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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…
Figures 2 and 3 shaw the tear-drop cell ot the stressed tape
design developed by General Mills, Inc. The tilm is .001 inch polyethylene,
but_t-welded, with scotch tape laid along the seam to reinforce the seal and
to carry and distribute 1he load. These strips, which converge to the loaa
ring at the bottom, actually support the load.
The overloading ot a General Mills 20-tdot balloon on Flight 12 at
Lakehurst kept the lower end of the balloon open during ascent. The
ceiling was greatly reduced by the resulting dilution ot the helium with
air. On later flights an unsuccessful attempt to minimize this mixing
was made, using a 10-toot external appendix passing through the shroud
lines. This appendix fouled ir1 the rigging and twisted completely shut,
causing the balloon to burst at pressure-altitude. A moditicationwith
a 10-foot appendix outside the shroud lines also tailed in actual flight.
Figure 4 shows this appendix construction on a General M lls balloon which
is being inflated. The final style is shown in Figures 5 and 6. It con-
sists of a 2-foot external appendix stiffened with cardboard battens.
This is taped on the outside of the load ring. It serves as a one-way
valve which excludes air during ascent but allows the extra helium to
valve freely when the balloon is full. No external appendix can be used
Whenever the rate of rise exceeds 600 feet per minute. For optimum balloon
performance, it has been determined that: 1) the equipment load for the
General Mills 20-foot balloon should be held tinder 30 pounds; 2) ratEBot
rise should be less than 900 feet per minute; and 3) for maximlml altitudes
an external e ppendix is needed; hence 1he limiting rate of rise is about
600 feet per minute in this case.
Several experimental flights have been made using shrouded Dewey
and Almy neoprene balloons, as well as small and large experimental cells in
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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.