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roswell

Office of the Secretary of Defense · 993 pages · text from the file's own layer

The Roswell Report: Fact versus Fiction in the New Mexico Desert was published in 1995 by Headquarters United States Air Force. It was written in response to Representative Steven H. Schiff's request and a General Accounting Office audit, and it contains Col. Richard L. Weaver's report and 1st Lt. James McAndrew's synopsis, along with attachments, appendices and photographs. The report says researchers found no evidence of an extraterrestrial craft or crew. It concludes that the 1947 debris came from a Project MOGUL balloon train.

  • p. 129 …6099 2 HQ AMC WRIGHT PAT 342-seA-6191 CAMBRIDGE LABS 342-A~ AMC HQ WRIGHT…
  • p. 228 …overhead and followed the balloons out to sea. I have no idea about the results that…
  • p. 235 …the regular 334 that we had at sea level. From that they could deduce the temperature…
  • p. 279 …actually located on the jurisdictional lines between Sea Girt and Springlake, New Jersey. It was an…
  • p. 280 …The Sea Girt Inn? A: Exactly. That's where John had his office, and I was…
  • p. 400 …alone 1a about 24,000.m1lea at sea level, aDd about '500 allea at 45,000…
  • p. 407 …five (25) feet at their ls.rgest sea-level diameter. The sonic unit was a combination…
  • p. 466 …hour when one-fifth inf~ated at sea level). One other type of balloon which has…
  • p. 490 …Let us, then, compare the rate of leakage at any given altitude with leakage at sea…
  • p. 492 …The leakage at any altitude may be expressed as a function of leakage at sea level…
  • p. 493 Comparing rete of leakage at 40,000 feet with leakage at sea level: ~ 188 .u§. - 0…
  • p. 495 …It a 20-foot diameter balloon~ full were tested at 10 sea level and found to…
  • p. 496 …At sea level this is equivalent to 5.32 ~r. for a 20-foot diameter balloon…
  • p. 502 …Using the rules of subsonic aerodynamics, Picard suggests that air at sea level escaping at 1333…
  • p. 503 …sea level (psi) escape velocity of air to produce back pressure of 1 atmosphere at sea…
  • p. 520 …to about 20 millibars and increased to sea-level pressure at different temperatures. The most comprehensive…
  • p. 654 …The height above mean sea level as determined fram pressure measurements used in this work with…
  • p. 686 …to a thtmble a.nd attached to re1n forced pCltches at alterna.te .sea.m.s…
  • p. 688 …lQr9e Ba.lloo n ~hould trQin de .sea nd to 101000'. 6 each.-Gene ral M1lls…
  • p. 736 …point at which the radiosonde reaches the sea surface. 2. Earlier attempts There have been numerous…
  • p. 737 …The balloons floated between the surface and 30,000 ft above sea level; those which reached…
  • p. 801 …Vet Gifford ;.;ho has 0 0' sea rescue boat this project is planning to use. Stayed…
  • p. 816 …Worzel working on gravity at sea. Saw Geo Woollard and the Ryders. Woollard after Guggenheim fellowship…
  • p. 887 …the launching site is markedly different from sea level, a shift in this curve is needed…
  • p. 925 …balloon at all times with respect to sea level. On this curve also it is customary…
  • p. 933 …The height above ~ean sea level as determined from pressure measurements used in this work with…
the pressure distribution of the liftinc gas and the internal
back pressure due to valving gas. To find maximum rates of
ascent for various balloons would necessitate a complicated
series of trial and error solution. In general, it has been
more practical to determine a maximum rate of rise for nor.mal
operating conditions for any given size balloon by findin~ the
maximum allowable rate for the balloon rising to its lowest
normal operating level (i.e., we will find the maximum all0?18ble
rate for the worst normal operating conditions and consider
it a maximum for all normal operating conditions.)
Let us take the case of a 20-foot diameter polyethylene balloon
of .001~ thickness. Lowest normal floating altitude is 20,000 ft.
MSL. Let us assume that the balloon will be full and begin
valvinf gas at 15,000 ft. MSL. Assume the appendix diameter
to be 2 foot. Using equation (1) to find maximum allowable
internal pressure and assuming the critical x-y plane to be that
of maximum diameter A~ = D/2 , we have:
A Pall. = 4 SJt = 4(900/2)· .001 = . 007 5 psi
t2· 20
(Here we have introduced a factor of safety by saying Sf =900/2
instead of 900 psi, the ultimate strength in tension of poly-
ethylene.) Pressure distribution:
A.p 012 = A~ :l (I-B) = l-2°·3.38 ·10-4 • .862 = .00291 psi
Allowable back pressure:
A Pbp =Ap 011 - AP012 = .0046 psi
Maximum rate of rise using equation (13)J
( 2780° C A \ fttsecv d a}
= 100.7 ft/sec
= 6000 ft /min
It is evident from this calculation that the rate of rise of the
20-ft. diameter polyethylene balloon is not a critical factor
in bursting unless the open appendix becomes snarled an~ gas is
not allowed to escape.
Rate of rise and appendix openings are important from the stand-
point of balloon design. For operationel reasons it is important
to have a rapid rate of rise. In order to make most efficient
use .of weight, the balloon film should be thin. As mentioned
-55-

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FOIA release, from the osd collection. The PDF is mirrored here; the original link is under it. 993 pages are in the text index: search them above, or from the library's search.