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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…
Flight 12 was designed to overcame the difficulties encountered
in flights 8 and 11, and, by the use of a thin tear-drop balloon (General
Mills balloon) to earn~ the load to a higher altitude than flight 10.
To guarantee a predetermined constant ballast flaw, the manual ballast
valve we.s added to the flight train. The minimum pressure switch
replaced the fixed pressure switch to activate the automatic ballast
valve, whether or not a predete~ined activation altitude was reached.
Figure 46 shows the train; figure 47 shows the time-altitude curve, Which
exhibits a marked departure from the ideal. The minimum pressure switch
failed to operate or operated near surface pressure, effectively preventing
the operation of the automatic ballast valve. The manual ballast valve did
not provide sufficient rlow to prevent the gradual descent of the balloon.
Finally, the heavy load necessitated almost complete inflation of the
balloon at the surface. lhis distention permitted continual mixing of
air through the open bottom of the balloon. Instead of reaching the pre-
calculated 38,000 feet maximum altitude, this flight had a peak of 14,000
feet from which it slowly descended. Since the blowout patch was set to
act upor. descent to 20,000 feet, it also failed to operate.
Five of the succeeding flights (nos. 13, 14, 15, 16 and 20) had as
a prime objective the development of a satisfactory a.ppendix to overcome
the loss of buoyancy due to mixing during launching and ascent. fhe types
considered have been discussed in Section II, Part A of this· report and
the (two foot) appendix stiffened with battens, Which was finally evolved,
is shown in figure 5. Figures 48, 49 and 50 show the time-altitude curves
for these flights. Either short flight or limited radio reception curtailed
the trajectory data.
In flight 19, the danger to perscrmel of the blowout patch was
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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.