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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…
Position of recording and radio instruments in the flight
train is in some oases dictated by the size and shape of
antennae or other special part. In general this type of
gear is not placed below the altitude control equipment
because of possibl~ damage which might result from
ballast being dropped upon them. ~pical trains are shown
in Figures 16, 17, and 18.
F. Flight Tools and Equipment
A list of tools and equipment and facilities which should
be provided for any launching site is given in Appendix II.
IV. PRE-FLIGHT COMPUTATIONS
A. Lifting Gas and Rate of Rise
When the equipment for a flight is in readiness and the
inflation procedure is to be begun, the total weight to
be lifted must be determined. A weight sheet (Shown in
Appendix I) is filled in, with the final weight of each
piece of gear with its rigging. In this work the wei~hts
of the equipment are measured in grams and kilograms. for
ease of computation. The gross load reported should be
accurate to the nearest 200 grams. The amount of lifting
gas to be used must be carefully figured to prevent in-
correct inflation which might result either in the bal-
loon failing to rise, or perhaps rising too fast and rup-
turing at its ceiling. After the total weight to be
lifted is found, a percentage of this total is added to
provide for lifting the load at some specified rate.
With a given excess of buoyancy, a balloon will lift its
load at an almost constant predictable speed. (The rate
of rise will increase by about 25% at higher altitudes,
due to the changes in balloon shape and decrease of air
density.) Graph 1 of Appendix II shows the relationship
between the free lift and the :t-ate of r·ise, with free
lift expressed as a percentage of the total or gross load
(which includes the weight of the balloon itself). For
example, if a gross load of 10.0 kilograms is to be lifted
at a desired ascent rate of 600 feet per minute, 9.2%
of the gross load should be added, giving a gross lift
of 10.0 t .920 • 10.920 kilograms. (The rete of rise
should not exceed 700 feet per minute if a standard appen-
dix is used.)
It should be noted that this graph, derived from equations
for spherical balloons, applies also to the tear-drop cells
of General .Mills, Inc., without regard for the balloon
die.mter.
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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.