Documents / FOIA release

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 and permits gas to be introduced into the
top of the cell first. As the balloon is laid out and
shotbags are positioned, this tube must be kept clear.
At the point where the bubble is pinched of£ the folds
of the balloon are carefully divided; the inflation tube
is made as free as possible with only one layer of poly-
ethylene above and one below it. The tube is then pulled
up above and between the arms of the releasing device or
the heavy shot bags, and the remainder of the fabric is
pinned down so that no shifting will permit premature re-
lease.
Depending upon the load to be lifted and the rate of rise
desired, a pre-computed amount of helium is fed into the
balloon (see Section IV, A). This amount is determined
by noting the equilibrium pressure and temperature of
the gas in each cylinder. A manifold is used to feed the
gas from the tanks to the inflation tube in the balloon.
Shown in Figures 26 and 27 this manifold system consists
of an adjustable number of flexible pigtails leading into
a main line of heavy copper tubing. This main line and
the fittings are capable of ~hstanding the full tank
pressure of about 2500 feet psi. Two pressure gazes are
included in the main line and it is thus possible to make
last-minute checks of the amount of gas (pressure) in
each tank. (Due to variable gage-calibrations, it has
been found necessary to establish the lift-pressure. ratio
of each gage before using it.) In the main line of the
manifold, two valves control the gas flow. The inflation
tube is often initially twisted when the balloon is first
laid out, A small amount of gas at very low pressure
Should be valved into the tube to strengthen it. In addi-
tion to the fine valve control required for this pre-
liminary gas feed, it is also nedessary for e manifold
valve to permit high gas flow from the tanks even when
the pressure is greatly reduced. For this, the coarse
globe valve is used.
Once the tube has been chedmd, inflation should proceed
as rapidly as possible. The balloon is outdoors and so
subject to buffeting by the wind. The limiting factor
of sr·eed of inflation is the vibration of the fabric
near the open end of the inflation tube.
A~ a result of the extreme cooling of the rapidly expanding
gas, the manifold and the tank valve generally become
coated with frost. Too rapid cooling may actually cause
the valve to freeze shut.
-44-

Cases discussed

About this file

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.