaccurate.
It is a given that as a no-pull, Cooper would have landed along the flight path. Hopefully, by this point in time the members of this site are in agreement that neither Cooper nor the placard would have landed upwind of the flight path. If you can't understand this point then don't bother reading further.
The standard accepted values for a typical sky diver in a stable spread position is that he will be descending at about 120 MPH at sea level if he is a no-pull. Also, if the same sky diver is descending head first he will be doing about 180 MPH at sea level if he is a no-pull. While I haven't bothered to check it out, my guess is that a tumbling sky diver will be doing somewhere between these two values under the same conditions. At higher altitudes, the descent rates will be greater.
To keep things simple, lets assume that the airliner was two statute miles (10,560 feet) above sea level when Cooper jumped. From charts that I remember seeing somewhere, at the 225 MPH speed that the airliner was probably traveling when Cooper jumped, his forward motion would have been reduced to zero in about 1500 feet and he would also have been about 1500 feet below the airliner's flight path at that point. His descent path would then have been straight down with respect to the local air mass (the winds aloft were moving the air mass horizontally).
With a vertical descent rate of 120 MPH, Cooper would have been on the ground and dead in about one minute. With a vertical descent rate of 180 MPH, Cooper would have been on the ground and dead in about 40 seconds.
Assuming that the airliner had a 30 MPH headwind that was 45 degrees off the flight path, that would be a 21 MPH wind component blowing the sky diver back down the flight path and a 21 MPH wind component perpendicular to the flight path.
If Cooper was descending at 120 MPH for one minute, he would have been blown about 1850 feet back down the flight path and the same distance perpendicular and downwind to the flight path. If Cooper was descending at 180 MPH for 40 seconds, he would have been blown about 1235 feet back down the flight path and the same distance perpendicular and downwind to the flight path.
So the ground "impact zone" for Cooper as a no-pull is basically as follows:
1. Along the flight path, from about 350 feet before his jump point to about 265 feet after his jump point. This is a total distance of about 615 feet.
2. Perpendicular to the flight path, from about 1235 feet to 1850 feet from the flight path which is also about 615 feet.
3. In reality, the impact zone is a parallelogram with the end points as indicated above.
The whole point of the above is that the ground impact area for Cooper as a no-pull would have been quite small. The one mile by seven mile estimate is grossly overstated.
As always, if better information about the flight path is released then the Cooper no-pull ground impact estimate can be refined.