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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 balloon can rise slowly until the balloon is again full and the
equilibrium is again reached between the buoyancy and the load. In tb3
General Mills 20-foot balloon, for example, diffusion losses equal about
300 grams per hourJ the balloon at its ceiling of 50,000 feet, with a
30-pound payload, risea about 900 feet with each kilogr~ of ballast
dropped. This means that a balloon, using the simple ballast-dropping
technique, will float at a ceiling·which rises at the rate of about 360
feet per hour. An idealized flight of this type is shown in the llolid
curve of Fig. 7., neglecting the oscillation shown at sunset.
The "manual ballast valve" Which was developed for this simple
control system is shown in Fig. a. This valve can be adjusted prior to
balloon release to allow any predetermined flow of compass fluid up to
2000 grams per hour. The filter housing and ballast reservoir used
with this valve are shown in Figures 9 and 10. This method is good where
l) a slowly rising ceiling can be tolerated, and 2) the flight tloes not
have to go thrcugh a sunset while at its ceiling.
For economy of ballast, hence longer flight duration, it is desirable
to keep the constant flow as close as possible to the total loss of buoyancy
resulting from diffusion and leakage. This means that whenever rapid loss
of buoyancy occurs, due to changes in solar radiation, the manual ballast
valve alone will not sustain the balloon. When the balloon is suddenly
cooled, due to sunset or clouds cutting off in§olation (loss of superheat),
the heavy loss will start the balloon downward and only a rapid expenditure
of ballast will check its fall and restore its stability.
The second type of ballast dropping control has been devised to
operate on a demand basis, when such a descent occurs. This control is
called the automatic ballast valve. Figures 11, 12 and 13 shaw the ap-
pearance and design of this pressure-actuated needle valve.
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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.